blob_id stringlengths 40 40 | directory_id stringlengths 40 40 | path stringlengths 6 214 | content_id stringlengths 40 40 | detected_licenses listlengths 0 50 | license_type stringclasses 2 values | repo_name stringlengths 6 87 | snapshot_id stringlengths 40 40 | revision_id stringlengths 40 40 | branch_name stringclasses 15 values | visit_date timestamp[us]date 2016-08-04 09:00:04 2023-09-05 17:18:33 | revision_date timestamp[us]date 1998-12-11 00:15:10 2023-09-02 05:42:40 | committer_date timestamp[us]date 2005-04-26 09:58:02 2023-09-02 05:42:40 | github_id int64 436k 586M ⌀ | star_events_count int64 0 12.3k | fork_events_count int64 0 6.3k | gha_license_id stringclasses 7 values | gha_event_created_at timestamp[us]date 2012-11-16 11:45:07 2023-09-14 20:45:37 ⌀ | gha_created_at timestamp[us]date 2010-03-22 23:34:58 2023-01-07 03:47:44 ⌀ | gha_language stringclasses 36 values | src_encoding stringclasses 17 values | language stringclasses 1 value | is_vendor bool 1 class | is_generated bool 1 class | length_bytes int64 5 10.4M | extension stringclasses 15 values | filename stringlengths 2 96 | content stringlengths 5 10.4M |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
da8dc71d5f78699e52e4bd2746caf6387d3b3d48 | a62e0da056102916ac0fe63d8475e3c4114f86b1 | /set9/s_Engineering_Physics_S._K._Srivastava_And_R._A._Yadav_2780.zip/Engineering_Physics_S._K._Srivastava_And_R._A._Yadav_2780/CH3/EX3.36/Ex3_36.sce | cfe2a3674d8073a0c2e18f7937c1bc211262e610 | [] | no_license | hohiroki/Scilab_TBC | cb11e171e47a6cf15dad6594726c14443b23d512 | 98e421ab71b2e8be0c70d67cca3ecb53eeef1df6 | refs/heads/master | 2021-01-18T02:07:29.200029 | 2016-04-29T07:01:39 | 2016-04-29T07:01:39 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 260 | sce | Ex3_36.sce | errcatch(-1,"stop");mode(2);
//to calculate limit of resolution of the telescope
lambda=5890*10^-8 //wavelength in cm
a=1 //diameter in cm
theta=1.22*lambda/a
disp("the limit of resolution of the telescope is theta="+string(theta)+"radians ")
exit();
|
b4ee734886e5a9c554c3fad1484012566ecd0cb7 | 449d555969bfd7befe906877abab098c6e63a0e8 | /991/CH24/EX24.3/Example24_3.sce | 435417ee56937706d39fa31b8ca95a65ef406cde | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 472 | sce | Example24_3.sce | //Example 24.3. convert decimal to hexadecimal number
clc
h=dec2hex([112])
disp("The procedure is as follows,")
disp("(i) 112 divided by 16 = quotient 7 with a remainder of 0")
disp(" 7 divided by 16 = quotient 0 with a remainder of 7")
disp(h,"decimal 112 = hex")
disp("(ii) 253 divided by 16 = quotient 7 with a remainder of 13 i.e. D")
disp(" 15 divided by 16 = quotient 0 with a remainder of 15 i.e. F")
h=dec2hex([253])
disp(h,"decimal 253 = hex") |
384d11c23d1c11ba36355591f3990fb1cbf7f252 | 36c5f94ce0d09d8d1cc8d0f9d79ecccaa78036bd | /Instakill.sce | 60498408fa04aaf11e24a752e148e37211ff3c32 | [] | no_license | Ahmad6543/Scenarios | cef76bf19d46e86249a6099c01928e4e33db5f20 | 6a4563d241e61a62020f76796762df5ae8817cc8 | refs/heads/master | 2023-03-18T23:30:49.653812 | 2020-09-23T06:26:05 | 2020-09-23T06:26:05 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 70,750 | sce | Instakill.sce | Name=Instakill
PlayerCharacters=Quaker Rail
BotCharacters=Quaker Bot lowH.bot
IsChallenge=true
Timelimit=300.0
PlayerProfile=Quaker Rail
AddedBots=Quaker Bot lowH.bot
PlayerMaxLives=0
BotMaxLives=0
PlayerTeam=1
BotTeams=2
MapName=liloput2.map
MapScale=4.0
BlockProjectilePredictors=false
BlockCheats=true
InvinciblePlayer=false
InvincibleBots=false
Timescale=1.0
BlockHealthbars=true
TimeRefilledByKill=0.0
ScoreToWin=100.0
ScorePerDamage=0.0
ScorePerKill=1.0
ScorePerMidairDirect=0.0
ScorePerAnyDirect=0.0
ScorePerTime=0.0
ScoreLossPerDamageTaken=0.0
ScoreLossPerDeath=1.0
ScoreLossPerMidairDirected=0.0
ScoreLossPerAnyDirected=0.0
ScoreMultAccuracy=false
ScoreMultDamageEfficiency=false
ScoreMultKillEfficiency=false
GameTag=Quake, flick, instagib
WeaponHeroTag=Rail
DifficultyTag=2
AuthorsTag=ikool
BlockHitMarkers=false
BlockHitSounds=false
BlockMissSounds=true
BlockFCT=false
Description=Fight the bots on the map with your Rail. One click one kill.
GameVersion=1.0.5
[Aim Profile]
Name=At Feet
MinReactionTime=0.3
MaxReactionTime=0.4
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=15.0
TrackSpeed=3.5
TrackError=3.5
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=40.0
ShootFOV=15.0
VerticalAimOffset=-200.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Aim Profile]
Name=Medium Skill
MinReactionTime=0.3
MaxReactionTime=0.4
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=15.0
TrackSpeed=3.5
TrackError=3.5
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=40.0
ShootFOV=15.0
VerticalAimOffset=0.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Aim Profile]
Name=Default
MinReactionTime=0.3
MaxReactionTime=0.4
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=15.0
TrackSpeed=3.5
TrackError=3.5
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=40.0
ShootFOV=15.0
VerticalAimOffset=0.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Bot Profile]
Name=Quaker Bot lowH
DodgeProfileNames=Circle Strafe;Short Strafes;Long Strafes NO Jump
DodgeProfileWeights=2.0;2.0;2.0
DodgeProfileMaxChangeTime=5.0
DodgeProfileMinChangeTime=1.0
WeaponProfileWeights=1.0;0.0;1.0;1.0;1.0;1.0;1.0;1.0
AimingProfileNames=At Feet;At Feet;Medium Skill;Default;Default;Default;Default;Default
WeaponSwitchTime=3.0
UseWeapons=true
CharacterProfile=Quaker-lowH
SeeThroughWalls=false
[Character Profile]
Name=Quaker Rail
MaxHealth=10.0
WeaponProfileNames=;;QC Railgun;;;;;
MinRespawnDelay=1.0
MaxRespawnDelay=1.0
StepUpHeight=175.0
CrouchHeightModifier=0.5
CrouchAnimationSpeed=1.0
CameraOffset=X=0.000 Y=0.000 Z=80.000
HeadshotOnly=false
DamageKnockbackFactor=6.0
MovementType=Base
MaxSpeed=2500.0
MaxCrouchSpeed=500.0
Acceleration=12000.0
AirAcceleration=16000.0
Friction=4.0
BrakingFrictionFactor=2.0
JumpVelocity=1200.0
Gravity=5.0
AirControl=0.25
CanCrouch=true
CanPogoJump=false
CanCrouchInAir=true
CanJumpFromCrouch=false
EnemyBodyColor=X=0.771 Y=0.000 Z=0.000
EnemyHeadColor=X=1.000 Y=1.000 Z=1.000
TeamBodyColor=X=1.000 Y=0.888 Z=0.000
TeamHeadColor=X=1.000 Y=1.000 Z=1.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=0.0
MainBBType=Cylindrical
MainBBHeight=300.0
MainBBRadius=50.0
MainBBHasHead=false
MainBBHeadRadius=45.0
MainBBHeadOffset=0.0
MainBBHide=false
ProjBBType=Cylindrical
ProjBBHeight=230.0
ProjBBRadius=55.0
ProjBBHasHead=false
ProjBBHeadRadius=45.0
ProjBBHeadOffset=0.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.2
JetpackFullFuelTime=4.0
JetpackFuelIncPerSec=1.0
JetpackFuelRegensInAir=false
JetpackThrust=6000.0
JetpackMaxZVelocity=400.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=false
AerialFriction=0.3
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=1.0
BlockedSpawnRadius=0.0
BlockSpawnFOV=0.0
BlockSpawnDistance=0.0
RespawnAnimationDuration=0.5
AllowBufferedJumps=true
BounceOffWalls=false
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=1.0
HealthRegainedonkill=600.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.0
[Character Profile]
Name=Quaker-lowH
MaxHealth=10.0
WeaponProfileNames=;;Railgun;;;;;
MinRespawnDelay=1.0
MaxRespawnDelay=1.0
StepUpHeight=75.0
CrouchHeightModifier=0.5
CrouchAnimationSpeed=2.0
CameraOffset=X=0.000 Y=0.000 Z=80.000
HeadshotOnly=false
DamageKnockbackFactor=4.0
MovementType=Base
MaxSpeed=1500.0
MaxCrouchSpeed=500.0
Acceleration=9000.0
AirAcceleration=16000.0
Friction=4.0
BrakingFrictionFactor=2.0
JumpVelocity=850.0
Gravity=3.0
AirControl=0.25
CanCrouch=true
CanPogoJump=false
CanCrouchInAir=true
CanJumpFromCrouch=false
EnemyBodyColor=X=0.771 Y=0.000 Z=0.000
EnemyHeadColor=X=1.000 Y=1.000 Z=1.000
TeamBodyColor=X=1.000 Y=0.888 Z=0.000
TeamHeadColor=X=1.000 Y=1.000 Z=1.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=0.0
MainBBType=Cylindrical
MainBBHeight=320.0
MainBBRadius=45.0
MainBBHasHead=false
MainBBHeadRadius=45.0
MainBBHeadOffset=0.0
MainBBHide=false
ProjBBType=Cylindrical
ProjBBHeight=230.0
ProjBBRadius=55.0
ProjBBHasHead=false
ProjBBHeadRadius=45.0
ProjBBHeadOffset=0.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.2
JetpackFullFuelTime=4.0
JetpackFuelIncPerSec=1.0
JetpackFuelRegensInAir=false
JetpackThrust=6000.0
JetpackMaxZVelocity=400.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=false
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=0.0
BlockSpawnFOV=0.0
BlockSpawnDistance=0.0
RespawnAnimationDuration=0.5
AllowBufferedJumps=true
BounceOffWalls=false
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=1.0
HealthRegainedonkill=0.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.0
[Dodge Profile]
Name=Circle Strafe
MaxTargetDistance=1245.901611
MinTargetDistance=373.770477
ToggleLeftRight=true
ToggleForwardBack=false
MinLRTimeChange=0.2
MaxLRTimeChange=0.5
MinFBTimeChange=0.2
MaxFBTimeChange=0.5
DamageReactionChangesDirection=true
DamageReactionChanceToIgnore=0.5
DamageReactionMinimumDelay=0.125
DamageReactionMaximumDelay=0.25
DamageReactionCooldown=1.0
DamageReactionThreshold=0.0
DamageReactionResetTimer=0.1
JumpFrequency=0.5
CrouchInAirFrequency=0.0
CrouchOnGroundFrequency=0.0
TargetStrafeOverride=Oppose
TargetStrafeMinDelay=0.125
TargetStrafeMaxDelay=0.25
MinProfileChangeTime=0.0
MaxProfileChangeTime=0.0
MinCrouchTime=0.3
MaxCrouchTime=0.6
MinJumpTime=0.3
MaxJumpTime=0.6
LeftStrafeTimeMult=1.0
RightStrafeTimeMult=1.0
StrafeSwapMinPause=0.0
StrafeSwapMaxPause=0.0
BlockedMovementPercent=0.5
BlockedMovementReactionMin=0.125
BlockedMovementReactionMax=0.2
[Dodge Profile]
Name=Short Strafes
MaxTargetDistance=2500.0
MinTargetDistance=750.0
ToggleLeftRight=true
ToggleForwardBack=false
MinLRTimeChange=0.2
MaxLRTimeChange=0.5
MinFBTimeChange=0.2
MaxFBTimeChange=0.5
DamageReactionChangesDirection=false
DamageReactionChanceToIgnore=0.5
DamageReactionMinimumDelay=0.125
DamageReactionMaximumDelay=0.25
DamageReactionCooldown=1.0
DamageReactionThreshold=50.0
DamageReactionResetTimer=0.5
JumpFrequency=0.2
CrouchInAirFrequency=0.0
CrouchOnGroundFrequency=0.0
TargetStrafeOverride=Ignore
TargetStrafeMinDelay=0.125
TargetStrafeMaxDelay=0.25
MinProfileChangeTime=0.0
MaxProfileChangeTime=0.0
MinCrouchTime=0.3
MaxCrouchTime=0.6
MinJumpTime=0.3
MaxJumpTime=0.6
LeftStrafeTimeMult=1.0
RightStrafeTimeMult=1.0
StrafeSwapMinPause=0.0
StrafeSwapMaxPause=0.0
BlockedMovementPercent=0.5
BlockedMovementReactionMin=0.125
BlockedMovementReactionMax=0.2
[Dodge Profile]
Name=Long Strafes NO Jump
MaxTargetDistance=100000.0
MinTargetDistance=0.0
ToggleLeftRight=true
ToggleForwardBack=false
MinLRTimeChange=0.5
MaxLRTimeChange=1.5
MinFBTimeChange=0.2
MaxFBTimeChange=0.5
DamageReactionChangesDirection=true
DamageReactionChanceToIgnore=0.5
DamageReactionMinimumDelay=0.125
DamageReactionMaximumDelay=0.25
DamageReactionCooldown=1.0
DamageReactionThreshold=50.0
DamageReactionResetTimer=0.5
JumpFrequency=0.0
CrouchInAirFrequency=0.0
CrouchOnGroundFrequency=0.0
TargetStrafeOverride=Ignore
TargetStrafeMinDelay=0.125
TargetStrafeMaxDelay=0.25
MinProfileChangeTime=0.0
MaxProfileChangeTime=0.0
MinCrouchTime=0.3
MaxCrouchTime=0.6
MinJumpTime=0.1
MaxJumpTime=0.1
LeftStrafeTimeMult=1.0
RightStrafeTimeMult=1.0
StrafeSwapMinPause=0.2
StrafeSwapMaxPause=0.5
BlockedMovementPercent=0.5
BlockedMovementReactionMin=0.125
BlockedMovementReactionMax=0.2
[Weapon Profile]
Name=QC Railgun
Type=Hitscan
ShotsPerClick=1
DamagePerShot=80.0
KnockbackFactor=9.0
TimeBetweenShots=1.4
Pierces=true
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=false
HeadshotMultiplier=2.0
MagazineMax=1
AmmoPerShot=1
ReloadTimeFromEmpty=1.4
ReloadTimeFromPartial=1.4
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=25.0
DelayBeforeShot=0.0
HitscanVisualEffect=Tracer
ProjectileGraphic=Ball
VisualLifetime=0.5
WallParticleEffect=Flare
HitParticleEffect=Blood
BounceOffWorld=false
BounceFactor=0.0
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=1.0
CanAimDownSight=true
ADSZoomDelay=0.0
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=9.0
RecoilNegatable=false
DecalType=1
DecalSize=30.0
DelayAfterShooting=0.0
BeamTracksCrosshair=true
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
ProjectileTrail=None
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=true
AimPunchAmount=0.0
AimPunchResetTime=0.05
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=true
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=1
CancelReloadOnKill=true
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
ADSScope=No Scope
ADSFOVOverride=72.099998
ADSFOVScale=Quake Champions
ADSAllowUserOverrideFOV=true
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=0.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,5.0
SpreadSCA=1.0,1.0,-1.0,5.0
SpreadMSA=1.0,1.0,-1.0,5.0
SpreadMCA=1.0,1.0,-1.0,5.0
SpreadSSH=1.0,1.0,-1.0,5.0
SpreadSCH=1.0,1.0,-1.0,5.0
SpreadMSH=1.0,1.0,-1.0,5.0
SpreadMCH=1.0,1.0,-1.0,5.0
MaxRecoilUp=0.0
MinRecoilUp=0.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=false
TimeToRecoilPeak=0.05
TimeToRecoilReset=0.35
AAMode=0
AAPreferClosestPlayer=false
AAAlpha=0.05
AAMaxSpeed=1.0
AADeadZone=0.0
AAFOV=30.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=true
TriggerBotDelay=0.01
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.095
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Weapon Profile]
Name=Railgun
Type=Hitscan
ShotsPerClick=1
DamagePerShot=80.0
KnockbackFactor=9.0
TimeBetweenShots=1.4
Pierces=true
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=false
HeadshotMultiplier=1.0
MagazineMax=0
AmmoPerShot=1
ReloadTimeFromEmpty=0.5
ReloadTimeFromPartial=0.5
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=25.0
DelayBeforeShot=0.0
HitscanVisualEffect=Tracer
ProjectileGraphic=Ball
VisualLifetime=0.5
WallParticleEffect=Gunshot
HitParticleEffect=Blood
BounceOffWorld=false
BounceFactor=0.0
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=1.0
CanAimDownSight=false
ADSZoomDelay=0.0
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=9.0
RecoilNegatable=false
DecalType=1
DecalSize=30.0
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
ProjectileTrail=None
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=true
AimPunchAmount=0.0
AimPunchResetTime=0.05
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=true
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=0
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
ADSScope=No Scope
ADSFOVOverride=72.099998
ADSFOVScale=Quake Champions
ADSAllowUserOverrideFOV=true
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=0.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,5.0
SpreadSCA=1.0,1.0,-1.0,5.0
SpreadMSA=1.0,1.0,-1.0,5.0
SpreadMCA=1.0,1.0,-1.0,5.0
SpreadSSH=1.0,1.0,-1.0,5.0
SpreadSCH=1.0,1.0,-1.0,5.0
SpreadMSH=1.0,1.0,-1.0,5.0
SpreadMCH=1.0,1.0,-1.0,5.0
MaxRecoilUp=0.0
MinRecoilUp=0.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=false
TimeToRecoilPeak=0.05
TimeToRecoilReset=0.35
AAMode=0
AAPreferClosestPlayer=false
AAAlpha=0.05
AAMaxSpeed=1.0
AADeadZone=0.0
AAFOV=30.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=true
TriggerBotDelay=0.01
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.095
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
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|
7ec527e87a80d4c2eaeb9689cd17fc9bf2ac46b8 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2354/CH5/EX5.5/5_5.sce | 51dc691fff061a7d0b56be4652875a4dfed2b204 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 326 | sce | 5_5.sce | //example 5.5
clc; funcprot(0);
// Initialization of Variable
A1=0.1;
V1=6.0;
V2=2.0;
delh=290.16-451.8;
p1=10^5;
Rbar=8314.0;
Qcvdot=-180.0/60;
M=28.97;//molecular mass
T1=290.0;
mdot=A1*V1*p1*M/Rbar/T1;
Wcvdot=Qcvdot+mdot*(delh+(V1^2/2-V2^2/2)/1000);
disp(Wcvdot,"heat transfer per unit time in kW")
clear()
|
80471e4fd58aeabe4a3cc84712a60d6d25e56176 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1094/CH2/EX2.3.2/EX2_3_2.sce | 3c59ebb74ce15bfe8687ae8fc9d37255347f9ece | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 293 | sce | EX2_3_2.sce | //Exa:2.3.2
clc;
clear;
close;
V_L=400 //supply voltage(in volts)
W_1=750 //power (in W)
W_2=250 //power (in W)
P_i=W_1+W_2
disp(P_i,'input power (in W)=')
pf=cosd(atand(sqrt(3)*(W_1-W_2)/(W_1+W_2)))
disp(pf,'power factor=')
I_L=P_i/(sqrt(3)*V_L*pf)
disp(I_L,'line current(in A)=') |
9994c12f4c79266f41c9546177685a84d8081936 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2072/CH22/EX22.5/Ex22_5.sce | 3cc1eeabbe1ee107595fccdc5402b673b484d69d | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 213 | sce | Ex22_5.sce | //Example 22.5
clc
x=699//in micrometer(w-a)
t=1200 //in micrometer
b=x/2
theta_2=atand(b/t)
disp(theta_2,"Angle in degree=")
y=sind(theta_2)
n1=1
n2=1.55
theta_1=asind((n2*y)/n1)
disp(theta_1,"Angle in degree=")
|
c6283a75a2616a003635010daff07df20b56fd07 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3311/CH6/EX6.22/Ex6_22.sce | 9b0f249d5012d4c445cb341b69cb84c30a707bb5 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,201 | sce | Ex6_22.sce | // chapter 6
// example 6.22
// Determine the minimum width of gate pulse
// page-345-346
clear;
clc;
// given
I_H=0.2; // in A (holding current)
td=2.5; // in us (delay time)
wt=%pi/3; // in radian (delay angle)
L1=8, L2=0; // in mH
R=2; // in ohm
E_line=208; // in V (line voltage)
f=50; // supply frequency
// calculate
L1=L1*1E-3;// changing unit from mH to H
td=td*1E-6;// changing unit from us to s
Ep=E_line/sqrt(3); // calculation of phase voltage
Em=Ep*sqrt(2); // calculation of peak voltage
e=sqrt(3)*Em*sin(wt+%pi/6);
di_dt_1=e/L1; // calculation of rate of rise of anode current when L=8 mH
// Since I_H=t1*(di_dt), therefore we get
t1=I_H/di_dt_1;// calculation of time required for anode current to rise to holding value when L=8 mH
tp1=t1+td; // calculation of minimum width of gate pulse when L=8 mH
//di_dt_2=e/L2; // rate of rise of anode current when L=0
t2=I_H/e*L2;// calculation of time required for anode current to rise to holding value when L=0
tp2=t2+td; // calculation of minimum width of gate pulse when L=0
printf("\nThe minimum width of gate pulse when L=8 mH is \t tp1=%.3f us",tp1*1E6);
printf("\nThe minimum width of gate pulse when L=0 H is \t tp2=%.1f us",tp2*1E6); |
5d3bae67b681ef918dc1c002c9beb094589b52f2 | 99b4e2e61348ee847a78faf6eee6d345fde36028 | /Toolbox Test/poly2rc/poly2rc4.sce | 08f0040c14b0dfc9c4259c64248d255928c8027b | [] | no_license | deecube/fosseetesting | ce66f691121021fa2f3474497397cded9d57658c | e353f1c03b0c0ef43abf44873e5e477b6adb6c7e | refs/heads/master | 2021-01-20T11:34:43.535019 | 2016-09-27T05:12:48 | 2016-09-27T05:12:48 | 59,456,386 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 146 | sce | poly2rc4.sce | //check o/p when the i/p is an empty vector
a=[];
efinal=0.2;
[b,E]=poly2rc(a,efinal);
disp(b);
disp(E);
////output
//
// []
//
// 0.2
|
4a730656f355195b6787ad6137fd6ab2b6d6c3b6 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1529/CH19/EX19.6/19_06.sce | 0d93b8c68a9b501a0c60e0320d648ff0509773c5 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 443 | sce | 19_06.sce | //Chapter 19, Problem 6, Fig.19.6
clc;
Av=40; //voltage gain
B=5000; //bandwidth
Ri=10000; //input resistance
A=10^(Av/20); //voltage gain in decibels
Rf=A*Ri; //feedback resistance
f=A*B; //frequency
printf("Gain = %d\n\nFeedback Resistor Rf = %d Megaohm\n\nFrequency = %d Khz",A,Rf/10^6,f/1000);
|
741bbc0b3b0c95422ce443d6cf138f471bffb239 | beca18778f40d44e713160c5b0e8136d8a92cad8 | /scilab/great-circle-small.sce | 55d0a82a32d1aeb8dd0610bd051d68701841e86b | [] | no_license | thomasantony/enjomitch-orbiter | 9542df3dfc83ce0a6cf06ec78dca91b4c1a0babf | 83967b7bf8f8c49d1e90f7b904846e66d1ad6e37 | refs/heads/master | 2022-12-02T07:47:03.976695 | 2020-03-22T13:54:57 | 2020-03-22T13:54:57 | 286,159,679 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 3,959 | sce | great-circle-small.sce | clear
r = 5;
offset = 0;
//offset = %pi/2;
// geographic coordinates
// 1 - starting point
// 2 - ending point
// latitude should be in range (-%pi/2, %pi/2)
// if displaying a satellite, lat1 is inclination
// divide the path into 2 steps - from 1 to 2 and from 2 to 3
// Increases precision greatly
lat1 = 10.57 * %pi / 180;
lat2 = 34 * %pi / 180;
// longitude should be in range (-%pi, %pi)
lon1 = 0 * %pi / 180;
lon2 = 50 * %pi / 180;
// converting to spherical coordinates
// theta should be in range of (0, %pi)
theta1 = lat1 + %pi/2;
theta2 = lat2 + %pi/2;
// phi should be in range of (0, %pi) (??)
phi1 = 0;
phi2 = lon2 - lon1;
// convert to cartesian coordinates
x1 = [0, r*sin(theta1)*cos(phi1)];
y1 = [0, r*sin(theta1)*sin(phi1)];
z1 = [0, r*cos(theta1)];
x2 = [0, r*sin(theta2)*cos(phi2)];
y2 = [0, r*sin(theta2)*sin(phi2)];
z2 = [0, r*cos(theta2)];
// create vectors for easy calculations
v1 = [x1(2), y1(2), z1(2)];
v2 = [x2(2), y2(2), z2(2)];
// actual path
vTheta12 = []; // 1st quart
vPhi12 = [];
// mirrored path
vPhi34 = [];
fixedStep = 0.04;
i = -fixedStep;
step = fixedStep;
// here, we'll be changing i from 0 to 1
// to properly scale a resulting vector below...
while (i <= 1 - step)
scf(0);
i = i + step;
// just a variable precision
//if i > 0.30 & i < 0.70
// step = fixedStep/2;
// else
// step = fixedStep;
// end
// the meatball equation of this approach:
// From v1, draw a vector to v2 and multiply it from 0 to 1
// so that we have many "straight line" points between p1 and 2
// on a plane defined by p1, p2 and origin of the planet (0,0,0)
v12 = v1 + i * (v2 - v1);
// check the length of the new point's vector
r12 = sqrt(v12(1)^2 + v12(2)^2 + v12(3)^2);
// make the vector as long as planet's radius
x121 = [0, v12(1)];
y121 = [0, v12(2)];
z121 = [0, v12(3)];
v12tmp = v12;
v12 = v12 * r / r12;
// rtest = sqrt(vtest(1)^2 + vtest(2)^2 + vtest(3)^2);
// for plotting
x12 = [0, v12(1)];
y12 = [0, v12(2)];
z12 = [0, v12(3)];
param3d(x12, y12, z12);
// param3d([v1(1) v2(1)], [v1(2) v2(2)], [v1(3) v2(3)]);
//param3d([v2(1) v3(1)], [v2(2) v3(2)], [v2(3) v3(3)]);
// convert to spherical
// r - already calculated
theta12 = acos(v12(3) / r);
phi12 = atan(v12(2) / v12(1));
// ensure proper range
if phi12 < 0
phi12 = phi12 + %pi;
end
// add new calculations to a vector
vTheta12 = [vTheta12, theta12];
vPhi12 = [vPhi12, phi12];
// mirror path (on the other side of planet)
phi34 = phi12 + %pi;
vPhi34 = [vPhi34, phi34];
end
// draw the final line with a different color
//plot2d(x12, y12);
param3d1(x12, y12, list(z12, [3,2]));
//param3d1(x23, y23, list(z23, [3,2]));
//vTheta = [vTheta, theta2];
//vPhi = [vPhi, phi2];
// convert back to geographical
vTheta12 = vTheta12 - %pi/2;
// use the initial longitude
vPhi12 = vPhi12 + lon1 + offset;
vPhi34 = vPhi34 + lon1 + offset;
// ensure proper ranges
s = size(vPhi12);
for i = 1:s(2)
if vPhi12(i) >= %pi
vPhi12(i) = vPhi12(i) - 2*%pi;
end
if vPhi34(i) >= %pi
vPhi34(i) = vPhi34(i) - 2*%pi;
end
end
scf(1);
// draw equator
plot2d([-%pi %pi], [0 0]);
// draw the actual trajectory from point 1 to 2
plot2d(vPhi12 , vTheta12, style=1, rect=[-%pi, -%pi/2, %pi, %pi/2]);
// draw mirror on the other side of planet
plot2d(vPhi34, -vTheta12, style=-2, rect=[-%pi, -%pi/2, %pi, %pi/2]);
// just a test of distance calculation
R = 6378;
d = acos( sin(lat1) * sin(lat2) + cos(lat1) * cos(lat2) * cos(lon2 - lon1) ) * R;
d = 2*asin(sqrt((sin((lat1-lat2)/2))^2 + cos(lat1)*cos(lat2)*(sin((lon1-lon2)/2))^2)) // equivalent but better
tc1=acos((sin(lat2)-sin(lat1)*cos(d))/(sin(d)*cos(lat1)));
if sin(lon2-lon1)<0 then
tc1 = 2*%pi - tc1;
else
end
|
92378f212d5fcb3fb02faa81c6b6449e633fb309 | d145a801b8f64afaf9dd0330b93936ca3343cbdb | /test_suite/td-syst-sort.tst | 62da407f676df7b79e41c0c09bee05be7344be40 | [] | no_license | ChemCryst/crystals | 0fff27ff8576b7c7199e1eaa671407d50132b98e | 8087c68d7f05b903473cee1cb131c06f819dc660 | refs/heads/master | 2023-08-17T16:36:03.675124 | 2023-06-26T10:54:29 | 2023-06-26T10:54:29 | 152,602,292 | 2 | 0 | null | 2023-06-26T10:54:30 | 2018-10-11T14:09:45 | Roff | UTF-8 | Scilab | false | false | 15,943 | tst | td-syst-sort.tst | #set time slow
#rele print CROUTPUT:
#TITLE Test SYST/SORT/MERGE
# Part 1 sets the FREIDEL pairs flag to NO in SYST, thus keeping
# the pairs separate independent of what was set in LIST 13
#
# After SORTing, the reflctions are first MERGED with TWIN set to YES,
# thus only merging FOT for reflections with identical ELEMENT flags. The
# data is still twinned and so needs a LIST 25 and a LIST 13 indicating twinning
#
# The data is then futher merged with TWIN=NO. This sets the ELEMENT flags to unity
# and merges FO, the de-twinned observed structure factors. Friedel pairs are still
# separate, so that there are 2 reflections in the final LIST 7.
#
# Part 2 sets the FRIEDEL flag to YES in SYST, thus applying Friedels law. SORT and MERGE
# are as before, but because Friedel pairs are transformed, there is only one reflection
# in the final LSIT 7
#
#
#LIST 1
REAL 7.5800 10.2880 12.0820 90.0000 108.3650 90.0000
END
#SPACE
symb P 21/C
END
#LIST 3
READ NSCATTERERS= 4
SCAT TYPE= C 0.003300 0.001600 2.310000 20.843920
CONT 1.020000 10.207509 1.588600 0.568700
CONT 0.865000 51.651241 0.215600
SCAT TYPE= H 0.000000 0.000000 0.493000 10.510910
CONT 0.322910 26.125732 0.140190 3.142360
CONT 0.040810 57.799770 0.003040
SCAT TYPE= CL 0.148400 0.158500 11.460400 0.010400
CONT 7.196400 1.166200 6.255600 18.519402
CONT 1.645500 47.778400 -9.557400
SCAT TYPE= N 0.006100 0.003300 12.212609 0.005700
CONT 3.132200 9.893311 2.012500 28.997540
CONT 1.166300 0.582600 -11.529010
END
#LIST 4
SCHEME 9 NPARAM= 0 TYPE=1/2FO
CONT WEIGHT= 2.0000000 MAX= 10000.0000 ROBUST=N
CONT DUNITZ=N TOLER= 6.0000 DS1= 1.0000
CONT DS2= 1.0000 QUASI= 0.2500
END
#
# Punched on 21/04/17 at 13:26:11
#
#LIST 5
READ NATOM = 22, NLAYER = 0, NELEMENT = 2, NBATCH = 0
OVERALL 4.719468 0.050000 0.050000 1.000000 0.000000 0.0000000
ATOM CL 1. 1.000000 0. 1.210669 0.671702 0.956236
CON U[11]= 0.029984 0.036835 0.026021 0.000261 0.012035 -0.000516
CON SPARE= 1.00 0 3 1 0
ATOM N 2. 1.000000 0. 0.707760 0.615560 0.692797
CON U[11]= 0.021537 0.026826 0.020818 0.000911 0.006855 -0.001468
CON SPARE= 1.00 0 3 2 0
ATOM C 3. 1.000000 0. 0.787799 0.538450 0.783300
CON U[11]= 0.028843 0.039354 0.025089 0.006118 0.010216 0.002082
CON SPARE= 1.00 0 3 2 0
ATOM N 4. 1.000000 0. 0.666798 0.518907 0.842160
CON U[11]= 0.030085 0.037029 0.026091 0.002806 0.011316 0.000092
CON SPARE= 1.00 0 3 2 0
ATOM C 5. 1.000000 0. 0.506065 0.587124 0.787878
CON U[11]= 0.025730 0.040344 0.026484 -0.004931 0.010213 -0.003974
CON SPARE= 1.00 0 3 2 0
ATOM C 6. 1.000000 0. 0.531432 0.647779 0.693724
CON U[11]= 0.026498 0.028320 0.025585 -0.003428 0.009244 -0.001256
CON SPARE= 1.00 0 3 2 0
ATOM C 7. 1.000000 0. 0.798141 0.665463 0.606984
CON U[11]= 0.026525 0.032726 0.022068 0.000275 0.009869 -0.004247
CON SPARE= 1.00 0 3 2 0
ATOM C 8. 1.000000 0. 0.807932 0.813725 0.619825
CON U[11]= 0.093643 0.035135 0.053699 -0.012074 0.044068 -0.031815
CON SPARE= 1.00 0 3 2 0
ATOM C 9. 1.000000 0. 0.675052 0.628352 0.483622
CON U[11]= 0.036485 0.049143 0.022806 -0.004232 0.010087 -0.006838
CON SPARE= 1.00 0 3 2 0
ATOM C 10. 1.000000 0. 0.991164 0.603140 0.633357
CON U[11]= 0.027342 0.102533 0.038446 0.018305 0.017252 0.013799
CON SPARE= 1.00 0 3 2 0
ATOM H 31. 1.000000 1. 0.915679 0.504396 0.802761
CON U[11]= 0.038362 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 51. 1.000000 1. 0.401523 0.591498 0.816523
CON U[11]= 0.037004 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 61. 1.000000 1. 0.447013 0.703554 0.638212
CON U[11]= 0.033570 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 83. 1.000000 1. 0.872611 0.851323 0.568457
CON U[11]= 0.084020 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 82. 1.000000 1. 0.874126 0.829437 0.701359
CON U[11]= 0.083920 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 81. 1.000000 1. 0.677373 0.844782 0.599535
CON U[11]= 0.085889 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 93. 1.000000 1. 0.730218 0.663223 0.427886
CON U[11]= 0.054073 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 92. 1.000000 1. 0.550037 0.667121 0.468814
CON U[11]= 0.055199 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 91. 1.000000 1. 0.669906 0.532894 0.476960
CON U[11]= 0.054728 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 103. 1.000000 1. 1.048166 0.640307 0.576401
CON U[11]= 0.081662 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 102. 1.000000 1. 1.061401 0.624756 0.713858
CON U[11]= 0.082273 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ATOM H 101. 1.000000 1. 0.974472 0.508693 0.621394
CON U[11]= 0.082814 0.000000 0.000000 0.000000 0.000000 0.000000
CON SPARE= 1.00 0 25165824 2 0
ELEMENTS 0.602762 0.397238
END
#
# Punched on 21/04/17 at 13:26:26
#
#LIST 12
BLOCK SCALE X'S U'S
SUMFIX ELEMENT SCALES
END
# Remove space after hash to activate next line
# USE LAST
#LIST 13
CRYST FRIEDELPAIRS=Y TWINNED=Y SPREAD=GAUSSIA
DIFFRACTION GEOMETRY=UNKNOWN RADIATION=XRAYS
CONDI WAVEL= 0.71073 6.050 90.000 0.5869359 0.6427007 0.0001788 90.000
MATR 0.000000000 0.000000000 0.000000000
CONT 0.000000000 0.000000000 0.000000000
CONT 0.000000000 0.000000000 0.000000000
END
#
# Punched on 21/04/17 at 13:26:36
#
#LIST 16
NO
REM HREST START (DO NOT REMOVE THIS LINE)
REM HREST END (DO NOT REMOVE THIS LINE)
END
# Remove space after hash to activate next line
# USE LAST
#LIST 23
MODIFY ANOM=N EXTI=N LAYER=N BATCH=N
CONT PARTI=N UPDA=N ENANT=N
MINIMI NSING= 0 F-SQ=Y RESTR=Y REFLEC=Y
ALLCYCLES U[MIN]= 0.00000000
CONT MIN-R= 0.000000 MAX-R= 100.000
CONT MIN-WR= 0.000000 MAX-WR= 100.000
CONT MIN-SUMSQ= 0.030000 MAX-SUMSQ= 10000.000
CONT MIN-MINFUNC= 0.000000 MAX-MINFUNC= 999999986991104.000
INTERCYCLE MIN-DR= -5.000000 MAX-DR= 100.000
CONT MIN-DWR= -5.000000 MAX-DWR= 100.000
CONT MIN-DSUMSQ=-10.000000 MAX-DSUMSQ= 10000.000
CONT MIN-DMINFUNC= 0.000000 MAX-DMINFUNC= 999999986991104.000
REFINE SPEC=CONSTRAIN UPDATE=PARAMETERS TOL= 0.60000
END
#LIST 25
READ NELEM= 2
MATRIX 1.000000000 0.000000000 0.000000000
CONT 0.000000000 1.000000000 0.000000000
CONT 0.000000000 0.000000000 1.000000000
MATRIX 1.000000000 0.000000000 0.000000000
CONT -0.000000000 -1.000000000 0.000000000
CONT -1.003999949 -0.000000000 -1.000000000
END
#LIST 28
READ NSLICE= 0 NOMIS= 0 NCOND= 0
MINIMA
CONT SINTH/L**2 = 0.01000
CONT RATIO = -3.00000
END
#LIST 29
READ NELEM= 4
# covalent,vdw,ionic,number,muA,weight,colour
ELEMENT C 0.7700 1.7800 0.0100 7.000 1.150 12.011 GREE
ELEMENT H 0.3200 1.3300 -0.3000 13.000 0.062 1.008 LGRE
ELEMENT CL 1.0800 2.0900 0.6000 1.000 67.800 35.453 BGRE
ELEMENT N 0.7700 1.7800 -0.1000 2.000 1.960 14.007 BLUE
END
#LIST 31
AMULT 0.00000100
MATRIX 1.21000 0.00000 0.00000 0.00000 0.00000 0.00000
CONT 3.24000 0.00000 0.00000 0.00000 0.00000
CONT 6.25000 0.00000 0.00000 0.00000
CONT 0.00000 0.00000 0.00000
CONT 0.00000 0.00000
CONT 0.00000
END
#LIST 39
OVERALL 0.00000000 0.00000000 0.00000000 0.00000000
CONT 0.00000000 0.00000000 0.00000000 0.00000000
CONT 0.00000000 0.00000000 0.00000000 0.00000000
READ NINT= 2 NREAL= 1
INT INFO 0 1 0 0 0 10
CONT 5 1 0 0 0
INT OVER 1 1 0 0 0 0
CONT 0 0 0 0 0
REAL SFLS 0. 1.000000 0.000000 0.000000 0.000000 0.000000
CONT 0.000000 0.000000 0.000000 0.000000 0.000000
END
#
#TITLE PART 1
#store unit ncpu 9
#LIST 7
READ NCOEF=13 TYPE=FIX, UNIT=DAT, CHECK=NO L30=NO ARCH=NO
STORE NCOEF=10
OUTPUT INDICES /FO/ SQRTW /FC/ BATCH/PHASE RATIO/JCODE
CONT SIGMA(/FO/) CORRECTIONS ELEMENTS /FOT/
INPUT H K L /FO/ SQRTW /FC/
CONT BATCH PHASE JCODE SIGMA(/FO/) CORRECTIONS ELEMENTS
CONT /FOT/
FOR (I4,I4,I4,F10.2,1X,G10.3,F10.2,F4.0,F6.2,F4.0,F8.2,F7.4,F8.0,F10.2)
END
1 -13 0 17.00 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 12. 17.00
1 -13 0 17.21 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 1. 17.20
1 -13 0 17.42 0.120E-01 3.23 1. -3.10 2. 1.57 1.0000 2. 17.40
1 -13 0 17.63 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 1. 17.60
1 13 0 18.68 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 12. 18.60
1 13 0 18.80 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 1. 18.80
1 13 0 19.01 0.120E-01 3.23 1. -3.10 2. 1.57 1.0000 2. 19.00
1 -13 0 17.84 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 12. 17.80
1 13 0 18.05 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 12. 18.00
1 13 0 18.26 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 1. 18.20
1 13 0 18.47 0.120E-01 3.23 1. -3.10 2. 1.57 1.0000 2. 18.40
-512
#purg
end
#punch 7 i
end
#syst 7 fried=no
end
#punch 7 i
end
#sort 7
end
#punch 7 i
end
#merge 7 twin=yes
ref list=hi
end
#punch 7 i
end
#merge 7 twin=no
ref list=hi
end
#punch 7 i
end
#TITLE PART 2
#LIST 7
READ NCOEF=13 TYPE=FIX, UNIT=DAT, CHECK=NO L30=NO ARCH=NO
STORE NCOEF=10
OUTPUT INDICES /FO/ SQRTW /FC/ BATCH/PHASE RATIO/JCODE
CONT SIGMA(/FO/) CORRECTIONS ELEMENTS /FOT/
INPUT H K L /FO/ SQRTW /FC/
CONT BATCH PHASE JCODE SIGMA(/FO/) CORRECTIONS ELEMENTS
CONT /FOT/
FOR (I4,I4,I4,F10.2,1X,G10.3,F10.2,F4.0,F6.2,F4.0,F8.2,F7.4,F8.0,F10.2)
END
1 -13 0 17.00 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 12. 17.00
1 -13 0 17.21 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 1. 17.20
1 -13 0 17.42 0.120E-01 3.23 1. -3.10 2. 1.57 1.0000 2. 17.40
1 -13 0 17.63 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 1. 17.60
1 13 0 18.68 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 12. 18.60
1 13 0 18.80 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 1. 18.80
1 13 0 19.01 0.120E-01 3.23 1. -3.10 2. 1.57 1.0000 2. 19.00
1 -13 0 17.84 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 12. 17.80
1 13 0 18.05 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 12. 18.00
1 13 0 18.26 0.120E-01 3.99 1. -3.10 2. 1.57 1.0000 1. 18.20
1 13 0 18.47 0.120E-01 3.23 1. -3.10 2. 1.57 1.0000 2. 18.40
-512
#purg
end
#use td-syst-sort.l7
#punch 7 i
end
#syst 7 fried=yes
end
#punch 7 i
end
#sort 7
end
#punch 7 i
end
#merge 7 twin=yes
ref list=hi
end
#punch 7 i
end
#merge 7 twin=no
ref list=hi
end
#punch 7 i
end
#end
|
38155072b712a5846f2e07cbe97ad85032098df3 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1922/CH4/EX4.23.b/4_23b.sce | 0b9d0622799b6047d24df84df382bc34deceff08 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 287 | sce | 4_23b.sce | clc
clear
//Initialization of variables
sd=6.7039//kJ/kg/K
sf=1.1453//kJ/kg/K
sg=7.5320//kJ/kg/K
hf=359.86//kJ/kg
hg=2653.5//kJ/kg
hd=3717.9//kJ/kg
//calculations
x=(sd-sg)/(sf-sg)
he=x*hf+(1-x)*hg
etar=(hd-he)/(hd-hf)
//results
printf("Thermal efficiency = %.4f",etar)
|
8bc01236e440ae3cd2a9318a5428cfa5ed5c4d30 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1592/CH9/EX9.6/example_9_6.sce | a52510e23e5073627c6080ad1f66cab1d37418fc | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 357 | sce | example_9_6.sce | //Scilab Code for Example 9.6 of Signals and systems by
//P.Ramakrishna Rao
clc;
clear;
A=1;
n=1;
wo=2*%pi;
theta=%pi/2;
for t=-5:0.01:5;
x(n)=A*cos(wo*t+theta);
n=n+1;
end
t=-5:0.01:5;
plot(t,x);
title('x(t)');
n=1;
for T=-5:0.1:5;
z(n)=(A^2/2)*cos(wo*T);
n=n+1;
end
figure(1);
T=-5:0.1:5;
plot(T,z);
title('Rxx(T)');
xlabel('t in seconds') |
d78c7fb4058eba219b570e9fe001bac49cdc73e8 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3750/CH1/EX1.10/Ex1_10.sce | f3cf4252a97cfad483f8820c20c8ef9d7ff0b12a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 2,442 | sce | Ex1_10.sce | //Strength Of Material By G.H.Ryder
//Chapter 1
//Example 10
//(a) To Calculate exiting stress in steel
//(b)To Calculate final stress in steel in steel if additional end trust is applied
clc();
//Initialization of variables
Ds=18; //Diameter of steel rod, Unit in mm
Dc=39; //Outside diameter of copper sleeve, Unit i mm
dc=24;//Inside diameter of copper sleeve, Unit in mm
EsbyEc=2;//Ratio of Young's modulus of steel to young's of copper
d=1.5//depth of copper removed, Unit in mm
//Computations
SigmaS1=10;//Tension stress set up in steel, Unit in N/mm^2
As=(%pi/4)*Ds^2; //Cross section Area of steel rod, Unit in mm^2
Ac=(%pi/4)*(Dc^2-dc^2); //Cross section Area of copper sleeve, Unit in mm^2
Acr=(%pi/4)*((Dc-2*d)^2-dc^2); //Area of reduce sectoin of copper, Unit in mm^2
SigmaC1=(As/Ac)*SigmaS1; //Stress set up in copper tube, Unit in N/mm^2
//(a)When tube reduced in area for half it's length
//Let SigmaC2 be stress in reduced secton in copper & SigmaCdash in the reminder
//Let SigmaS2 be stress in rod
//Equilibrium equation: Load on tube=Load on Rod
//SigmaC2*Acr=SigmaC2dash*Ac=SigmaS2*As
//SigmaC2=(As/Acr)*SigmaS2......(i)
//SigmaC2dash=(As/Ac)*SigmaC2.....(ii)
//Compatibility Equation: Reduction in lenght of rod=Reduction in length of tube
//(SigmaS1-SigmaS2)*l/Es=(SigmaC2-SigmaC1)*l/(2*Ec) + (SigmaC3dash-SigmaC1)*l/(2*Ec)
//Solving Equilibrium Equations and compatibility equation
SigmaS2=(SigmaS1+EsbyEc*SigmaC1)/(1+As*EsbyEc/(2*Acr)+As*EsbyEc/(2*Ac)); //Unit in N/mm^2 The answer vary due to round off error
//Result (a)
printf("The exiting stress in steel, SigmaS2= %.1fN/mm^2\n",SigmaS2)
//(b)An additonal end thrust of 5000N is applied
P=5000;//Additonal end thrust, Unit in N
//Let SigmaS3 And SigmaC3 be stresses in reduce section of steel and copper respectively
//Let SigmaC3dash be stress in remainder section of copper
//Equlibrium Equation:
//P=SigmaC3*Acr-SigmaS3*As
//SigmaC3=P/Acr+(As/Acr)*SigmaS3............(iii)
//SigmaC3dash=P/Ac+(As/Ac)*SigmaS3............(iv)
SigmaS3=(SigmaS1+EsbyEc*SigmaC1-(EsbyEc/2)*(P/Acr+P/Ac))/(1+EsbyEc*As/(2*Acr)+EsbyEc*As/(2*Ac)); //Unit in N/mm^2, The answer vary due to round off error
//Result (b)
printf("Final Stress in Steel,SigmaS3=%.1f N/mm^2",SigmaS3)
|
b1c44dbdbe5e922b541be9e93e7547d88ad9e13e | 449d555969bfd7befe906877abab098c6e63a0e8 | /1820/CH13/EX13.1/Example13_1.sce | d5d0d97ebdc8f62d0ba20501166ea3ed3c1fc409 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,486 | sce | Example13_1.sce | // ELECTRIC POWER TRANSMISSION SYSTEM ENGINEERING ANALYSIS AND DESIGN
// TURAN GONEN
// CRC PRESS
// SECOND EDITION
// CHAPTER : 13 : SAG AND TENSION ANALYSIS
// EXAMPLE : 13.1 :
clear ; clc ; close ; // Clear the work space and console
// GIVEN DATA
c = 1600 ; // Length of conductor in feet
L = 500 ; // span b/w conductors in ft
w1 = 4122 ; // Weight of conductor in lb/mi
// CALCULATIONS
// For case (a)
l = 2 * c *( sinh(L/(2*c)) ) ; // Length of conductor in ft using eq 13.6
l_1 = L * (1 + (L^2)/(24*c^2) ) ; // Length of conductor in ft using eq 13.8
// For case (b)
d = c*( cosh( L/(2*c) ) - 1 ) ; // sag in ft
// For case (c)
w = w1/5280 ; // Weight of conductor in lb/ft . [1 mile = 5280 feet]
T_max = w * (c + d) ; // Max conductor tension in lb
T_min = w * c ; // Min conductor tension in lb
// For case (d)
T = w * (L^2)/(8*d) ; // Appr value of tension in lb using parabolic method
// DISPLAY RESULTS
disp("EXAMPLE : 13.1 : SOLUTION :-") ;
printf("\n (a) Length of conductor using eq 13.6 , l = %.3f ft \n",l) ;
printf("\n & Length of conductor using eq 13.8 , l = %.4f ft \n",l_1) ;
printf("\n (b) Sag , d = %.1f ft \n",d) ;
printf("\n (c) Maximum value of conductor tension using catenary method , T_max = %.1f lb \n",T_max) ;
printf("\n Minimum value of conductor tension using catenary method , T_min = %.1f lb \n",T_min) ;
printf("\n (d) Approximate value of tension using parabolic method , T = %.2f lb \n",T) ;
|
fb17de503b5ec561479af6149877c9733a7b2b61 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1752/CH5/EX5.11/exa_5_11.sce | 04cec344201ab5b32c470778ab98092c4ce7c844 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 535 | sce | exa_5_11.sce | //Exa 5.11
clc;
clear;
close;
//given data
delta=15.68*10^-6;// in m^2/s
t_infinite=25+273;// in K
t_s=80+273;// in K
t_infinite=25+273;// in K
k=0.02625;// in W/m degree C
Pr=0.708;
miu_infinite=1.846*10^-5;//in kg/ms
miu_s= 2.076*10^-5;// in kg/ms
d=10*10^-3;// in m
V=5;// in m/s
A=4*%pi*(d/2)^2;
Re=V*d/delta;
Nu= 2+ (0.4*Re^(1/2)+0.06*Re^(2/3))*Pr^0.4*(miu_infinite/miu_s)^(1/4);
// Nu = h*d/k
h=Nu*k/d;// in W/m^2K
// heat transfer rate
q=h*A*(t_s-t_infinite);// in watt
disp(q,"Heat transfer rate in watt") |
f0a61e02f96c36e06ceaf3b7fd9930eb2f342830 | 3b9a879e67cbab4a5a4a5081e2e9c38b3e27a8cc | /Área 2/Aula 8 - Minimos quadráticos/MinimosQuadraticosPolinomioN.sce | ee3cc6e7260927e47e25ccb522036ff9f23f57f6 | [
"MIT"
] | permissive | JPedroSilveira/numerical-calculus-with-scilab | 32e04e9b1234a0a82275f86aa2d6416198fa6c81 | 190bc816dfaa73ec2efe289c34baf21191944a53 | refs/heads/master | 2023-05-10T22:39:02.550321 | 2021-05-11T17:17:09 | 2021-05-11T17:17:09 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 538 | sce | MinimosQuadraticosPolinomioN.sce | clear
x = (1:0.1:4)';
y = sin(20 + 1./x);
n = size(x,1);
p = 3;
for i=1:p+1
for j=1:p+1
/*Monta a matriz do elemento genérico polinomial*/
M(i,j) = sum(x.^(i+j-2));
end
end
for i = 1:p+1
/*Monta o vetor b do sistema*/
b(i) = sum(y.*x.^(i-1));
end
a = M\b;
XX = 1:0.5:12;
YY = a(1)+a(2).*XX+a(3).*XX.^2;
plot(XX,YY,'b');
plot(x,y,'r*');xgrid;
Xl = 2.1
resposta = a(1)+a(2)*Xl+a(3)*Xl^2+a(4)*Xl^3;
/*
residuo = 0;
for i=1:p+1
YY=YY+a(i)*XX.^(i-1);
residuo = residuo + a(i)*x.^(i-1);
end
*/
|
19bfa003b5f68ed1f91579b48632cff56c1f2be4 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1271/CH2/EX2.44/example2_44.sce | af7da1e7e87fccfaa5907b440d965d34f58c850a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 401 | sce | example2_44.sce | clc
// Given that
lambda = 5.5e-7 // wavelength of light in meter
theta = %pi / 6 // semi-angle of cone in radian
// Sample Problem 44 on page no. 2.55
printf("\n # PROBLEM 44 # \n")
d = (1.22 * lambda) / (2 * sin(theta)) // calculation for the resolving limit of microscope
printf("Standard formula used \n d*sin(theta)= 1.22*lamda. \n")
printf("\n The resolving limit of microscope = %e meter",d)
|
1f62bca460e0ff462ad6cd78151a1ff06c453043 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3204/CH8/EX8.5/Ex8_5.sce | ef37ead7ebf35b3297553e70739e7172f0509080 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 848 | sce | Ex8_5.sce | // Initilization of variables
W=2000 //N // Load to be raised
l=0.70 //m // length of the handle
d=0.05 //m // diameter of the screw
p=0.01 //m // pitch of the screw
mu=0.15 // coefficient of friction at the screw thread
pie=3.14 //constant
E=1 // efficiency
// Calculations
phi=atand(mu) //degree
theta=atand(p/(pie*d)) //degree // where theta is the Helix angle
// Force required at the circumference of the screw is,
P=W*tand(theta+phi) // N //
// Force required at the end of the handle is,
F=(P*(d/2))/l //N
// Force required (Ideal case)
V.R=2*pie*l/p
M.A=E*V.R // from formulae E=M.A/V,R
P_ideal=W/M.A //N // From formulae, M.A=W/P
// Results
clc
printf('The force required at the end of the handle is %f N \n',F)
printf('The force required if the screw jack is considered to be an ideal machine is %f N \n',P_ideal)
|
8a02a410265e58e412836d3608a31823784eb3d6 | 449d555969bfd7befe906877abab098c6e63a0e8 | /629/CH7/EX7.5/example7_5.sce | 2b7f2344fc50fcdda07eab6c6289e6f9e6176534 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 686 | sce | example7_5.sce | clear
clc
//Example 7.5 FORCE ON A CONTRACTION IN A PIPE
D1=0.3; //[m]
D2=0.2; //[m]
A1=%pi*D1^2/4 //area[m^2]
A2=%pi*D2^2/4 //area[m^2]
Q=0.707; //rate of flow[m^3/s]
V1=Q/A1; //velocity[m/s]
V2=Q/A2; //velocity[m/s]
ht=0;
hp=0;
hL=2.58; //[m]
alpha1=1;
alpha2=1;
rho=1000; //density[kg/m^3]
Gamma=9810; //specific weight[N/m^3]
g=9.81; //[m/s^2]
p1=250000; //pressure[Pa]
p2=p1+Gamma*(hp-ht-hL-(alpha2*V2^2-alpha1*V1^2)/(2*g)) //pressure at L[Pa]
//Momentum equation
//p1*A1-p2*A2+Fx=m*V2-m*V1, m=rho*Q
Fx=(rho*Q*(V2-V1)+p2*A2-p1*A1)/10^3 //force[kN]
printf("\nThe horizontal force required to hold the transition in place = %.2f kN,in -ve x direction.\n",-Fx) |
0b0480fabef04d9c8625a637f52e010992746817 | 449d555969bfd7befe906877abab098c6e63a0e8 | /680/CH5/EX5.11/5_11.sce | ebfd57fdb735ff94e9b57e48797327f4de57b23c | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 324 | sce | 5_11.sce | //Problem 5.11:
//initializing the variables:
wr = 5; // in ton/hr
pcl = 0.02
x = 2000
MWHCl = 36.5
MWCl = 35.5
y = 0.99
//calculation:
Clfeed = wr*pcl*x
HCl = Clfeed*MWHCl/MWCl
maxrate = HCl*(1-y)
printf("\n\nResult\n\n")
printf("\n maximum permissible mass emission rate of HCl = %.2f lb HCl/h",maxrate) |
c0f8bbd28405d8cf4392931670ce45231b982654 | 449d555969bfd7befe906877abab098c6e63a0e8 | /431/CH4/EX4.3/EX4_3.sce | 87f807e18654a6f674d245f8707af87a9323bd3a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 753 | sce | EX4_3.sce | //Calculating synchronous speed and speed of a rotor
//Chapter 4
//Example 4.3
//page 289
clear;
clc;
disp("example 4.3");
disp("induction motor is to be run at 1440 rpm")
P=10; //poles of alternator
N=600; //speed of alternator
f=(P*N)/120 //frequency
printf("frequency=%d",f);
disp("when P=2");p=2
Ns=(120*f)/p; //synchronous speed
printf("Syhchronous speed,Ns=%d \n",Ns);
disp("when P=4");p=4;
Ns=(120*f)/p; //synchronous speed
printf("Syhchronous speed,Ns=%d \n",Ns);
//speed of rotor(1440) is less than synchronous speed 1500, therefore P=4
disp("speed of rotor(1440) is less than synchronous speed 1500, therefore P=4\n")
Ns=1500;
Nr=1440;
S=((Ns-Nr)/Ns)*100
printf("\nslip is %d percent and number of poles is 4",S) |
363ab357c6b656ed8eda716e1e916f9fdf9d3d64 | 449d555969bfd7befe906877abab098c6e63a0e8 | /257/CH5/EX5.17/example_5_17.sce | f79ff5d459cec723adf7a5e808a2f78526baf06a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 333 | sce | example_5_17.sce | syms Ro Ra Rb Rc Rd
//shifting summing points to left of 1/Ra and 1/Rb and combining the summing points
a=((1/Ra)*Rc)/(1+(1/Ra)*Rc*1)
b=(Rd/Rb)/(1+(Rd/Rb))
//shift input summing points to the right and combine the three summing points
c=(1/Ro)/(1+(1/Ro)*(Ra*Rc/(Ra+Rc)))
d=c/(1-(b*Rb*c))
e=a-b
Y=e*d
disp(Y,"Io/Vi = ") |
99f38e37599f4392986f6bfedc924b360e7088d3 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2411/CH8/EX8.2/Ex8_2.sce | 39158fbd1043a9d29b836a54a8a054ff734bf104 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 524 | sce | Ex8_2.sce | // Scilab Code Ex8.2: Page-398 (2008)
clc; clear;
lambda = 632.8e-009; // Wavelength of the lase beam, cm
E_2P = 15.2e-019; // Energy of 2P level, J
h = 6.626e-034; // Planck's constant, Js
c = 3e+008; // Speed of light, m/s
e = 1.6e-019; // Energy equivalent of 1 eV, J/eV
E_Pump = E_2P + h*c/lambda; // The required pumping energy, J
printf("\nThe pumping energy required for He Ne laser transition = %5.2f eV", E_Pump/e);
// Result
// The pumping energy required for He Ne laser transition = 11.46 eV
|
1302dbe31612a1c32ad87dea3850107f8be752e4 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1943/CH7/EX7.8/Ex7_8.sce | bf6c2ce357b454576f6adae7d4bffa56677aeed1 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,052 | sce | Ex7_8.sce |
clc
clear
//Input data
p1=5//Pressure in bar
T1=200//Temperature in degree C
p2=2//Pressure in bar
m=0.3//Mass flow rate in kg/s
n=1.3//Adiabatic index
nn=0.92//Nozzle efficiency
cp=1.925//mean specific heat in kJ/kg.K
x=[2.308,1943]//pv*10^3 = 2.308(h-1943)
//Calculations
vo=0.4249//Specific volume in m^3/kg
ho=2855.4//Enthalpy in kJ/kg
so=7.0592//Entropy in kJ/kg.K
x1=0.972//Dryness fraction
h1=(504.7+x1*2201.9)//Enthalpy in kJ/kg
v1=x1*0.8857//Specific volume in m^3/kg
V1=44.72*sqrt(ho-h1)//Velocity in m/s
h=ho-h1//Change in enthalpy in kJ/kg
hoq=nn*h//Change in enthalpy in kJ/kg
VQ=44.72*sqrt(hoq)//Velocity in m/s
toq=(hoq/cp)//Temperature difference in degree C
tQ=(T1-toq)//Temperature in degree C
TQ=tQ+273//Temperature in K
vQ=((p1*100*vo)/(T1+273))*(TQ/T1)//Specific volume in m^3/kg
A1=((m*vQ)/VQ)*10^6//Area in mm^2
vQ=(x(1)*(ho-hoq-x(2)))/(10^3*p2)//Specific volume in m^3/kg
A11=((m*vQ)/VQ)*10^6//Area in mm^2
//Output
printf('Exit area is %3.1f mm^2 which upon checking is %3.0f mm^2',A1,A11)
|
f78cf88eccde70dcb98b13b09d78d6a127e894ff | 24fb1e72f2244733455f40fda1ae95423110e82a | /lab1.sce | e2695b5523eec752c5b4f0ef47f7d52b084f5c0f | [] | no_license | Aie-Aie/scilab | a4cbed5b58134009de1c084950a45da1e2b6f2db | 616568e7589f61dcda425410fbedc943b238f11b | refs/heads/master | 2021-09-11T20:42:55.522610 | 2018-04-12T05:29:52 | 2018-04-12T05:29:52 | 106,638,444 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 143 | sce | lab1.sce | disp("Hello Philippines and Hello World!")
printf("Hello world")
data="Aspe Ailen Grace T."
string(data)
disp(data)
x="b"
y="a"
v="Hello"
|
6ff7e246d5df7da931d2c856d69b818afa8992ab | abdfb2db73e5240261372a514baa0c1a7bed7467 | /cudd-3.0.0/nanotrav/ham01.tst | 34680bb7c6278585f334e6cda82bf1739ea432e4 | [] | no_license | steefbrown/ece6740 | 21001ca156e24e23b71d6b719f11010ba4ce2a40 | cefe8dd498c7849546ece98fbd4d70b844f2bd5c | refs/heads/master | 2021-01-01T05:23:01.008122 | 2016-05-09T19:16:56 | 2016-05-09T19:16:56 | 57,227,414 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 137 | tst | ham01.tst | # Nanotrav Version #0.12, Release date 2003/12/31
# nanotrav/nanotrav -p 1 -reordering linear ./nanotrav/ham01.blif
# CUDD Version 3.0.0
|
dd10efc17b5259936c42064a187b94e18c74d233 | 449d555969bfd7befe906877abab098c6e63a0e8 | /569/CH5/EX5.6/5_6.sci | f928b21325782c1da6b8fae8b24d52cc839b8430 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 164 | sci | 5_6.sci | //Calculating the output voltage
clc;
RAB=125;
Rtotal=5000;
R2=75/125*Rtotal;
R4=2500;
ei=5;
eo=[(R2/Rtotal)-(R4/Rtotal)]*ei;
disp(eo,'output voltage (V)=') |
2c5ae3d0c2421591b9383be648851a69544b0ac1 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3020/CH17/EX17.9/ex17_9.sce | 5f7ccb215e58d8933b130459cba5d971a44f28bd | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 272 | sce | ex17_9.sce | clc;
clear all;
h=6.626e-34;//planck's constant
m=9.1e-31;//mass of electron
n=18.1e28;//electron density of aluminium
Efo=(h*h/(2*m))*((3*n/(8*%pi))^(2/3));//fermi energy at 0K
Efo1=Efo/(1.6e-19);//conversion into eV from J
disp('eV',Efo1,'fermi energy at 0 K');
|
f1a1339c176f856031b1d35317eeb741542cc6a0 | 717ddeb7e700373742c617a95e25a2376565112c | /278/CH3/EX3.4/ex_3_4.sce | a401781bdd422bf1364f9098a6ebae232d27cf05 | [] | no_license | appucrossroads/Scilab-TBC-Uploads | b7ce9a8665d6253926fa8cc0989cda3c0db8e63d | 1d1c6f68fe7afb15ea12fd38492ec171491f8ce7 | refs/heads/master | 2021-01-22T04:15:15.512674 | 2017-09-19T11:51:56 | 2017-09-19T11:51:56 | 92,444,732 | 0 | 0 | null | 2017-05-25T21:09:20 | 2017-05-25T21:09:19 | null | UTF-8 | Scilab | false | false | 593 | sce | ex_3_4.sce | //find limits of shaft and bearing and maximum and minimum clearance
clc
//solution
//given
//75 mm basic size
//since 75 lies betweenn 50 and 80
D=sqrt(50*80)//mm
i=0.45*(D)^0.33+0.001*D//standard tolerance unit
IT8=25*i*0.001//mm
IT7=16*i*0.001//mm
es=-2.5*(D)^0.34//mm//upper deviation of shaft
ei=es-IT7//mm//lower deviation fot hole
bs=75//mm//basic size
uh=75+IT8//upper limit of hole
us=75-0.01//mm//upper limit of shft
ls=us-0.03//mm
MxC=uh-ls//mm//maximum clearance
miC=75-us//mm
printf("maximum clearance is,%f mm\n",MxC)
printf("minimum clearance is,%f mm",miC) |
1e29292ed087678078456439b1dc1c8e81806d06 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1301/CH26/EX27.7/ex27_7.sce | 2a8f51e3dd22c3a7464af3e08b68874125b97d36 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 52 | sce | ex27_7.sce | clc;
disp(0.075*111,"Mass = "); //displaying result |
608ac46e6d9dc885ed0cfd1e8077cdcb8fd079a5 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2990/CH6/EX6.13/Ex6_13.sce | a03a6ed1784191c88fc5b431c82c5aaa68f7ad01 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 822 | sce | Ex6_13.sce |
clc; funcprot(0);
// Initialization of Variable
t=3*%pi/180;//tilt
xa=-62.45;//x coordinate of a
xb=78.25;//x coorbinate of b
f=152.4;//focal length in mm
H=2500.0;//actual height in m
hb=800;//height B in m
ha=500.0;//height A in m
ya=82.25;//y coordinate of a
yb=-41.15;//y coordinate of b
s=220.0;
//calculation
theta=s-180;
ya1=xa*sin(theta*%pi/180)+ya*cos(theta*%pi/180)+f*tan(t);//ya'
xa1=xa*cos(theta*%pi/180)-ya*sin(theta*%pi/180);//xa'
xb1=xb*cos(theta*%pi/180)-yb*sin(theta*%pi/180);//xb'
yb1=xb*sin(theta*%pi/180)+yb*cos(theta*%pi/180)+f*tan(t);//yb'
Xa=xa1*(H-ha)/(f/cos(t)-ya1*sin(t));
Xb=xb1*(H-hb)/(f/cos(t)-yb1*sin(t));
Ya=ya1*cos(t)*(H-ha)/(f/cos(t)-ya1*sin(t));
Yb=yb1*cos(t)*(H-hb)/(f/cos(t)-yb1*sin(t));
AB=sqrt((Xb-Xa)**2+(Yb-Ya)**2);
disp(AB,"distance of AB in m")
clear()
|
b401210c3db5fd9968a00c45ec95f6d4ec532c03 | 449d555969bfd7befe906877abab098c6e63a0e8 | /764/CH7/EX7.6.a/data7_6.sci | c8264780cedc9694dc378d32b58a69185612dc89 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 350 | sci | data7_6.sci |
//(Threaded Joints) Example 7.6
//Refer Fig.7.21 on page 237
//Number of bolts N
N = 4
//Allowable tensile stress in the bolts sigmaMax (N/mm2)
sigmaMax = 35
//Load acting on the bracket P (kN)
P = 25
//Eccentricity value e (mm)
e = 500
//Height of bolt1 from the base l1 (mm)
l1 = 550
//Height of bolt2 from the base l2 (mm)
l2 = 50
|
eaaa8e80f611b3b5946f9370df95f542d7e206aa | 1489f5f3f467ff75c3223c5c1defb60ccb55df3d | /tests/test_diff_1_i.tst | 13a88a80afe6a8d8cbc2bbf8a9d4b154aed64b51 | [
"MIT"
] | permissive | ciyam/ciyam | 8e078673340b43f04e7b0d6ac81740b6cf3d78d0 | 935df95387fb140487d2e0053fabf612b0d3f9e2 | refs/heads/master | 2023-08-31T11:03:25.835641 | 2023-08-31T04:31:22 | 2023-08-31T04:31:22 | 3,124,021 | 18 | 16 | null | 2017-01-28T16:22:57 | 2012-01-07T10:55:14 | C++ | UTF-8 | Scilab | false | false | 16 | tst | test_diff_1_i.tst | d3 3
a7 2
x0
x1
|
d3757e5ed3f3793e57006470baada4779f946a23 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3760/CH6/EX6.62/Ex6_62.sce | d5a1a4b77c2346a7966707f8d87a9ee73112b629 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 452 | sce | Ex6_62.sce | clc;
s=0.03; // full load slip
R=0.015; // rotor resistance per phase
n=4; // number of step in starter
al=s^(1/n);
R1=R/s; // resistance of whole section
r1=R1*(1-al);
printf('Resistance of first element is %f ohms\n',r1);
r2=r1*al;
printf('Resistance of second element is %f ohms\n',r2);
r3=r1*al^2;
printf('Resistance of third element is %f ohms\n',r3);
r4=r1*al^3;
printf('Resistance of fourth element is %f ohms\n',r4);
|
a21bbf339cbee04f23b259b30ca9670a06b3a577 | 449d555969bfd7befe906877abab098c6e63a0e8 | /69/CH9/EX9.3/9_3.sce | 2ac41c126371aefedf97cf900a9a02ed5a8f561b | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 95 | sce | 9_3.sce | clear; clc; close;
disp(10^1.6,'ans for part a :- ');
disp(%e^0.04,'ans for part b :- ');
|
7a71ec0852934fca4773a66b7c701cb1b17d1844 | af301357b0dfd5c5ca0825378008dd7924e7d5db | /IntegraçãoTodosMetodos.sce | 39d22371f40709cd825fb3cf514236401e82ba8b | [] | no_license | fonte-nele/Metodos-Numerico-Scilab | c544f1a9951f33708f62bdee38a7cddf7699625b | 62a2be7afb3a1f7901bc5f005500475f52f2caae | refs/heads/master | 2020-06-10T11:31:42.291337 | 2019-07-03T18:10:03 | 2019-07-03T18:10:03 | 193,640,719 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 1,558 | sce | IntegraçãoTodosMetodos.sce | clc; clear;
function [y]=f(x);
y = 0.5*x^2 - 0.15*x; // Função da Integral
endfunction;
a = 1.5 // Limite inferior integração
b = 7.5 // Limite superior integração
m = 6 // Quantidade de intervalos
h = (b-a)/m
// Regra dos Trapézios
xi = a
soma = f(xi) // Soma da multiplicação dos coeficientes com o valor de f(x)
xi = a + h
for i = 2:m
soma = soma + 2*f(xi) // Elementos do meio multiplicado por 2
xi = xi + h
end
soma = soma + f(xi) // Último multiplicado por 1
I = (h/2) * soma // Fórmula Regra dos Trapézios
printf("\nO valor da integral pela Regra dos Trapézios eh %.6f \n", I)
// 1º Regra de Simpson
xi = a
soma = f(xi) // Multiplica por 1
xi = a + h
for i = 2:m
if modulo(i, 2) == 0 then
soma = soma + (4 * f(xi)) // Se for par multiplica por 4
else
soma = soma + (2 * f(xi)) // Se for ímpar multiplica por 2
end
xi = xi + h
end
soma = soma + f(xi) // Multiplica por 1
I = (h / 3) * soma // Fórmula 1º Regra de Simpson
printf("\nO valor da integral pela 1º Regra de Simpson eh %.6f \n", I)
// 2º Regra de Simpson
xi = a
soma = f(xi)
xi = a + h
aux = 1
for i = 2:m
if aux == 3 then
soma = soma + (2 * f(xi)) // Intermediários = multiplica por 2
aux = 1
else
soma = soma + (3 * f(xi)) // Intermediários = multiplica por 3
aux = aux + 1
end
xi = xi + h
end
soma = soma + f(xi) // Multiplica por 1
I = (3 * h / 8) * soma// Fórmula 2º Regra de Simpson
printf("\nO valor da integral pela 2º Regra de Simpson eh %.6f \n", I)
|
49cac19b8a666fe539cb0c3e5979efe1e7a61d3b | 449d555969bfd7befe906877abab098c6e63a0e8 | /2777/CH4/EX4.4/Ex4_4.sce | 104c1364d40f8ca4ce703ec320719a39d4b7d6e5 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 899 | sce | Ex4_4.sce |
// ELECTRICAL MACHINES
// R.K.Srivastava
// First Impression 2011
// CENGAGE LEARNING INDIA PVT. LTD
// CHAPTER : 4 : DIRECT CURRENT MACHINES
// EXAMPLE : 4.4
clear ; clc ; close ; // Clear the work space and console
// GIVEN DATA
L = 0.3; // Length of the Machine in Meter
Ia = 10; // Current through The Conductors in Ampheres
N = 10; // Number of the Conductors in each Slot
Za = 24; // Number of the Slots
Bav = 0.6; // Average Flux Density in Telsa
D = 0.1; // Machine Daimeter in Meter
// CALCULATIONS
F = N*Ia*Bav*L; // Force due to the Single Slot in Newton
T = (Bav*L*Ia*N*D*Za)/2 // Torque produced in the Machine in Newton-Meter
// DISPLAY RESULTS
disp("EXAMPLE : 4.4 : SOLUTION :-") ;
printf("\n (a) Torque produced in the Machine, T = %.1f N-m \n",T);
|
a9e20f46fd7b3f894e9ff58867999f52efa92ef5 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2777/CH5/EX5.22/Ex5_22.sce | 6103f5fbedfac7b8641ec377a2f313f708d59097 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 4,518 | sce | Ex5_22.sce |
// ELECTRICAL MACHINES
// R.K.Srivastava
// First Impression 2011
// CENGAGE LEARNING INDIA PVT. LTD
// CHAPTER : 5 : INDUCTION MACHINES
// EXAMPLE : 5.22
clear ; clc ; close ; // Clear the work space and console
// GIVEN DATA
Wsc = 1000; // Power at Blocked Rotor test in Watts
Vsc = 56; // Voltage at Blocked Rotor test in Volts
Isc = 18; // Current at Blocked Rotor test in Amphere
Woc = 52; // Power at No-load test in Watts
Voc = 220; // Voltage at No-load test in Volts
Ioc = 2.6; // Current at No-load test in Amphere
m = 3; // Total Number of phase in Induction Motor
p = 4; // Total number of Poles of Induction Motor
V = 220; // Operating voltage of the Induction motor in Volts
f = 50; // Frequency in Hertz
s = 0.05; // Slip
R = 0.65; // Per phase stator Resistance in Ohms
// CALCULATIONS
Vph = Voc/sqrt(3); // Per phase Voltage in Volts
Wo = Woc/m; // Per phase No-load loss in Watts
theta_0 = acosd(Wo/(Voc*Ioc*sqrt(3))); // No-load power factor angle in degree
VSC = Vsc/sqrt(3); // Per phase locked rotor Voltage in Volts
WSC = Wsc/m; // Per phase locked rotor loss in Watts
theta_sc = acosd(WSC/(VSC*Isc)); // No-load power factor angle in degree
ISC = Isc*(Voc/Vsc); // locked rotor current at full Voltage in Amphere
Re = WSC/Isc^2; // Resistance in Ohms
R1 = R*1.1; // Per phase AC stator Resistance in Ohms
R_2 = Re - R1; // Per phase rotor Resistance in Ohms
Zsc = VSC/Isc; // Per phase impedance in Ohms
Xs = sqrt((Zsc^2)-(Re^2)); // Leakage Reactance in Ohms
I_2 = (Voc/sqrt(3))/sqrt((R1+(R_2/s))^2+(Xs^2)); // Current in Amphere
pf = cosd(atand(Xs/(R1+(R_2/s)))); // Power Factor
Ws = 2*%pi*((120*f/p)*(1/60)); // Rotational Speed in Radians per Seconds
Pg = (3*(abs(I_2)^2*R_2))/s; // 3-phase air gap power or Rotor intake Power in Watts
T = Pg/Ws; // Torque in Newton-Meter
// CALCULATIONS OR DATA OBTAINED FROM CIRCLE DIAGRAM FIGURE 5.35 and PAGE NO:-303
OA = 2.60; // Correspounding Current in Amphere at 87' from Y-axis (from Circle diagram)
OE = 70.70; // Correspounding Current in Amphere at 55' from Y-axis (from Circle diagram)
OP = 17.77; // Current in Amphere (from Circle diagram)
OV = Voc/sqrt(3); // Phase Voltage in No-load test or value obatined from circle diagram in Volts
PK = 11.6; // Correspounding Value from Circle diagram
JK = 0.8; // Correspounding Value from Circle diagram
PJ = 10.8; // Correspounding Value from Circle diagram
PM = 11.6; // Correspounding Value from Circle diagram
Pir = 3*OV*PK; // Total Rotor intake in Watts
Plr = 3*OV*JK; // Total Rotor loss in Watts
Po = 3*OV*PJ; // Total Mechanical power output in Watts
T_c = (3*OV*PK)/Ws; // Total Torque in Newton-Meter
s_c = JK/PK; // Slip obtained from Circle diagram
s_pc = 100*s_c; // Slip in percentage
eta = 100*(PJ/PM); // Eifficiency in Percentage
// DISPLAY RESULTS
disp("EXAMPLE : 5.22 : SOLUTION :-");
printf("\n (a) Input line current, I2 = %.2f A \n",I_2)
printf("\n (b) Power Factor, Pf = %.3f \n",pf)
printf("\n (c) Torque, T = %.2f Nm \n",T)
printf(" \n Verification Results from Circle Diagram :-\n");
printf("\n (a) Efficency, eta = %.2f Percent \n",eta)
printf("\n (b) slip, s = %.3f = %.f percent \n",s_c,s_pc)
printf("\n (c) Torque, T = %.2f Nm \n",T_c)
|
e10284091c7c06cf7d8b98d09c2e26ce3595144e | 449d555969bfd7befe906877abab098c6e63a0e8 | /1442/CH13/EX13.7/13_7.sce | 0e78f8770a889d8f89e0911cc4470ea87c824805 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 508 | sce | 13_7.sce | clc
//initialisation of variables
vi= 0.0009992 //m^3
T= 60 //C
T1= 20 //C
T2= 40 //C
vi1= 0.0010042 //m^3
vi2= 0.0009886 //m^3
v= 0.000951 //m^3
v1= 0.0009992 //m^3
v2= 0.0009956 //m^3
//CALCULATIONS
B= (vi1-vi2)/(vi*(T-T1))
Kt= (v1-v2)/(v*(T2-T1))
Et= 1/Kt
//RESULTS
printf (' volume exapansion coefficient= %.2e L/s',B)
printf (' \n isothermal compressibility= %.3e Mpa',Kt)
printf (' \n isothermal modulus of elasticity= %.f Mpa',Et)
//ANSWER FOR Et GIVEN IN THE TEXTBOO IS WRONG
|
fc066db4d899355fe62e71aa929fd0c8f13a598f | fcc4645d4eee021a4cf8b2cee0922d812710573f | /perf/prelim_design.sce | 3d07cfcba630cb341075477d6aeea78de735d0c6 | [] | no_license | gviolato/nemo | 656a6db0481d9828bff307de24ee0b92045d653f | 44cf1554de9e1c4bc8450ae147bdec512599e0d9 | refs/heads/master | 2020-12-29T02:37:17.515209 | 2017-05-28T16:12:49 | 2017-05-28T16:12:49 | 43,207,682 | 2 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 9,338 | sce | prelim_design.sce | // HPH preliminary design script
//
// Based on article "The 20-knot human-powered water craft" - Alec Brooks
// "Human Power" Magazine, Spring 1987, Vol6 N.1 - p.1
//
// Diego Montero; Gustavo Violato; Fernando Valentini
// First release: Sep. 2015
clc
xdel(winsid())
clear
// Script flags
DO_CALC=1;
DO_PLOTS=1;
// Fixed variables
GRAV = 9.80665; // gravity [m/s^2]
FT2M = 0.3048; // feet to meter
// Riders parameters
gustavo.mass = 87;
gustavo.pwr = 250;
gustavo.name = "Gustavo";
fernando.mass = 88;
fernando.pwr = 250;
fernando.name = "Valentini";
diego.mass = 72;
diego.pwr = 275;
diego.name = "Diego";
// Chosen wing dimensions
prj_span = 1.8; // [m]
prj_aspect = 17; // [m]
// Rider
rider = gustavo;
// User defined variables
rho_w = 1000; // density of water 16C [kg/m^3]
rho_a = 1.225; // density of air 15C [kg/m^3]
CL_max_w = 1.1; // max wing lift coeff [-]
mass_hph = 15; // vehicle mass [kg]
tc_w = 0.12; // wing thickness ratio [-]
lambda_w = 0.45; // wing taper ratio [-]
eff_prop = 0.85; // propeller efficiency [-]
eff_mech = 0.95; // mechanical drivetrain efficiency
f_i = 1.48; // induced drag factor [-]
CD_0_w = 0.007; // wing profile drag coeff
CD_strut = 0.0085; // strut profile drag coeff
S_strut = 0.0427; // strut area (submerged) [m^2]
t_strut = 0.028; // strut thickness [m]
CD_fw = 0.009; // front-wing drag coeff
S_fw = 0.04; // front-wing area [m^2]
CD_spray = 0.24; // spray drag coeff
CD_air = 1.0; // Drag coefficient of air-exposed comp.
S_air = 0.35; // Area of air-exposed comp. [m^2]
// "20-Knot" article values are CD_air=0.7 and S_air=0.6503
// Recumbent "Robinho" area is 0.377m^2
// It seems that a 'drag area" of 0.35m^2 for recumbent is reasonable
// Drag Sum-Up (all sources except wing)
Drag_q.Interference = (17*(tc_w)^2-0.05)*t_strut^2;
Drag_q.Spray = CD_spray*t_strut^2;
Drag_q.Air = CD_air*S_air*rho_a/rho_w;
Drag_q.Strut = CD_strut*S_strut;
Drag_q.Front = CD_fw*S_fw;
Sref = 0;
fn = fieldnames(Drag_q);
for n=1:length(length(fn))
Sref = Sref + Drag_q(fn(n));
end
// Deflection data (Taken from Figure 6.5, chapter 6 of "Human-Powered
// Vehicles", p. 87)
// 0.08 tip deflection for Fiberglass
DEFL = [2 (1.5/7.3)*30+5;
(3.75/11.4)*7+2 (2.7/7.3)*30+5;
9 (4.4/7.3)*30+5];
// As presented in the paper, we will build iso-lines of certain
// performance parameters (Max Speed, TO-Speed, Max wing-tip deflection)
// as a function of aspect-ratio and wing span
function Pwr = OpPointPwr(aspect,wing_span,speed,rider)
mass_tot = rider.mass + mass_hph;
e = 1/(1+0.015);
q = 0.5*rho_w*speed^2;
S = wing_span^2/aspect;
Di = f_i*(mass_tot*GRAV)^2/(%pi*e*q*wing_span^2);
S_drag = CD_0_w*S+Sref;
Pwr = speed*(q*S_drag + Di)/(eff_prop*eff_mech);
endfunction
function V = MaxSpeed(aspect,wing_span,rider)
mass_tot = rider.mass + mass_hph;
Pwr_des = rider.pwr;
function y=dragequation(x)
v = x(1);
e = 1/(1+0.015);
q = 0.5*rho_w*v^2;
S = wing_span^2/aspect;
Di = f_i*(mass_tot*GRAV)^2/(%pi*e*q*wing_span^2);
y = Pwr_des*eff_prop*eff_mech - v*q*(CD_0_w*S+Sref) - v*Di;
endfunction
[xres,val,info] = fsolve([8],dragequation);
if info==1
V = xres(1);
else
V = %nan;
end
endfunction
function [Pwr, Vel] = MinPower(aspect,wing_span,rider)
mass_tot = rider.mass + mass_hph;
function y = minpowersystem(x)
y = zeros(2,1);
v = x(1);
pwr = x(2);
e = 1/(1+0.015);
q = 0.5*rho_w*v^2;
S = wing_span^2/aspect;
Di = f_i*(mass_tot*GRAV)^2/(%pi*e*q*wing_span^2);
S_drag = CD_0_w*S+Sref;
y(1) = pwr*eff_prop*eff_mech - v*(q*S_drag+Di);
y(2) = 3*q*(S_drag)- Di;
endfunction
[xres,val,info] = fsolve([3;1.5],minpowersystem);
if info==1
Vel = xres(1);
Pwr = xres(2);
else
Vel = %nan;
Pwr = %nan;
end
endfunction //MinPower
function V = TOSpeed(aspect,wing_span,rider)
mass_tot = rider.mass + mass_hph;
V = sqrt(aspect*mass_tot*GRAV/...
(0.5*rho_w*0.9*CL_max_w*wing_span^2));
endfunction // TOSpeed
//Axiliary functions
function map = mapspace(func,xvec,yvec,extras)
rider = extras(1).entries;
xi=1;
for x=xvec
yi=1;
for y=yvec
map(yi,xi)=func(x,y,rider);
yi=yi+1;
end
xi=xi+1;
end
endfunction
// Plotting and printing functions
function setmyaxprops()
ax = gca();
myfontstyle = 5;
ax.filled = "on";
ax.background = color('white');
ax.grid = [color('gray') ,color('gray')];
ax.grid_style = [7,7]; // short-dashed lines
ax.font_style = myfontstyle;
ax.font_size = 2;
ax.y_label.font_style = myfontstyle;
ax.y_label.font_size = 3;
ax.x_label.font_style = myfontstyle;
ax.x_label.font_size = 3;
ax.title.font_style = myfontstyle;
ax.title.font_size = 4;
endfunction // setmyaxprops
function cr = PlotWing(aspect,wing_span,lambda)
S = wing_span^2/aspect;
cr = 2*S/(wing_span*(1+lambda));
x_tip_l = -wing_span/2;
x_tip_r = wing_span/2;
y_tip_lw = -lambda*cr/2;
y_tip_up = lambda*cr/2;
pol_x = [x_tip_l x_tip_l 0 x_tip_r x_tip_r 0];
pol_y = [y_tip_lw y_tip_up cr/2 y_tip_up y_tip_lw -cr/2];
figure();
xpoly(pol_x,pol_y,"lines",1);
xfpolys(pol_x',pol_y',color('white'));
ax = gca();
ax.isoview = "on";
endfunction // PlotWing
function PlotDragPie(drags)
x = [];
sp = [];
txt = [];
fn = fieldnames(drags);
for n=1:length(length(fn))
x = [x drags(fn(n))];
txt = [txt fn(n)];
if length(strstr(fn(n),'Wing'))>0
sp = [sp 1];
else
sp = [sp 0];
end
end
figure()
pie(x,sp,txt);
endfunction
// Script calculations
if DO_CALC
// Extra variables for mapping functions
extras = cell(1,1);
extras(1).entries = rider;
// First define reasonable intervals for aspect ratio and
// wing span
aspects = linspace(5,35,75);
span_interval = linspace(1.05,2.3,75);
// Calculate isolines of the interesting performance parameters
// as function of wing dimensions using the above-defined functions
V_max = mapspace(MaxSpeed,aspects,span_interval,extras);
Pwr_min = mapspace(MinPower,aspects,span_interval,extras);
V_TO = mapspace(TOSpeed,aspects,span_interval,extras);
end
// Plot results
if DO_PLOTS
speeds = [4.5 5 5.5 6];
minpwrlvl = [125 150 175 200];
speedsTO = [2.5 2.75 3 3.25];
N_speeds = length(speeds);
N_pwr = length(minpwrlvl);
N_TO = length(speedsTO);
// Isoline plots
figure();
contour2d(span_interval,aspects,V_max,speeds,...
style=color('blue')*ones(1,N_speeds));
contour2d(span_interval,aspects,Pwr_min,minpwrlvl,...
style=color('red')*ones(1,N_pwr));
contour2d(span_interval,aspects,V_TO,speedsTO,...
style=color('green')*ones(1,N_TO));
plot2d(DEFL(:,1)*FT2M,DEFL(:,2),color('magenta'));
plot2d(prj_span,prj_aspect,-3);
xgrid();
xlabel('Wing Span [m]');
ylabel('Aspect Ratio');
xtitle('Performance Curves. Rider: '+rider.name);
legends(['Take-off speed','Cruise speed','Min power','Tip deflection'], [color('green') color('blue') color('red') color('magenta')], 'ur');
setmyaxprops();
ax = gca();
ax.tight_limits = 'on';
ax.data_bounds = [1.1 5; 2.3 30];
// Wing Plot
cr = PlotWing(prj_aspect,prj_span,lambda_w);
// Drag build-up @ 5m/s
mass_tot = rider.mass + mass_hph;
e = 1/(1+0.025);
q = 0.5*rho_w*5^2;
Drag_q.WingCD0 = CD_0_w*prj_span^2/prj_aspect;
Drag_q.WingDi = f_i*(mass_tot*GRAV)^2/(%pi*e*q^2*prj_span^2);
PlotDragPie(Drag_q);
end
// Compute results
to_speed = TOSpeed(prj_aspect,prj_span,rider);
to_power = OpPointPwr(prj_aspect,prj_span,to_speed,rider);
cruise_speed = MaxSpeed(prj_aspect,prj_span,rider);
old_pwr = rider.pwr;
rider.pwr = 750;
max_speed = MaxSpeed(prj_aspect,prj_span,rider);
rider.pwr = old_pwr;
[min_power minpwrvel] = MinPower(prj_aspect,prj_span,rider);
// Print results
mprintf('Results:\n');
mprintf('----------------\n');
mprintf('Chosen wind span[m]/aspect ratio[-]: %.2f, %.1f\n\n',prj_span,prj_aspect);
mprintf('-Rider----------\n');
mprintf('Name : %s\n',rider.name);
mprintf('Mass [kg]: %.1f\n',rider.mass);
mprintf('Power [W]: %.1f\n\n',rider.pwr);
mprintf('-Wing-----------\n');
mprintf('Wing area [m^2]: %.3f\n',prj_span^2/prj_aspect);
mprintf('Root Chord [m]: %.3f\n',cr);
mprintf('Tip Chord [m]: %.3f\n\n',lambda_w*cr);
mprintf('-Performance----\n');
mprintf('Take-off speed [m/s]: %.1f\n',to_speed);
mprintf('Take-off power [W]: %.1f\n',to_power);
mprintf('Cruise Speed [m/s]: %.1f\n',cruise_speed);
mprintf('Range [km]: %.2f\n',cruise_speed*1.0*3600/1000);
mprintf('Speed@750W [m/s]: %.1f\n',max_speed);
mprintf('Min power [W]: %.1f\n',min_power);
mprintf('Speed@MinPwr [m/s]: %.1f\n',minpwrvel);
// Change log
// 2015-10-17 - Diego Montero
// ----------------------------
// Added legends to the line functions :)
// 2015-09-29 - Gustavo Violato
// ----------------------------
// Change original line functions for height-maps of desired variables
// Plot of wing planform and drag build-up for design point as a pie chart
// 2015-09-20 - Gustavo Violato
// ----------------------------
// First release
|
e3510abb27b1696be2ee9a4aa97dc0ef2893a20e | 8217f7986187902617ad1bf89cb789618a90dd0a | /browsable_source/2.5/Unix-Windows/scilab-2.5/macros/fraclab/WT2Dext.sci | 7f2b400ac18cb30ed748b189d5eff49a655982c3 | [
"LicenseRef-scancode-public-domain",
"LicenseRef-scancode-warranty-disclaimer"
] | permissive | clg55/Scilab-Workbench | 4ebc01d2daea5026ad07fbfc53e16d4b29179502 | 9f8fd29c7f2a98100fa9aed8b58f6768d24a1875 | refs/heads/master | 2023-05-31T04:06:22.931111 | 2022-09-13T14:41:51 | 2022-09-13T14:41:51 | 258,270,193 | 0 | 1 | null | null | null | null | UTF-8 | Scilab | false | false | 2,071 | sci | WT2Dext.sci | function V=WT2Dext(wt,Sc,Num)
// This Software is ( Copyright INRIA . 1998 1 )
//
// INRIA holds all the ownership rights on the Software.
// The scientific community is asked to use the SOFTWARE
// in order to test and evaluate it.
//
// INRIA freely grants the right to use modify the Software,
// integrate it in another Software.
// Any use or reproduction of this Software to obtain profit or
// for commercial ends being subject to obtaining the prior express
// authorization of INRIA.
//
// INRIA authorizes any reproduction of this Software.
//
// - in limits defined in clauses 9 and 10 of the Berne
// agreement for the protection of literary and artistic works
// respectively specify in their paragraphs 2 and 3 authorizing
// only the reproduction and quoting of works on the condition
// that :
//
// - "this reproduction does not adversely affect the normal
// exploitation of the work or cause any unjustified prejudice
// to the legitimate interests of the author".
//
// - that the quotations given by way of illustration and/or
// tuition conform to the proper uses and that it mentions
// the source and name of the author if this name features
// in the source",
//
// - under the condition that this file is included with
// any reproduction.
//
// Any commercial use made without obtaining the prior express
// agreement of INRIA would therefore constitute a fraudulent
// imitation.
//
// The Software beeing currently developed, INRIA is assuming no
// liability, and should not be responsible, in any manner or any
// case, for any direct or indirect dammages sustained by the user.
//
// Any user of the software shall notify at INRIA any comments
// concerning the use of the Sofware (e-mail : FracLab@inria.fr)
//
// This file is part of FracLab, a Fractal Analysis Software
[wti, wtl]=WT2DStruct(wt);
V=zeros(wtl(Sc,1), wtl(Sc,2));
index=0;
for i=0:(wtl(Sc,1)-1),
for j=0:(wtl(Sc,2)-1),
V(i+1,j+1)=wt(wti(Sc,Num)+index),
index = index+1;
end;
end;
|
929fa3f5228a51eebb730325685f27dec9427e9f | 449d555969bfd7befe906877abab098c6e63a0e8 | /564/DEPENDENCIES/5_3data.sci | 058ae4be0c0f53015c1ccb127e5aa8dd57212d29 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 190 | sci | 5_3data.sci | AC=30;//C.S. area of AC,given,in mm^2
A=20;//C.S. areaa of other elements,given,in mm^2
L=800;//langth,given in mm
E=200000;//given in N/mm^2
theta=60*(%pi/180);
Load=100;//given,in N
|
d184a467d12b24c4eb5e8b321fcbfdf75c52e6c3 | a62e0da056102916ac0fe63d8475e3c4114f86b1 | /set8/s_Elements_Of_Thermodynamics_And_Heat_Transfer_O._N._Young_2519.zip/Elements_Of_Thermodynamics_And_Heat_Transfer_O._N._Young_2519/CH5/EX5.2/Ex5_2.sce | adae4516fe72af86453c9a26ac9b2dc6b5762b21 | [] | no_license | hohiroki/Scilab_TBC | cb11e171e47a6cf15dad6594726c14443b23d512 | 98e421ab71b2e8be0c70d67cca3ecb53eeef1df6 | refs/heads/master | 2021-01-18T02:07:29.200029 | 2016-04-29T07:01:39 | 2016-04-29T07:01:39 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 196 | sce | Ex5_2.sce | errcatch(-1,"stop");mode(2);
//Initialization of variables
V=100 //ft/s
v=15 //lbm/ft^3
m=5 //lbm/s
//calculations
A=m*v/V
//results
printf("Area of inlet pipe = %.2f ft^2",A)
exit();
|
bcf61fd14e2d0150200496aad2dde47730006c4f | 449d555969bfd7befe906877abab098c6e63a0e8 | /3862/CH2/EX2.10/Ex2_10.sce | 75bb34d510601620020a1ea601beaed3d91526de | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 646 | sce | Ex2_10.sce | clear
//
//variable declaration
PA=800.0 //Vertical down loading at A,N
PC=400.0 //vertical up loading at B,N
HD=600.0 //Horizontal left loading at A,N
HB=200.0 //Horizontal right loading at B,N
a=1.0 //length of side,m
//sum of vertical Fy & sum of horizontal forces Fx is zero
//Assume direction of Fx is right
//Assume direction of Fy is up
Fx=HB-HD
Fy=PC-PA
R=sqrt((Fx**2)+(Fy**2))
printf("\n R= %0.2f N",R)
theta=atan(Fy/Fx)*180/%pi
printf("\n theta= %0.0f °",theta)
//moment at A
MA=PC*a+HD*a
//Let x be the distance from A along x axis, where resultant cuts AB.
x=MA/Fy
printf("\n x= %0.1f m",(-x))
|
409a64ff36b738bc15e2af377e10be8d111dcec2 | 3a11df70b5f5b856da599098aa46b015099f34e9 | /logic_gates/DMux4Way.tst | d7f31ea70488cf51b9a4b477bdb556200a185099 | [] | no_license | nkyorov/logic-gates-hdl | 7da52af49a0c333e3f755a9ec552746662580cd3 | 1deff96f5a6631ce7c5b7ea2db8a7250f2d37908 | refs/heads/master | 2021-04-27T00:46:58.298377 | 2019-05-25T12:32:09 | 2019-05-25T12:32:09 | 122,660,544 | 3 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 392 | tst | DMux4Way.tst | load DMux4Way.hdl,
output-file DMux4Way.out,
compare-to DMux4Way.cmp,
output-list in%B2.1.2 sel%B2.2.2 w%B2.1.2 x%B2.1.2 y%B2.1.2 z%B2.1.2;
set in 0,
set sel %B00,
eval,
output;
set sel %B01,
eval,
output;
set sel %B10,
eval,
output;
set sel %B11,
eval,
output;
set in 1,
set sel %B00,
eval,
output;
set sel %B01,
eval,
output;
set sel %B10,
eval,
output;
set sel %B11,
eval,
output;
|
3473253d0b21e7230985eceda416ba9211c33a23 | 449d555969bfd7befe906877abab098c6e63a0e8 | /69/CH2/EX2.26.a/2_26_a.sce | db9e1a2b18b43a7dd8c1f023e1486b70c09b6fa3 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 280 | sce | 2_26_a.sce | //Implementation of example 2.26_a in chapter 2
clear; clc; close;
Rl = 1.2*10^(3);
R = 10^(3);
Vi = 16;
Vz = 10;
V = (Rl*Vi)/(R+Rl);
Vl = V;
Vr = Vi-Vl;
Iz = 0;
Pz = Iz*Vz;
disp(Vl,'Vl is : ');
disp(Vr,'Vr is :');
disp(Iz,'IZ is :');
disp(Pz,'Pz is :');
|
d8aac7b303c985905314d25717d0d3c6baabde5d | a8592d34f144b71794ebf30f1c2a1b5faf0b053c | /AkarPersamaan/scilab/newton_raphson.sce | 2720b5a78e031978a2d23cfdc80f034201203c29 | [] | no_license | f-fathurrahman/ffr-MetodeNumerik | ee9a6a7153b174b1ba3d714fe61ccbd1cb1dd327 | e3a9da224c0fd5b32e671708e890018a3c4104c4 | refs/heads/master | 2023-07-19T22:29:38.810143 | 2023-07-07T10:02:34 | 2023-07-07T10:02:34 | 107,272,110 | 2 | 2 | null | null | null | null | UTF-8 | Scilab | false | false | 898 | sce | newton_raphson.sce | function root = newton_raphson( f, df, a, tol, NiterMax )
if ~exists("tol", "local")
tol = 1e-9
end
if ~exists("NiterMax", "local")
NiterMax = 30
end
printf("\nRoot searching via Newton-Raphson method\n")
printf("Initial guess root: %18.10f\n", a)
printf("Tolerance: %18.10e\n", tol)
printf("newton_raphson will iterate up to %d maximum iterations.\n", NiterMax)
x = a
printf("\n")
for iter = 1:NiterMax
fx = f(x)
printf("newton_raphson: %5d %18.10f %18.10e\n", iter, x, fx )
if abs(fx) < tol
printf("newton_raphson: Convergence achieved\n")
root = x
return
end
dfx = df(x)
if abs(dfx) < %eps
printf("ERROR in newton_raphson: very small derivative\n")
root = x
return
end
dx = -fx/dfx
x = x + dx
end
printf("WARNING in newton_rapshon: Iterations does not converge\n")
endfunction
|
70889294798602132cd900ddcc0d19321faa6bf7 | 449d555969bfd7befe906877abab098c6e63a0e8 | /503/CH7/EX7.12/ch7_12.sci | b0751da8e607539907cf4fd2f8bd3fde4ddd9410 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 231 | sci | ch7_12.sci | //to calculate no of turns reqd on each interpole
clc;
P=25000;
V=440;
I_a=P/V;
Z=846;
A=2;
P=4;
B_i=.5;
u_o=4*%pi*10^-7;
l_gi=.003;
AT_i=((I_a*Z)/(2*A*P))+(B_i*l_gi)/u_o;
N_i=ceil(AT_i/I_a);
disp(N_i,'no of turns'); |
39ec930f0c73ff119f3762bcb78ab28a17e89da8 | 22ebb77444925f738e01f4ceeae89fac1b2ca711 | /Single-phase transformer/fluxfmm.sci | 83a1325205eedd9932321bbc4d36a18f4d473c94 | [] | no_license | jacometoss/Transformer | 4e4b4d39f370b162afd6364a229efc81a5c4ea8d | d9bd077b3fbc45dca52dd3367f40a4289b812e54 | refs/heads/master | 2021-06-21T14:57:12.644937 | 2020-12-03T19:23:20 | 2020-12-03T19:23:20 | 146,820,465 | 1 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 139 | sci | fluxfmm.sci | function [Flux,Fmm]=fluxfmm(Voc,Ioc,Np,l,A)
fhz=60;
B=Voc/(sqrt(2)*%pi*fhz*Np*A);
Flux=B*A;
Fmm=Np*Ioc;
endfunction
|
5e6c50712991805076ff0e379bbb29c0ce296a99 | fce47a4c482ae622563fc72d7643d824cc572edc | /_scilabTP/tp2/exercice4.sce | 592f4e2b90e21dc7445408dd072d696a67d7c7bf | [] | no_license | ece2lr/ece2lr.github.io | a57ff8852ef06b7cef1c734106f1badd668ebcb1 | 13479dc224e39521c6c387401b889e62a90a8d0b | refs/heads/master | 2021-01-12T12:07:37.196408 | 2017-12-16T19:25:16 | 2017-12-16T19:25:16 | 72,310,248 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 477 | sce | exercice4.sce | LIGNES = 1
COLONNES = 10^5
// // pour la loi uniforme
// echUnif = grand (LIGNES, COLONNES, "uin", 0,20)
//
// clf()
// classes = 21
// histplot(classes, echUnif)
//les parametres de la loi binomiale B(n,p)
n = 50 // essayez de changer ! exemples :
//n = 10 // ou
//n = 300
p = .3
// mon échantillon
echBin = grand (LIGNES, COLONNES, "bin", n,p)
clf()
classes = -1:n
histplot(classes, echBin)
plot(0:n, binomial(p,n))
// disp(echUnif) // affichage de l'échantillon
|
2cb09483806bc484b7a39233efc3e4fccfb8b731 | 449d555969bfd7befe906877abab098c6e63a0e8 | /620/CH26/EX26.3/example26_3.sce | b1298e660a6dbc261d51a744e7cca081f62e689f | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 106 | sce | example26_3.sce | p=100;
c=10*10^(-6);
i=0.87;
x_c=p/i^2;
f=1/(2*%pi*x_c*c);
disp("the frequency (in Hz) is"); disp(f); |
adde8960c7dc683a2ace522dcac17f649f733514 | 8627886261b3eddf8440c0b470cd9ee25c762d97 | /сайлаб/twelve.sce | 7710184201c479637b2032c90bdcf602d3e2a16e | [] | no_license | timurzotov/pvis | ba75cf86fae91b6adc8dd3fe9cd2672eea561cca | d60e8e241d6ce0ad3a9b2a75c8771f92a9b039ba | refs/heads/master | 2020-09-08T07:59:31.719500 | 2019-11-11T21:14:13 | 2019-11-11T21:14:13 | 221,070,925 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 493 | sce | twelve.sce | xname('ЗАДАНИЕ 12.1')
clc
x=-5:.1:5; y=x^3/3-x^2/2-6*x+1;
plot2d(x,y,axesflag=5); xgrid()
xtitle('График функции: y=x^3/3-x^2/2-6*x+1', 'x', 'y'),
clc
function y= gg(x)
if q==1 then y=x.^3/3-x.^2/2-6*x+1 else
y=-(x.^3/3-x.^2/2-6*x+1) end
endfunction
funcprot(0);
function [f,g,r]=z(x,r)
f=gg(x)
g=numderivative(gg,x)
endfunction
x0=-2; q=3; //max = -2
[fmax,xmax]=optim(z,x0)
xmax,fmax=-fmax
x0=3;q=1;
[fmin,xmin]=optim(z,x0)
//xmin, fmin, xmax, fmax
|
6aaaacb0e90dfbebe0bd4c318d21a416e1024141 | 449d555969bfd7befe906877abab098c6e63a0e8 | /45/CH11/EX11.1/example_11_1.sce | 252cd799c7b4ea36520fb52dfaec372d2394d1ba | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 999 | sce | example_11_1.sce | //example 11.1
clc;
//this program requires
//kmap3a.sci to find the kmap
//noof.sci function used inside kmap
//noof0.sci function used inside kmap
n= [ 0 0 0;
0 0 1;
0 1 0;
0 1 1;
1 0 0;
1 0 1;
1 1 0;
1 1 1];
for i= 1:8 //printing the state synthesis table
an1(i,1)=n(i,3);
dn(i,1)=n(i,3);
if n(i,1)==1 & n(i,2) ==1 & n(i,3)==0 then
z(i,1)=1;
else
z(i,1)=0;
end
end;
dis=[n an1 dn z];
disp('State Synthesis table :');
disp(' An X Y An1 Dn Z');
disp(dis);
printf('\n\n Design equations :\n');
Dn = [ 0 1 1 0;0 1 1 0];
Z= [ 0 0 0 0;0 0 0 1];
dn1= kmap3a(Dn); // finding the 3 varible kmap of Dn
printf('\n Dn = %s \n\n',dn1); //displaying the minimized expression
z1= kmap3a(Z); //finding the 3 variable kmap of Z
printf('\n Z = %s \n\n',z1); //displaying the minimized expression
|
975417d897e643b0113c1426c1110baab7205680 | ec137036bbd0b9a8f83ce1b09d94fd2f6fdcbfdf | /part2/nld.judgements.tst | f8aa03806342bb34286718d52b3e95f84f9526ce | [] | no_license | sigmorphon/2021Task0 | cef358c80898421a3b9dc966b17b3fe337690a14 | a8b31713b838bdb32a9bd84a866ee7d330a0badb | refs/heads/main | 2023-08-25T18:06:42.560860 | 2021-10-14T01:01:48 | 2021-10-14T01:01:48 | 339,821,394 | 21 | 10 | null | 2021-10-06T06:49:37 | 2021-02-17T18:40:57 | Scilab | UTF-8 | Scilab | false | false | 6,177 | tst | nld.judgements.tst | ɑ s ə ɑ s t ə V;PST;PL
ɑ s ə ɑ iː s ə V;PST;PL
b ə l ɛɪ z ə b ə l ɛɪ z d ə V;PST;PL
b ə l ɛɪ z ə b ə l eː z ə V;PST;PL
b ə r aː ɣ ə b ə r aː ɣ d ə V;PST;PL
b ə r aː ɣ ə b ə r iː ɣ ə V;PST;PL
b ə z eː l ə b ə z eː l d ə V;PST;PL
b ə z eː l ə b ə z aː l ə V;PST;PL
b ɛɪ ɣ ə b ɛɪ ɣ d ə V;PST;PL
b ɛɪ ɣ ə b eː ɣ ə V;PST;PL
b ɪ n ə b ɪ n d ə V;PST;PL
b ɪ n ə b ɔ n ə V;PST;PL
b l aː ɣ ə b l aː ɣ d ə V;PST;PL
b l aː ɣ ə b l iː ɣ ə V;PST;PL
b l aː p ə b l aː p t ə V;PST;PL
b l aː p ə b l iː p ə V;PST;PL
b r aː ɣ ə b r aː ɣ d ə V;PST;PL
b r aː ɣ ə b r uː ɣ ə V;PST;PL
b r ɪ ŋ k ə b r ɪ ŋ k t ə V;PST;PL
b r ɪ ŋ k ə b r ɔ ŋ k ə V;PST;PL
d ɛɪ ɣ ə d ɛɪ ɣ d ə V;PST;PL
d ɛɪ ɣ ə d eː ɣ ə V;PST;PL
d r aː z ə d r aː z d ə V;PST;PL
d r aː z ə d r iː z ə V;PST;PL
d r eː k ə d r eː k t ə V;PST;PL
d r eː k ə d r aː k ə V;PST;PL
f ɪ n ə f ɪ n d ə V;PST;PL
f ɪ n ə f ɔ n ə V;PST;PL
f l ɛɪ p ə f l ɛɪ p t ə V;PST;PL
f l ɛɪ p ə f l eː p ə V;PST;PL
f l ɪ m ə f l ɪ m d ə V;PST;PL
f l ɪ m ə f l ɔ m ə V;PST;PL
ɣ eː z ə ɣ aː r ə V;PST;PL
ɣ eː z ə ɣ aː z ə V;PST;PL
h ɑ l ə h ɑ l d ə V;PST;PL
h ɑ l ə h iː l ə V;PST;PL
j ɪ n ə j ɪ n d ə V;PST;PL
j ɪ n ə j ɔ n ə V;PST;PL
k ɛɪ ɣ ə k ɛɪ ɣ d ə V;PST;PL
k ɛɪ ɣ ə k eː ɣ ə V;PST;PL
k ɛ r ɣ ə k ɛ r ɣ d ə V;PST;PL
k ɛ r ɣ ə k ɔ r ɣ ə V;PST;PL
k ɪ n ə k ɪ n d ə V;PST;PL
k ɪ n ə k ɔ n ə V;PST;PL
k l ɛɪ ɣ ə k l ɛɪ ɣ d ə V;PST;PL
k l ɛɪ ɣ ə k l eː ɣ ə V;PST;PL
k l ɛɪ p ə k l ɛɪ p t ə V;PST;PL
k l ɛɪ p ə k l eː p ə V;PST;PL
k n eː k ə k n eː k t ə V;PST;PL
k n eː k ə k n aː k ə V;PST;PL
k n ɪ m ə k n ɪ m d ə V;PST;PL
k n ɪ m ə k n ɔ m ə V;PST;PL
k n ɪ ŋ ə k n ɪ ŋ d ə V;PST;PL
k n ɪ ŋ ə k n ɔ ŋ ə V;PST;PL
k r aː ɣ ə k r aː ɣ d ə V;PST;PL
k r aː ɣ ə k r uː ɣ ə V;PST;PL
k r eː k ə k r eː k t ə V;PST;PL
k r eː k ə k r aː k ə V;PST;PL
k r ɛɪ n ə k r ɛɪ n d ə V;PST;PL
k r ɛɪ n ə k r eː n ə V;PST;PL
k r iː z ə k r iː z d ə V;PST;PL
k r iː z ə k r oː z ə V;PST;PL
k r ɪ m ə k r ɪ m d ə V;PST;PL
k r ɪ m ə k r ɔ m ə V;PST;PL
k r ɪ ŋ ə k r ɪ ŋ d ə V;PST;PL
k r ɪ ŋ ə k r ɔ ŋ ə V;PST;PL
k w ɑ s ə k w ɑ s t ə V;PST;PL
k w ɑ s ə k w iː s ə V;PST;PL
n eː z ə n aː r ə V;PST;PL
n eː z ə n aː z ə V;PST;PL
n ɛɪ v ə n ɛɪ v d ə V;PST;PL
n ɛɪ v ə n eː v ə V;PST;PL
n ʊɪ k ə n ʊɪ k t ə V;PST;PL
n ʊɪ k ə n oː k ə V;PST;PL
ɔ n t r aː r ə ɔ n t r aː r d ə V;PST;PL
ɔ n t r aː r ə ɔ n t r iː r ə V;PST;PL
ɔ n t r ʊɪ k ə ɔ n t r ʊɪ k t ə V;PST;PL
ɔ n t r ʊɪ k ə ɔ n t r oː k ə V;PST;PL
p l ɛɪ z ə p l ɛɪ z d ə V;PST;PL
p l ɛɪ z ə p l eː z ə V;PST;PL
p r ɪ n ə p r ɪ n d ə V;PST;PL
p r ɪ n ə p r ɔ n ə V;PST;PL
s n ɛɪ k ə s n ɛɪ k t ə V;PST;PL
s n ɛɪ k ə s n eː k ə V;PST;PL
s n ʊɪ p ə s n ʊɪ p t ə V;PST;PL
s n ʊɪ p ə s n oː p ə V;PST;PL
ʃ ɛɪ ɣ ə ʃ ɛɪ ɣ d ə V;PST;PL
ʃ ɛɪ ɣ ə ʃ eː ɣ ə V;PST;PL
ʃ ɪ n ə ʃ ɪ n d ə V;PST;PL
ʃ ɪ n ə ʃ ɔ n ə V;PST;PL
ʃ ɪ ŋ k ə ʃ ɪ ŋ k t ə V;PST;PL
ʃ ɪ ŋ k ə ʃ ɔ ŋ k ə V;PST;PL
t ɛ r v ə t ɛ r v d ə V;PST;PL
t ɛ r v ə t iː r v ə V;PST;PL
t r eː m ə t r eː m d ə V;PST;PL
t r eː m ə t r aː m ə V;PST;PL
t r eː z ə t r aː r ə V;PST;PL
t r eː z ə t r aː z ə V;PST;PL
t r iː z ə t r iː z d ə V;PST;PL
t r iː z ə t r oː z ə V;PST;PL
t r ɪ ŋ ə t r ɪ ŋ d ə V;PST;PL
t r ɪ ŋ ə t r ɔ ŋ ə V;PST;PL
t r ʊɪ k ə t r ʊɪ k t ə V;PST;PL
t r ʊɪ k ə t r oː k ə V;PST;PL
v eː z ə v eː z d ə V;PST;PL
v eː z ə v aː z ə V;PST;PL
v ə r aː ɣ ə v ə r aː ɣ d ə V;PST;PL
v ə r aː ɣ ə v ə r iː ɣ ə V;PST;PL
v ə r aː v ə v ə r aː v d ə V;PST;PL
v ə r aː v ə v ə r iː v ə V;PST;PL
v ə r d r ɪ k ə v ə r d r ɪ k t ə V;PST;PL
v ə r d r ɪ k ə v ə r d r ɔ k ə V;PST;PL
v ə r h ɑ f ə v ə r h ɑ f t ə V;PST;PL
v ə r h ɑ f ə v ə r h iː v ə V;PST;PL
v ə r h eː k ə v ə r h eː k t ə V;PST;PL
v ə r h eː k ə v ə r h aː k ə V;PST;PL
v ə r z ɛɪ k ə v ə r z ɛɪ k t ə V;PST;PL
v ə r z ɛɪ k ə v ə r z eː k ə V;PST;PL
v ɛɪ ɣ ə v ɛɪ ɣ d ə V;PST;PL
v ɛɪ ɣ ə v eː ɣ ə V;PST;PL
v ɛɪ k ə v ɛɪ k t ə V;PST;PL
v ɛɪ k ə v eː k ə V;PST;PL
v ɛɪ s ə v ɛɪ s t ə V;PST;PL
v ɛɪ s ə v eː s ə V;PST;PL
v ɪ n ə v ɪ n d ə V;PST;PL
v ɪ n ə v ɔ n ə V;PST;PL
v l aː z ə v l aː z d ə V;PST;PL
v l aː z ə v l iː z ə V;PST;PL
w ɛɪ ɣ ə w ɛɪ ɣ d ə V;PST;PL
w ɛɪ ɣ ə w eː ɣ ə V;PST;PL
w ɛ r ɣ ə w ɛ r ɣ d ə V;PST;PL
w ɛ r ɣ ə w iː r ɣ ə V;PST;PL
w ʊɪ k ə w ʊɪ k t ə V;PST;PL
w ʊɪ k ə w oː k ə V;PST;PL
x eː m ə x eː m d ə V;PST;PL
x eː m ə x aː m ə V;PST;PL
x eː z ə x aː z ə V;PST;PL
x eː z ə x aː r ə V;PST;PL
x ɛɪ ɣ ə x ɛɪ ɣ d ə V;PST;PL
x ɛɪ ɣ ə x eː ɣ ə V;PST;PL
x ɛ l ə x ɛ l d ə V;PST;PL
x ɛ l ə x ɔ l ə V;PST;PL
x ɛ l p ə x ɛ l p t ə V;PST;PL
x ɛ l p ə x ɔ l p ə V;PST;PL
x r ɛɪ ɣ ə x r ɛɪ ɣ d ə V;PST;PL
x r ɛɪ ɣ ə x r eː ɣ ə V;PST;PL
x r ɛɪ k ə x r ɛɪ k t ə V;PST;PL
x r ɛɪ k ə x r eː k ə V;PST;PL
z iː z ə z iː z d ə V;PST;PL
z iː z ə z iː s t ə V;PST;PL
z ɪ m ə z ɪ m d ə V;PST;PL
z ɪ m ə z ɔ m ə V;PST;PL
z ʊɪ k ə z ʊɪ k t ə V;PST;PL
z ʊɪ k ə z oː k ə V;PST;PL
z ʊɪ v ə z ʊɪ v d ə V;PST;PL
z ʊɪ v ə z oː v ə V;PST;PL
z w ɑ ŋ ə z w ɑ ŋ d ə V;PST;PL
z w ɑ ŋ ə z w ɪ ŋ d ə V;PST;PL
z w ɑ s ə z w ɑ s t ə V;PST;PL
z w ɑ s ə z w iː s ə V;PST;PL
z w ɛ ŋ ə z w ɛ ŋ d ə V;PST;PL
z w ɛ ŋ ə z w ɔ ŋ ə V;PST;PL
z w ɪ ŋ ə z w ɪ ŋ d ə V;PST;PL
z w ɪ ŋ ə z w ɔ ŋ ə V;PST;PL
z w ɪ ŋ k ə z w ɪ ŋ k t ə V;PST;PL
z w ɪ ŋ k ə z w ɔ ŋ k ə V;PST;PL
|
8898e137a398f31a306aceed78d0bf75928d9864 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2063/CH7/EX7.17/7_17.sce | b8b5b3407ed2fe73d3d36abff4f1de75440d4020 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,313 | sce | 7_17.sce | clc
clear
//Input data
P=200;//Power developed by a six cylinder diesel engine in kW
N=2000;//Operating speed of the engine in rpm
bs=0.2;//The brake specific fuel consumption in kg/kWh
p1=35;//The pressure of air in the cylinder at the beginning of injection in bar
p2=55;//Maximum cylinder pressure in bar
p3=180;//Initial injection pressure in bar
p4=520;//Maximum pressure at the injector in bar
Cd=0.75;//Coefficient of discharge
S=850;//Specific gravity of fuel
p5=1;//Atmospheric pressure in bar
a=16;//The crank angle over which injection takes place in degrees
//Calculations
Po=P/6;//Power output per cylinder in kW
F=(Po*bs)/60;//Fuel consumed per cylinder in kg/min
Fi=F/(N/2);//Fuel injected per cycle in kg
T=a/(360*(N/60));//Duration of injection in s
deltaP1=p3-p1;//Pressure difference at the beginning of injection in bar
deltaP2=p4-p2;//Pressure difference at the end of injection in bar
avP=(deltaP1+deltaP2)/2;//Average pressure difference in bar
V=Cd*(2*(avP*10^5)/S)^(1/2);//Velocity of injection of fuel jet in m/s
Vo=Fi/S;//Volume of fuel injected per cycle in m^3/cycle
A=(Vo/(V*T))*10^6;//Area of fuel orifices in mm^2
//Output
printf('The total orifice area required per injector if the injection takes place over 16 degree crank angle is %3.4f mm^2',A)
|
97ccca5dd3a7e52b0aa0a195e5ca38c582e5bdbd | 449d555969bfd7befe906877abab098c6e63a0e8 | /1376/CH12/EX12.4/12_4.sci | c541d126b19559238ea1905f900db4b2ff57625a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 327 | sci | 12_4.sci | //12.4
clc;
disp('1.5 cm core displacement produces 6V so')
d_15=6;
d_18=1.8*d_15/1.5
printf("1.8 cm core displacement produces=%.2f V",d_18);
d_08=(-0.8)*(-d_15)/(-1.5);
printf("\n-0.8 cm core displacement produces=%.2f V",d_08);
d_06=(-0.6)*(-d_15)/(-1.5);
printf("\n-0.6 cm core displacement produces=%.2f V",d_06); |
4c14434b720c518098fd8b3c2953e88fa500bdd8 | 9545443abf3ba785ea80d459f01efa5be8df2087 | /cfs/apps/fm/test_and_ground/asist/image/FMCAT3.TST | 457c30325ff536b7deaaaf73957b04623de1c759 | [
"NASA-1.3",
"Apache-2.0"
] | permissive | anthonyneedles/WISE-HEADACHE-JASH | 9ab8f1bcd87a45ddc11fc115e512a5b4465e81e3 | 28199218a8855db88adc43c3daa4a5a832571012 | refs/heads/master | 2023-07-15T04:26:19.817108 | 2020-08-18T01:34:00 | 2020-08-18T01:34:00 | 272,212,651 | 2 | 1 | Apache-2.0 | 2021-09-02T03:58:33 | 2020-06-14T13:57:03 | C | UTF-8 | Scilab | false | false | 1,255 | tst | FMCAT3.TST | This is the test file 3 for the fm_filecat_basic test
Garbage to follow...
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
|
c3fe8736a619412c00d7eefb12f1b6c0a5df3558 | 99b4e2e61348ee847a78faf6eee6d345fde36028 | /Toolbox Test/filtord/filtord9.sce | ddad1d242a743f8cb06d1a7c501326be961dcef4 | [] | no_license | deecube/fosseetesting | ce66f691121021fa2f3474497397cded9d57658c | e353f1c03b0c0ef43abf44873e5e477b6adb6c7e | refs/heads/master | 2021-01-20T11:34:43.535019 | 2016-09-27T05:12:48 | 2016-09-27T05:12:48 | 59,456,386 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 239 | sce | filtord9.sce | a=[1 2 3 45 6];
b=[2 3 4 56 7];
y=filtord(b,a,1);
disp(y);
//output
//!--error 10000
//too many input arguments
//at line 6 of function narginchk called by :
//at line 3 of function filtord called by :
//y=filtord(b,a,1);
|
02705b7cd02c95aeed64c45b82755d8897f2321e | 1bb72df9a084fe4f8c0ec39f778282eb52750801 | /test/RV3.prev.tst | 52b2076b0d0ec3e214bcf17d9db63d58f920cc95 | [
"Apache-2.0",
"LicenseRef-scancode-unknown-license-reference"
] | permissive | gfis/ramath | 498adfc7a6d353d4775b33020fdf992628e3fbff | b09b48639ddd4709ffb1c729e33f6a4b9ef676b5 | refs/heads/master | 2023-08-17T00:10:37.092379 | 2023-08-04T07:48:00 | 2023-08-04T07:48:00 | 30,116,803 | 2 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 57 | tst | RV3.prev.tst | [1/2,2/3,-1/5,-4/3] - [1/2,1/3,1/5] = [0,1/3,-2/5,-4/3]
|
688c2026ee7e5c58c6add430f82bc2a106844c05 | 1db0a7f58e484c067efa384b541cecee64d190ab | /macros/zplane.sci | f0cf610520202a31b56b30ecb43388d3e1f2902a | [] | no_license | sonusharma55/Signal-Toolbox | 3eff678d177633ee8aadca7fb9782b8bd7c2f1ce | 89bfeffefc89137fe3c266d3a3e746a749bbc1e9 | refs/heads/master | 2020-03-22T21:37:22.593805 | 2018-07-12T12:35:54 | 2018-07-12T12:35:54 | 140,701,211 | 2 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 3,825 | sci | zplane.sci | <<<<<<< HEAD
//Pole-Zero plot for Discrete time systems
//Calling Sequence
//zplane(z)
//zpalne(z,p)
//Parameters:
//z: vector containing numerator coefficients
//p: vector containing denumerator coefficients
//Description:
//This function gives pole zero plote of discrete time systems
//Example :
//zplane([1 2 3],[4 5 6])
//Output :
//Output is pole zero plot of respective discrete time system.
//**************************************************************************************************
//______________________________________version1 code (not working)_________________________________
//__________________________________________________________________________________________________
//**************************************************************************************************
//function [y] = zplane(z,p)
//funcprot(0);
//
//rhs = argn(2)
//
//if(rhs<1 | rhs>2)
//error("Wrong number of input arguments.")
//end
// select(rhs)
// case 1 then
// callOctave("zplane",z)
// case 2 then
// callOctave("zplane",z,p)
// end
//endfunction
//**************************************************************************************************
//______________________________________________version2 code ( working)____________________________
//__________________________________________________________________________________________________
//**************************************************************************************************
function zplane(z,varargin)
funcprot(0);
[nargout nargin] = argn();
if nargin == 1 then
p = [];
else
p = varargin(1);
end
[rows_z columns_z] = size(z);
[rows_p columns_p] = size(p);
if (nargin < 1 | nargin > 2)
error("Invalid inputs")
end
if columns_z>1 | columns_p>1
if rows_z>1 | rows_p>1
// ## matrix form: columns are already zeros/poles
else
// ## z -> b
// ## p -> a
if isempty(z), z=1; end
if isempty(p), p=1; end
M = length(z) - 1;
N = length(p) - 1;
z = [ roots(z); zeros(N - M, 1) ];
p = [ roots(p); zeros(M - N, 1) ];
end
end
xmin = min([-1; real(z(:)); real(p(:))]);
xmax = max([ 1; real(z(:)); real(p(:))]);
ymin = min([-1; imag(z(:)); imag(p(:))]);
ymax = max([ 1; imag(z(:)); imag(p(:))]);
xfluff = max([0.05*(xmax-xmin), (1.05*(ymax-ymin)-(xmax-xmin))/10]);
yfluff = max([0.05*(ymax-ymin), (1.05*(xmax-xmin)-(ymax-ymin))/10]);
xmin = xmin - xfluff;
xmax = xmax + xfluff;
ymin = ymin - yfluff;
ymax = ymax + yfluff;
// text();
// plot_with_labels(z, "o");
// plot_with_labels(p, "x");
// refresh;
r = exp(2*%i*%pi*[0:100]/100);
plot(real(r), imag(r),'k'); //hold on;
// axis equal;
// grid on;
xgrid ;
mtlb_axis(1.05*[xmin, xmax, ymin, ymax]);
if (~isempty(p))
h = plot(real(p), imag(p), "bx");
//set (h, 'MarkerSize', 7);
end
if (~isempty(z))
h = plot(real(z), imag(z), "bo");
//set (h, 'MarkerSize', 7);
end
legend('unit circle','poles','zeros');
// hold off;
endfunction
//function plot_with_labels(x, symbol)
//
// [rows_x columns_x] = size(x);
//
// if ( ~isempty(x) )
//
// x_u = unique(x(:));
//
// for i = 1:length(x_u)
// n = sum(x_u(i) == x(:));
// if (n > 1)
// xstring(real(x_u(i)), imag(x_u(i)), [" " msprintf('string', n)]);
// end
// end
//
// col = "rgbcmy";
// for c = 1:columns_x
// plot(real( x(:,c) ), imag( x(:,c) ), [col(pmodulo(c,6)),symbol ";;"]);
// end
//
// end
//
//endfunction
=======
function [y] = zplane(z,p)
funcprot(0);
rhs = argn(2)
if(rhs<1 | rhs>2)
error("Wrong number of input arguments.")
end
select(rhs)
case 1 then
callOctave("zplane",z)
case 2 then
callOctave("zplane",z,p)
end
endfunction
>>>>>>> 6bbb00d0f0128381ee95194cf7d008fb6504de7d
|
2352f717b7e5953376ecb2b5500f42d5649aeac6 | 449d555969bfd7befe906877abab098c6e63a0e8 | /575/DEPENDENCIES/7_5_1.sci | b98adad10dc234468e690fa348ab324d1a40228e | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 137 | sci | 7_5_1.sci | H0=196.23 //Btu/lbm
H50=202.28 //Btu/lbm
Pfinal=51.99 //psia
Pinitial=18.90 //psia
Vfinal=1.920 //ft^3/lbm
Vinitial=4.969 //ft^3/lbm |
812853a8d69f43288d1422298f35b0111c41ebd8 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1022/CH14/EX14.5/14_5.sce | 3941e49c343838a64f6145949f8c747366fa8145 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 280 | sce | 14_5.sce | clc
//initialisation of variables
T= 300 //F
T1= 50 //F
s= 0.17*10^-8 //Btu/hr ft^2 R^4
e1= 0.93
A= 10 //in
F= 1
//CALCULATIONS
A1= 10*(40/(12*10))
q= A1*F*e1*s*((T+460)^4-(T1+460)^4)
//RESULTS
printf ('Heat loss from the conduit by radiation = %.f Btu/hr per ft',q)
|
2585cb559693cc461aaedadb367507e4414214c6 | 449d555969bfd7befe906877abab098c6e63a0e8 | /608/CH33/EX33.08/33_08.sce | 0669f2cb5c913da87c04dbd53ff018dfe424abeb | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,740 | sce | 33_08.sce | //Problem 33.08: For the a.c. bridge network shown in Figure 33.35, determine the current flowing in the capacitor, and its direction, by using Th´evenin’s theorem. Assume the 306/_0° V source to have negligible internal impedance.
//initializing the variables:
rv = 30; // in volts
thetav = 0; // in degrees
R1 = 15; // in ohm
R2 = 40; // in ohm
R3 = %i*20; // in ohm
R4 = 20; // in ohm
R5 = %i*5; // in ohm
R6 = 5; // in ohm
R7 = -1*%i*25; // in ohm
//calculation:
//voltage
V = rv*cos(thetav*%pi/180) + %i*rv*sin(thetav*%pi/180)
//The R7 is initially removed from the network, as shown in Figure 33.36
Z1 = R1
Z2 = R2
Z3 = R3 + R4
Z4 = R5 + R6
//P.d. between A and C,
Vac = (Z1/(Z1 + Z4))*V
//P.d. between B and C,
Vbc = (Z2/(Z2 + Z3))*V
//Assuming that point A is at a higher potential than point B, then the p.d. between A and B is
Vab = Vac - Vbc
//the open-circuit voltage across AB is given by
E = Vab
//Point C is at a potential of V . Between C and A is a volt drop of Vac. Hence the voltage at point A is
Va = V - Vac
//Between points C and B is a voltage drop of Vbc. Hence the voltage at point B
Vb = V - Vbc
//Replacing the V source with a short-circuit (i.e., zero internal impedance) gives the network shown in Figure 33.37(a). The network is shown redrawn in Figure 33.37(b) and simplified in Figure 33.37(c). Hence the impedance, z, ‘looking in’ at terminals AB is given by
z = Z1*Z4/(Z1 + Z4) + Z2*Z3/(Z2 + Z3)
//The Th´evenin equivalent circuit is shown in Figure 33.38, where current I is given by
I = E/(z + R7)
Imag = (real(I)^2 + imag(I)^2)^0.5
printf("\n\n Result \n\n")
printf("\n the current flowing in the capacitor is %.3f A in direction from B to A.",Imag) |
6526d80ee803e51415edea551a6bfb9bbf3e4a28 | 463377b6374a24bbe111707a34e24949f3bd2543 | /iv4.sci | 32fd7780ab04eb08b7bfa0e9b0c5684427c6dcce | [] | no_license | solothinker/Scilab-Identification | 3a46c0f3b8b1a7430f8a799be5e1310e2723b535 | cdad0d7292c31c29d377b640f6966a7c3bb81bb9 | refs/heads/master | 2022-01-05T12:39:07.410803 | 2019-06-15T02:18:13 | 2019-06-15T02:18:13 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 2,519 | sci | iv4.sci | function varargout = iv4(varargin)
[lhs, rhs] = argn(0)
plantData = varargin(1)
orderData = varargin(2)
na = orderData(1);nb = orderData(2)
// arranging na ,nb,nk
if size(orderData,"*") == 2 then
nk = 1
elseif size(orderData,'*') == 3 then
nk = orderData(3)
end
nb1 = nb + nk - 1
n = max(na, nb1)
// arranging the plant data
if typeof(plantData) == 'constant' then
Ts = 1;unitData = 'second'
elseif typeof(plantData) == 'iddata' then
Ts = plantData.Ts;unitData = plantData.TimeUnit
plantData = [plantData.OutputData plantData.InputData]
end
noOfSample = size(plantData,'r')
// finding the iv model
ivTest = iv(plantData,[na nb nk]);
// residual
[aTemp,bTemp,cTemp] = pe(plantData,ivTest);
Lhat = ar(aTemp,na+nb);
x = sim(plantData(:,2),ivTest);
yData = plantData(:,1);uData = plantData(:,2)
Yf = filter(Lhat.a,Lhat.b,[plantData(:,1);zeros(n,1)]);
phif = zeros(noOfSample,na+nb)
psif = zeros(noOfSample,na+nb)
// arranging samples of y matrix
for ii = 1:na
phif(ii+1:ii+noOfSample,ii) = -yData
psif(ii+1:ii+noOfSample,ii) = -x
end
// arranging samples of u matrix
for ii = 1:nb
phif(ii+nk:ii+noOfSample+nk-1,ii+na) = uData
psif(ii+nk:ii+noOfSample+nk-1,ii+na) = uData
end
// passing it through the filters
for ii = 1:na+nb
phif(:,ii) = filter(Lhat.a,Lhat.b,phif(:,ii));
psif(:,ii) = filter(Lhat.a,Lhat.b,psif(:,ii));
end
lhs = psif'*phif
lhsinv = pinv(lhs)
theta = lhsinv * (psif)' * Yf
ypred = (phif * theta)
ypred = ypred(1:size(yData,'r'))
e = yData - ypred
sigma2 = norm(e)^2/(size(yData,'r') - na - nb)
vcov = sigma2 * pinv((phif)' * phif)
t = idpoly([1; theta(1:na)],[zeros(nk,1); theta(na+1:$)],1,1,1,Ts)
// estimating the other parameters
[temp1,temp2,temp3] = predict(z,t)
[temp11,temp22,temp33] = pe(z,t)
estData = calModelPara(temp1,temp11,na+nb)
//pause
t.Report.Fit.MSE = estData.MSE
t.Report.Fit.FPE = estData.FPE
t.Report.Fit.FitPer = estData.FitPer
t.Report.Fit.AIC = estData.AIC
t.Report.Fit.AICc = estData.AICc
t.Report.Fit.nAIC = estData.nAIC
t.Report.Fit.BIC = estData.BIC
t.TimeUnit = unitData
//sys = t
varargout(1) = t
//varargout(1) = idpoly([1; -theta(1:na)],[zeros(nk,1); theta(na+1:$)],1,1,1,Ts)
endfunction
|
6f376c3a0f4370eb2e913289036df8fa48ca45ad | 449d555969bfd7befe906877abab098c6e63a0e8 | /3808/CH6/EX6.11/Ex6_11.sce | e16105aabe8ff0265f9fe54d290619ad56a7deff | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 783 | sce | Ex6_11.sce | //Chapter 06: Counting
clc;
clear;
function result=combination(n,r) //function definition
i=n
num=1
denominator=1
l=(n-r)+1
u=n
for i=l:u //to compute the value of the numerator
num=num*i
end
for j=1:r //to compute the value of the denominator
denominator=denominator*j
end
result=num/denominator
return result
endfunction
//Part A Solution
num=input("Enter the number of cards in the deck(For standard deck n=52):")
com1=input("Enter the number of cards for poker hands determination:")
com2=input("Enter the number of cards to select no of ways:")
res1=combination(num,com1)
mprintf("The number of poker hands of %d cards that can be dealt are %d ",com1,res1)
res2=combination(num,com2)
mprintf("\nThe number of ways to select %d cards from a standard deck are %d ",com2,res1)
|
953670d073025f2d1b81f3b862633b4cded3304b | 449d555969bfd7befe906877abab098c6e63a0e8 | /2414/CH19/EX19.2/Ex19_2.sce | cf34aefb6d38e745bbbc61098c3baccda6539741 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 278 | sce | Ex19_2.sce | clc;
close();
clear();
//page no 605
//prob no. 19.2
b=[0 23 62 8 43 16 71 47 19 61]
for i=1:10
f9(i)=[b(i)+9]+2
if f9(i)>79 then
f9(i)=f9(i)-79
end
mprintf('\nFor i=%i ,b(i)=%i. Therefore.f9(%i)=[%i+9]mod(79)+2=%i',i,b(i),i,b(i),f9(i))
end
|
28d37c694e166ca184877997bdaa981ce9fb16ed | e0124ace5e8cdd9581e74c4e29f58b56f7f97611 | /3913/CH6/EX6.2/Ex6_2.sce | 52f5688f91944ed5aa928c10cef131e8be65cae2 | [] | no_license | psinalkar1988/Scilab-TBC-Uploads-1 | 159b750ddf97aad1119598b124c8ea6508966e40 | ae4c2ff8cbc3acc5033a9904425bc362472e09a3 | refs/heads/master | 2021-09-25T22:44:08.781062 | 2018-10-26T06:57:45 | 2018-10-26T06:57:45 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 644 | sce | Ex6_2.sce | //Chapter 6 : Linear Mappings
//Example 6.12
//Scilab 6.0.1
//Windows 10
clear;
clc;
A=[1 0 1;1 1 2;2 1 3];
B=['a','']
disp(A,'A=')
A(2,:)=A(2,:)-1*A(1,:)
A(3,:)=A(3,:)-2*A(1,:)
A(3,:)=A(3,:)-1*A(2,:)
disp(A,'Hermite form of A=')
mprintf('\n(a,b,c) belongs to Im f only if c=a+b')
mprintf('\n(x,y,z) belongs to Ker f only if')
mprintf('\nx+z=0')
mprintf('\nx+y+2z=0')
mprintf('\n2x+y+3z=0')
mprintf('\nfor Ker f tobe zero subspace system needs to have unique solution-(0,0,0)')
mprintf('\nBut from above Hermite form coefficient matrix has rank 2, so non-trivial solutions exist')
mprintf('\nHence f is not injective')
|
f9e50474db2ca67c22d7e3bc5a6b1aecb9fe0ad9 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1892/CH1/EX1.3/Example1_3.sce | 2aa9445b78cc139c1c5cc670a81ae65d608c2b56 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 263 | sce | Example1_3.sce | // Example 1.3
clear; clc; close;
format('v',6);
// Given data
P=4;//No. of poles
f=50;//in Hz
N=1470;//in rpm
//Calculations
Ns=120*f/P;//in rpm
S=(Ns-N)/Ns;//Slip
fr=S*f;//induced emf frequency in Hz
disp(fr,"Induced emf frequency in Hz : ");
|
86202a5897309119155e54110ec99124bbfa0601 | 449d555969bfd7befe906877abab098c6e63a0e8 | /764/CH7/EX7.9.a/data7_9.sci | 2820dafc48e77013d9a4f304a30aaccd2969ff6e | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 343 | sci | data7_9.sci |
//(Threaded Joints)Example 7.9
//Refer Fig.7.24 on page 240
//Number of bolts N
N = 4
//Load supported by the bracket P (kN)
P = 25
//Distance of bolt1 from C l1 (mm)
l1 = 50
//Distance of bolt2 from C l2 (mm)
l2 = 200
//Eccentricity value l (mm)
l = 400
//Permissible tensile stress in the bolt sigmaMax (N/mm2)
sigmaMax = 50
|
f6b3033a2954cc0b831b1d1f720fb4db7e5a8cd9 | 449d555969bfd7befe906877abab098c6e63a0e8 | /181/CH2/EX2.20/example2_20.sce | a41da47f379443caaa37d379071018ad038356b2 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 460 | sce | example2_20.sce | // Leakage resistance shunting the diode
// Basic Electronics
// By Debashis De
// First Edition, 2010
// Dorling Kindersley Pvt. Ltd. India
// Example 2-20 in page 99
clear; clc; close;
// Given data
// Kirchoff's law has been applied and equations solved to get final expression
// Calculation
I_R=(0.08*5*10^-6)/0.15;
R=10/I_R;
printf("Leakage resistance = %0.2e Mohm",R);
// Result
// Leakage resistance shunting the diode = 3.75 Mohm |
d9223fb7d229207b5b3f8413c5dbc51975a7a7a7 | 0fea4b1807b35c0ef50433aa99f483c2de5777df | /assignment 2/assignment2_2(4 fundamental sub spaces).sce | a831ce51ead7bbff55829d6b47735475e2dca85b | [] | no_license | shivansh8/Scilab | 319fdfcbec1cc24b4c3c9d4385112ade99419c73 | 7922ffe14c554718cc7682b6419db9bce8261213 | refs/heads/master | 2020-12-29T06:10:48.542794 | 2020-04-05T14:19:06 | 2020-04-05T14:19:06 | 238,486,140 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 808 | sce | assignment2_2(4 fundamental sub spaces).sce | //clear ;close;clc;
str = input("Enter a space-separated 3x3 matrix in this order a11 a12 a13 .a32 33 ", "string")
v = evstr(strsplit(str, " "))
a11=v(1)
a12=v(2)
a13=v(3)
a21=v(4)
a22=v(5)
a23=v(6)
a31=v(7)
a32=v(8)
a33=v(9)
A=[a11 a12 a13;a21 a22 a23;a31 a32 a33];
function ffss(A)
disp(A,"A=");
[m,n]=size(A);
disp(m,"m=");
disp(n,"n=");
[vv,pivot]=rref(A);
//disp(vv,pivot,"vv-pivot:");
//
disp(rref(A),"rref(a)");
disp(vv,"vv");
r=length(pivot);
disp(r,"rank=");
coluspa=A(:,pivot);
disp(coluspa,"column space=");
nullspa=kernel(A);
disp(nullspa,"null space=");
rowspa=vv(1:r,:)';
disp(rowspa,"rowspace=");
leftnspa=kernel(A');
disp(leftnspa,"left null spaec=");
endfunction
ffss(A);
|
e41d630151f4897740e8d88ee4fd57baa6ff9d03 | 8217f7986187902617ad1bf89cb789618a90dd0a | /browsable_source/2.5/Unix-Windows/scilab-2.5/demos/sci2for/dem4.sce | 0dd9fd1a01805d278291bd0ca7931e3d7df6f333 | [
"LicenseRef-scancode-public-domain",
"LicenseRef-scancode-warranty-disclaimer"
] | permissive | clg55/Scilab-Workbench | 4ebc01d2daea5026ad07fbfc53e16d4b29179502 | 9f8fd29c7f2a98100fa9aed8b58f6768d24a1875 | refs/heads/master | 2023-05-31T04:06:22.931111 | 2022-09-13T14:41:51 | 2022-09-13T14:41:51 | 258,270,193 | 0 | 1 | null | null | null | null | UTF-8 | Scilab | false | false | 430 | sce | dem4.sce | // function definition
// Copyright INRIA
deff('[x]=t4(a,n)',[
'[lhs,rhs]=argn(0),'
'[m,n]=size(a),'
'if m==n then error(''incorrect dimensions ''),end,'
'x=sin(a),'
'u=norm(x),'
'if u==%eps then x=x/u,end,'],'n')
// define type and dimension of the input args
lt4=list();
lt4(1)=list('1','m1','n1');
// show the initial data
printspecs(t4,lt4)
//translate
txt=sci2for(t4,'t4',lt4);
message(['Generated Fortran code';' ';txt])
|
6d9cf5d4ebafc61687e15745fbf5718ce8a3660a | 1ebbdce5d3f3daa6d9e8b439410e447941bc49f5 | /résolution numérique/script2.sce | 94851cfcac1de6d891b6ff4dc8b0661a2cfe3579 | [] | no_license | sebastienbaur/legionella_proliferation_modeling | 2aff0e2499584e99c07116a700e43218976b9b12 | ae9b5d4dde1912a98584c6319eae41980355ef03 | refs/heads/master | 2020-03-07T15:25:49.881820 | 2018-03-31T17:27:52 | 2018-03-31T17:27:52 | 127,554,634 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 6,777 | sce | script2.sce | // -----------------------------------------------------------------------------
// VALEURS NUMERIQUES DES CONSTANTES DU PROBLEME
// -----------------------------------------------------------------------------
// constantes de Monod :
k_1 = 100*10^(-5) ; // constante de vitesse légionnelle-nutriment
k_2 = 2*10^(-4) ;
k_3 = 100*10^(-5) ; // constante de vitesse légionnelle-amibe
k_4 = 2*10^(-4) ;
k_5 = 100*10^(-5) ; // constante de vitesse amibe-nutriment
k_6 = 2*10^(-4) ;
// masses volumiques
rho_A = 1;
rho_L = 1;
// coefficient de diffusion
D = 10^(-10);
// coefficient d'arrachement
lambda = 0;
// flux à la limite supérieure de substrat
phi_0 = 1;
// discrétisation du temps et de l'espace
N = 2000*201;
M = 100;
T = 2000;
L = 10^(-6)*M;
t = linspace(0,T,N+1);
z = linspace(0,L,M+1);
dt = t(2) - t(1);
dz = z(2) - z(1);
// VALEURS INITIALES DES VARIABLES, à t = 0
tCourant = 0;
L0 = zeros(M,1);
L0(1) = 1/2 ;// valeur du vecteur légionnelle à l'instant initial
L0(2)=1/2;
L0(3)=1/2;
L0(4)=1/2;
LCourant = l0;
LAvant = l0;
A0 = zeros(M,1); // valeur du vecteur amibe à l'instant initial
A0(1) = 1/2 ;
A0(2)=1/2;
A0(3)=1/2;
A0(4) = 1/2;
ACourant = A0;
AAvant = A0;
S0 = 100*ones(M,1);
//S0 = zeros(M,1); // valeur du vecteur substrat à l'instant initial
//S0(1,1) = 100;
//S0(2,1) = 100;
SCourant = S0;
//e0 = dz; // épaisseur initiale
//eCourant = e0;
vitesse0 = zeros(M,1);
// vitesse0(1)=10^(-8);
vitesseCourante = vitesse0;
multiplieur = ones(1,M);
m_L = [];
m_A = [];
m_S = [];
m_L_relatif = [];
m_A_relatif = [];
m_S_relatif = [];
// remarque : ci-dessous, la composante de la i_ème ligne, j_ème colonne des matrices l, a, S, et V donne les valeurs de l, a, S et V en z_i, à l'instant t_j
// remarque2 : ci-dessous, le vecteur ligne E contient à la j_ème colonne la valeur de l'épaisseur du biofilm à l'instant t_j
L = [L0];
A = [A0];
S = [S0];
V = [vitesse0];
//E = [e0];
m_L = [m_L dz*10^(-4)*(L(1,1)+L(2,1))];
m_A = [m_A dz*10^(-4)*(A(1,1)+A(2,1))];
m_S = [m_S dz*10^(-4)*(S(1,1)+S(2,1))];
m_L_relatif = [1];
m_A_relatif = [1];
m_S_relatif = [1];
// -----------------------------------------------------------------------------
// QUELQUES MATRICES UTILES DANS LES CALCULS
// -----------------------------------------------------------------------------
one = ones(M,1); // vecteur colonne à M lignes qui ne contient que des 1
anotherOne = ones(M-1,1);
identity = diag(one,0); // matrice identité de taille M
surDiag = diag(anotherOne,1); // matrice carrée de taille M dont la surdiagonale ne contient que des 1, le reste est nul
sousDiag = diag(anotherOne,-1); // matrice carrée de taille M dont la sousdiagonale ne contient que des 1, le reste est nul
matriceDeriveePremiere = identity - sousDiag;
matriceDeriveePremiere(1,1) = 0;
matriceDeriveeSeconde = -2*identity + surDiag + sousDiag;
matriceDeriveeSeconde(1,1) = 0;
matriceDeriveeSeconde(1,2) = 0;
matriceDeriveeSeconde(M,M) = 0;
matriceDeriveeSeconde(M,M-1) = 0;
matriceVitesse = identity;
for i = 1 : M
matriceVitesse = matriceVitesse + surDiag^i;
end
matriceVitesse = matriceVitesse';
i=-1;
// -----------------------------------------------------------------------------
// BOUCLE QUI CALCULE LES DIFFERENTES VALEURS DES LEGIONNELLES, AMIBES, SUBSTRATS, VITESSE, ET EPAISSEUR DU BIOFILM
// -----------------------------------------------------------------------------
while (tCourant < T)
i=i+1;
// calcul des valeurs des légionnelles, amibes, et substrats à l'instant j pour les différentes abscisses z_i
LCourant = LCourant + dt * (monodL(SCourant, LCourant, ACourant).*LCourant - (1/dz) * matriceDeriveePremiere * (vitesseCourante .* LCourant));
// lCourant = lCourant + dt * (monodL(SCourant, lCourant, aCourant) - deriveeVitesse(SCourant, lCourant, aCourant)) .* lCourant - dt * vitesseCourante.*((1/dz)*matriceDeriveePremiere*lCourant);
LCourant(1,1) = LCourant(2,1);
ACourant = ACourant + dt * (monodA(SCourant, LAvant, ACourant).*ACourant - (1/dz) * matriceDeriveePremiere * (vitesseCourante .* ACourant));
// aCourant = aCourant + dt * (monodA(SCourant,l(:,$),aCourant) - deriveeVitesse(SCourant,l(:,$),aCourant)) .* aCourant - dt*vitesseCourante.*((1/dz)*matriceDeriveePremiere*aCourant);
ACourant(1,1) = ACourant(2,1);
SCourant = SCourant + dt * (D * (1/(dz*dz) ) * (matriceDeriveeSeconde * SCourant) + consoNutri(SCourant,LAvant,AAvant)); //.* SCourant);
SCourant(1,1) = SCourant(2,1);
SCourant(M,1) = 100;
// calcul de l'épaisseur grâce à la condition à la limite de/dt = -lambda e^2 + u(t,e(t))
// indiceEpaisseur = round(eCourant/dz);
// eCourant = eCourant + dt * (-lambda * eCourant^2 + vitesseCourante(indiceEpaisseur,1) );
// calcul de la vitesse
vitesseCourante = dz * matriceVitesse * deriveeVitesse(SCourant,LCourant,ACourant);
// incrémentation du temps
tCourant = tCourant + dt;
// troncage des vecteurs au delà de l'épaisseur du biofilm
// for i = indiceEpaisseur+1:M
// lCourant(i,1)=0;
// aCourant(i,1)=0;
// SCourant(i,1)=0;
// end
// conditions limites : flux nul aux interfaces
// aCourant(1,1)=aCourant(2,1);
// lCourant(1,1)=lCourant(2,1);
// SCourant(1,1)=SCourant(2,1);
// aCourant(indiceEpaisseur,1)=aCourant(indiceEpaisseur-1,1);
// lCourant(indiceEpaisseur,1)=lCourant(indiceEpaisseur-1,1);
// SCourant(indiceEpaisseur,1)=SCourant(indiceEpaisseur-1,1);
// enregistrement des nouvelles valeurs des grandeurs observées
if modulo(i,1000) == 0 then
A = [A aCourant];
L = [L lCourant];
S = [S SCourant];
// E = [E eCourant];
V = [V vitesseCourante];
m_A = [m_A dz*10^(-4)*multiplieur*ACourant];
m_S = [m_S dz*10^(-4)*multiplieur*SCourant];
m_L = [m_L dz*10^(-4)*multiplieur*LCourant];
m_L_relatif = [m_L_relatif m_L(1,i/1000+2)/m_L(1,1)];
m_A_relatif = [m_A_relatif m_A(1,i/1000+2)/m_A(1,1)];
m_S_relatif = [m_S_relatif m_S(1,i/1000+2)/m_S(1,1)];
end
AAvant = ACourant;
LAvant = LCourant;
// permet de tomber pile sur T à la fin
dt = min(dt, T - tCourant);
end
//plot2d(linspace(0,T,N+2)',[m_S(1,:)',m_L(1,:)',m_A(1,:)'],leg = "m_S@m_L@m_A");
//xtitle("avec amibes","t (en s)","m (en kg)")
//plot2d(linspace(0,T,N+1)',[m_S_relatif(1,:)',m_L_relatif(1,:)',m_A_relatif(1,:)'],leg="m_S@m_L@m_A");
//xtitle("évolution temporelle des masses relatives avec amibes","t (en s)","m/m0 (sans unité)");
//plot2d(linspace(0,T,N+2)',[S(1,:)',S(5,:)',S(7,:)',S(10,:)',S(12,:)',S(13,:)'],leg="z=0@z=5@z=7@z=10@z=12@z=13", rect = [0,0,1000,0.4]);
//xtitle("évolution temporelle de S(z,t) à différents z, ","t (en s)","C_s (en g/L)");
|
53875fd338168535a7bb382f603543d5aa6a6a01 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2969/CH4/EX4.18/Ex4_18.sce | 683a454b482dd8f75c6ec95e8b3ff8a009454b79 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,149 | sce | Ex4_18.sce | clc
clear
//DATA GIVEN
m=1; //mass of steam in kg
p=20; //pressure of steam in bar
Tsup=400+273; //temp. of steam in K
x=0.9; //dryness fraction
Cps=2.3; //specific heat of steam in kJ/kgK
//At 20 bar, from steam tables
Ts=212.4+273; //in K
hf=908.6; //kJ/kg
hfg=1888.6; //kJ/kg
vg=0.0995; //m^3/kg
hsup=hf+hfg+Cps*(Tsup-Ts); //kJ/kg
//Assume superheated steam to behave as a perfect gas from the commencement of superheating and thus obey Charle's Law
//By vg/Ts=vsup/Tsup
vsup=vg*Tsup/Ts;
usup=hsup-p*10^5*vsup*10^-3; //internal energy of 1 kg of superheated steam in kJ/kg
h=hf+x*hfg;
u=h-p*10^5*x*vg*10^-3; //internal energy of 1 kg of wet steam in kJ/kg
printf('(i) The Internal energy of 1 kg of superheated steam at 400 deg celsius is: %4.2f kJ/kg. \n',usup);
printf('(ii) The Internal energy of 1 kg of wet steam with dryness fraction 0.9 is: %4.2f kJ/kg. \n',u);
|
d438acee8149d919dd055fd937fc0d02666ece83 | 449d555969bfd7befe906877abab098c6e63a0e8 | /587/CH4/EX4.9/example4_9.sce | 8cd7a2a9928359c89bac6206eb41eed02fbd1955 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,086 | sce | example4_9.sce | clear;
clc;
//Example4.9[Heat transfer from a Short Cylinder]
//Given:-
Ti=120;//Initial Temperature[degree Celcius]
T_ambient=25;//Temperature of atmospheric air[degree Celcius]
rho=8530;//density of brass cyliner[kg/m^3]
Cp=0.380;//Specific heat of brass cylinder[kJ/kg.degree Celcius]
r=0.05;//radius[m]
H=0.12;//Height of cylinder[m]
h=60;//convetcion heat transfer coefficient[W/m^2.degree Celcius]
a=3.39*(10^(-5));//Diffusivity of brass [m^2/s]
k=110;//Thermal conductivity of brass[W/m.degree Celcius]
L=0.06;//[m]
t=900;//[seconds]
//Solution:-
m=rho*(%pi*(r^2)*H);//mass of cylinder[kg]
Q_max=m*Cp*(Ti-T_ambient);//[kJ]
disp("At the center of the plane wall")
tau1=(a*t)/(L^2);
Bi1=(h*L)/k;
x=(Bi1^2)*tau1;
//For given x and Bi1
p=0.23;//(Q/Qmax) for plane wall
disp("At the center of the cylinder")
tau2=(a*t)/(r^2);
Bi2=(h*r)/k;
y=(Bi2^2)*tau2;
//For given y and Bi2
q=0.47;//(Q/Qmax) for infinite cylinder
Q=Q_max*(p+(q*(1-p)));//[kJ]
disp("kJ",ceil (Q),"The total heat transfer from the cylinder during the first 15 minutes of cooling is") |
0a37fcd3c284dfecdee6d5aa3753993647dfb2ca | d167200e784b8019615f6b37b5a46b91ec43b98d | /macros/histogramCostExtractor.sci | 37b81fa7b8b23dd57999221a5e549687a52b87c7 | [] | no_license | AshishMantosh/FOSSEE-Image-Processing-Toolbox | ee9c1a00f97627f372fae1d7d851c4905ac9d83e | e4fbe1891e13e4dc9b62513f0aef2b101638f084 | refs/heads/master | 2021-01-01T19:05:15.966438 | 2017-07-27T07:16:11 | 2017-07-27T07:16:11 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 3,098 | sci | histogramCostExtractor.sci | // Copyright (C) 2015 - IIT Bombay - FOSSEE
//
// This file must be used under the terms of the CeCILL.
// This source file is licensed as described in the file COPYING, which
// you should have received as part of this distribution. The terms
// are also available at
// http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt
// Author: Ashish Manatosh Barik & Shubham Lohakare
// Organization: FOSSEE, IIT Bombay
// Email: toolbox@scilab.in
//
function [costMat] = histogramCostExtractor(srcImg1, srcImg2, typeOfMethod, hessianThreshold, varargin)
// This function computes the cost matrix.
//
// Calling Sequence
// [ costMatrix ] = histogramCostExtractor(srcImg1, srcImg2, typeOfMethod=3, hessianThreshold); // Norm based cost
// [ costMatrix ] = histogramcostExtractor(srcImg1, srcImg2, typeOfMethod=1, hessianThreshold, nDummies, defaultCost); // Chi as well as EMDL1 based cost extraction
// [ costMatrix ] = histogramCostExtractor(srcImg1, srcImg2, typeOfMethod=2, hessianThreshold, nDummies, defaultCost); // EMDL1 based cost extraction
//
// Parameters
// srcImg1 : It is the first input image.
// srcImg2 : It is the second input image.
// typeOfMethod : It is used as a flag to pick a certain type of transformation. Use value '1' for 'Chi based cost ectraction', '2' for 'EMDL1 based cost extraction' and '3' for 'Norm based cost extraction'. It is of double type.
// hessianThreshold : It is the threshold value for Hessian keypoint detector in SURF(Speeded-Up Robust Features). It is of double type.
// rpTPS : It is used to set the regularization parameter for relaxing the exact interpolation requirements of the TPS algorithm. It is of double type.
// costMatrix : It is the cost matrix.
//
// Description
// This function is used to calculate the histogram based cost matrix of two images, the user gets to choose and apply the type of transformation she/he wishes to perform.
//
// Examples
// // Chi based cost extraction
// a= imread("/images/n.jpeg");
// b= imread("/images/n1.jpeg");
// typeOfMethod=1;
// hessianThreshold=5000;
// nDummies=25;
// defaultCost=0.2;
// c=histogramCostExtractor(a,b,typeOfMethod,hessianThreshold,nDummies,defaultCost);
//
// Examples
// // EMDL1
// a = imread("/images/n.jpeg");
// b = imread("/images/n1.jpeg");
// typeOfMethod=2;
// hessianThreshold=5000;
// nDummies=25;
// defaultCost=0.2;
// c=histogramCostExtractor(a,b,typeOfMethod,hessianThreshold,nDummies,defaultCost);
//
// Examples
// Norm based cost extraction
// a = imread("/images/n.jpeg");
// b= imread("/images/n1.jpeg");
// typeOfMethod=3;
// hessianThreshold=5000;
// c=histogramCostExtractor(a,b,typeOfMethod,hessianThreshold);
//
// Authors
// Ashish Mantosh Barik, NIT Rouekela
// Shubham Lohakare, NITK Surathkal
srcMat1 = mattolist(srcImg1)
srcMat2 = mattolist(srcImg2)
[lhs, rhs] = argn(0)
select rhs
case 4 then
costMat = raw_histogramCostExtractor(srcMat1, srcMat2, typeOfMethod, hessianThreshold)
case 6 then
costMat = raw_histogramCostExtractor(srcMat1, srcMat2, typeOfMethod, hessianThreshold, varargin(1), varargin(2))
end
endfunction
|
b4363dcbc4c731cee3d0ddaa87041ec66f934d81 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2258/CH7/EX7.23/7_23.sce | 9e0ec3ba03cc56ac392399e4bf4020d756283284 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 727 | sce | 7_23.sce | clc();
clear;
// To calculate the probability of occupation
Eg=0.4; //energy gap in eV
Eg=Eg*1.6*10^-19; //Eg in J
KB=1.38*10^-23;
T1=0; //temp 1 in C
T1k=T1+273; //temp 1 in K
T2=50; //temp 2 in C
T2k=T2+273; //temp 2 in K
T3=100; //temp 3 in C
T3k=T3+273; //temp 3 in K
//F(E) = 1/(1+(exp((E-Ep)/(KB*T))))
//but E-Ep = (1/2)*Eg
//therefore F(E) = 1/(1+(exp(Eg/(2*KB*T))))
FE1=1/(1+(exp(Eg/(2*KB*T1k))));
FE2=1/(1+(exp(Eg/(2*KB*T2k))));
FE3=1/(1+(exp(Eg/(2*KB*T3k))));
printf("probability of occupation at 0 C is %f eV",FE1);
printf("probability of occupation at 50 C is %f eV",FE2);
printf("probability of occupation at 100 C is %f eV",FE3);
//answers given in the book are wrong
|
727b7f12d93da1989c11d25a6e43028de52577ca | 1b969fbb81566edd3ef2887c98b61d98b380afd4 | /Rez/bivariate-lcmsr-post_mi/bfi_c_vrt_ind_d/~BivLCM-SR-bfi_c_vrt_ind_d-PLin-VLin.tst | b290db5ad010b5b8599c6d0f4b4818ebe9a3cd6e | [] | no_license | psdlab/life-in-time-values-and-personality | 35fbf5bbe4edd54b429a934caf289fbb0edfefee | 7f6f8e9a6c24f29faa02ee9baffbe8ae556e227e | refs/heads/master | 2020-03-24T22:08:27.964205 | 2019-03-04T17:03:26 | 2019-03-04T17:03:26 | 143,070,821 | 1 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 11,974 | tst | ~BivLCM-SR-bfi_c_vrt_ind_d-PLin-VLin.tst |
THE OPTIMIZATION ALGORITHM HAS CHANGED TO THE EM ALGORITHM.
ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES
1 2 3 4 5
________ ________ ________ ________ ________
1 0.301485D+00
2 -0.221252D-02 0.231236D-02
3 0.394841D-01 -0.837124D-03 0.397353D+00
4 -0.176945D-03 0.291453D-03 -0.706293D-02 0.333983D-02
5 -0.735319D-03 0.876981D-04 -0.552912D-04 0.843613D-04 0.365544D-02
6 0.527528D-03 -0.118513D-04 -0.274768D-04 0.420786D-04 -0.123324D-03
7 -0.475399D-03 0.213067D-03 -0.151564D-02 0.123607D-03 0.454245D-03
8 0.494839D-03 -0.366464D-04 0.865511D-03 0.163463D-03 0.723594D-04
9 -0.325959D+00 0.119456D-01 0.173246D+00 -0.124370D-01 0.412565D-01
10 -0.180682D+00 -0.108869D-01 0.180438D+00 -0.227917D-02 0.114404D+00
11 -0.194686D+00 -0.313969D-02 0.588615D-01 0.155192D-02 0.283151D-01
12 -0.500729D-01 0.659084D-02 0.108522D+00 -0.629590D-01 0.475208D-01
13 0.110248D-01 0.112846D-01 -0.770802D-01 0.101228D-02 -0.809044D-02
14 0.118044D+00 0.897691D-02 0.289107D+00 0.246879D-01 0.207612D-01
15 -0.224117D+01 -0.308939D-01 -0.412642D+00 -0.139145D-01 -0.120238D+00
16 -0.628644D-01 -0.231032D-02 -0.163248D-02 -0.362730D-02 -0.134336D-02
17 0.980339D-02 -0.509771D-03 -0.179539D-02 0.185593D-03 -0.393320D-03
18 -0.433940D+00 -0.285536D-01 0.100889D+00 -0.673945D-01 0.125420D-01
19 -0.560470D-01 0.461550D-02 0.448608D-01 -0.766984D-02 0.649420D-02
20 0.271943D+00 -0.322078D-01 -0.734757D+00 -0.826652D-01 -0.577531D-01
21 0.536752D-01 -0.995834D-02 -0.322990D-01 0.335292D-02 -0.484731D-02
22 -0.332338D-03 0.213125D-03 -0.212735D-02 0.628293D-03 -0.489752D-03
23 0.188404D-01 -0.372474D-02 0.715798D-02 -0.435821D-03 0.412489D-03
24 -0.442235D-02 0.476332D-03 0.430465D-02 0.120739D-02 0.204755D-03
ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES
6 7 8 9 10
________ ________ ________ ________ ________
6 0.647687D-03
7 0.700544D-03 0.370454D-02
8 -0.163746D-03 -0.105080D-03 0.289547D-02
9 0.154721D-01 0.278202D-01 -0.430236D-02 0.451493D+02
10 -0.587127D-02 -0.117560D-02 0.931840D-03 0.431802D+01 0.190062D+02
11 0.461002D-01 0.853273D-01 0.149001D-01 0.904576D+01 0.207893D+01
12 -0.178427D-01 0.213415D-01 0.854316D-01 0.922738D+01 0.158149D+01
13 0.434451D-01 0.115367D+00 -0.164538D-01 0.169918D+01 -0.174429D+01
14 -0.118254D-01 0.145830D-01 0.252580D+00 0.103875D+01 0.243402D+01
15 -0.168995D-01 -0.420198D-01 -0.345231D-01 -0.937764D+01 -0.113644D+02
16 0.475886D-03 0.301481D-03 -0.186020D-02 0.808124D+00 -0.171300D+00
17 -0.820377D-05 -0.252804D-03 0.275230D-03 -0.159571D+00 0.640703D-03
18 -0.342595D-01 -0.117624D+00 -0.209386D-02 -0.540051D+01 0.183176D+01
19 -0.132194D-01 0.292920D-02 -0.866586D-02 -0.131613D+01 -0.151679D+00
20 0.245738D-01 0.141183D-01 -0.251422D+00 -0.628280D+01 0.105010D+01
21 0.128828D-01 -0.221326D-02 0.801634D-02 0.124337D+01 0.350138D+00
22 -0.100739D-03 -0.178679D-03 0.117320D-03 -0.603405D-03 -0.403349D-01
23 0.115564D-03 -0.453274D-03 -0.196390D-02 -0.299152D-01 -0.509440D-01
24 -0.361741D-04 0.887152D-05 -0.565823D-04 0.175602D-01 0.848915D-02
ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES
11 12 13 14 15
________ ________ ________ ________ ________
11 0.476165D+02
12 0.605115D+01 0.195184D+03
13 0.130393D+00 -0.552781D+00 0.121561D+02
14 0.437584D+01 0.139552D+02 -0.183445D+01 0.857935D+02
15 -0.155553D+01 -0.965630D+00 -0.118515D+01 0.320444D+01 0.242730D+03
16 -0.413592D-01 0.865779D-01 0.840857D-01 -0.166793D+00 0.178494D+01
17 -0.132052D-01 -0.372627D-01 -0.558462D-02 -0.173949D-01 -0.104085D+01
18 -0.645868D+01 -0.302012D+01 -0.471956D+01 0.209803D+01 0.308232D+02
19 -0.136927D+01 0.129751D+01 -0.239586D+00 -0.305325D+01 0.200318D+01
20 -0.833756D+01 -0.243079D+02 0.701557D+00 -0.573637D+02 0.756979D+01
21 0.246739D+01 -0.151278D+01 0.236935D+00 0.341252D+01 -0.160525D+01
22 -0.878060D-01 -0.450480D-02 -0.435079D-02 -0.353468D-01 -0.103261D+00
23 -0.706304D-01 0.963369D+00 -0.613934D-01 -0.175059D+00 -0.767887D+00
24 0.681705D-02 -0.251505D+00 0.292051D-02 0.531940D-01 0.784886D-01
ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES
16 17 18 19 20
________ ________ ________ ________ ________
16 0.454114D+00
17 -0.202871D-01 0.136104D-01
18 0.268614D+00 -0.962871D-01 0.179308D+03
19 0.628320D-01 -0.148755D-02 0.417507D+01 0.525212D+01
20 -0.270833D+00 0.411314D-01 0.264754D+02 -0.114095D+01 0.384834D+03
21 0.164146D+00 -0.273330D-02 -0.259202D+01 -0.495878D+01 0.291200D+00
22 -0.238218D-02 0.266529D-02 -0.728130D+00 -0.201307D-01 -0.929190D-01
23 0.221932D-01 0.987456D-04 0.340995D+00 0.183657D+00 0.280931D+01
24 -0.161526D-02 -0.471304D-03 -0.155274D+00 -0.189103D-01 -0.156339D+01
ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES
21 22 23 24
________ ________ ________ ________
21 0.606255D+01
22 -0.362716D-01 0.883075D-02
23 -0.950968D-01 -0.710491D-02 0.636971D+00
24 0.139760D-01 0.154779D-02 -0.619515D-01 0.171302D-01
ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES
1 2 3 4 5
________ ________ ________ ________ ________
1 1.000
2 -0.084 1.000
3 0.114 -0.028 1.000
4 -0.006 0.105 -0.194 1.000
5 -0.022 0.030 -0.001 0.024 1.000
6 0.038 -0.010 -0.002 0.029 -0.080
7 -0.014 0.073 -0.040 0.035 0.123
8 0.017 -0.014 0.026 0.053 0.022
9 -0.088 0.037 0.041 -0.032 0.102
10 -0.075 -0.052 0.066 -0.009 0.434
11 -0.051 -0.009 0.014 0.004 0.068
12 -0.007 0.010 0.012 -0.078 0.056
13 0.006 0.067 -0.035 0.005 -0.038
14 0.023 0.020 0.050 0.046 0.037
15 -0.262 -0.041 -0.042 -0.015 -0.128
16 -0.170 -0.071 -0.004 -0.093 -0.033
17 0.153 -0.091 -0.024 0.028 -0.056
18 -0.059 -0.044 0.012 -0.087 0.015
19 -0.045 0.042 0.031 -0.058 0.047
20 0.025 -0.034 -0.059 -0.073 -0.049
21 0.040 -0.084 -0.021 0.024 -0.033
22 -0.006 0.047 -0.036 0.116 -0.086
23 0.043 -0.097 0.014 -0.009 0.009
24 -0.062 0.076 0.052 0.160 0.026
ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES
6 7 8 9 10
________ ________ ________ ________ ________
6 1.000
7 0.452 1.000
8 -0.120 -0.032 1.000
9 0.090 0.068 -0.012 1.000
10 -0.053 -0.004 0.004 0.147 1.000
11 0.263 0.203 0.040 0.195 0.069
12 -0.050 0.025 0.114 0.098 0.026
13 0.490 0.544 -0.088 0.073 -0.115
14 -0.050 0.026 0.507 0.017 0.060
15 -0.043 -0.044 -0.041 -0.090 -0.167
16 0.028 0.007 -0.051 0.178 -0.058
17 -0.003 -0.036 0.044 -0.204 0.001
18 -0.101 -0.144 -0.003 -0.060 0.031
19 -0.227 0.021 -0.070 -0.085 -0.015
20 0.049 0.012 -0.238 -0.048 0.012
21 0.206 -0.015 0.061 0.075 0.033
22 -0.042 -0.031 0.023 -0.001 -0.098
23 0.006 -0.009 -0.046 -0.006 -0.015
24 -0.011 0.001 -0.008 0.020 0.015
ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES
11 12 13 14 15
________ ________ ________ ________ ________
11 1.000
12 0.063 1.000
13 0.005 -0.011 1.000
14 0.068 0.108 -0.057 1.000
15 -0.014 -0.004 -0.022 0.022 1.000
16 -0.009 0.009 0.036 -0.027 0.170
17 -0.016 -0.023 -0.014 -0.016 -0.573
18 -0.070 -0.016 -0.101 0.017 0.148
19 -0.087 0.041 -0.030 -0.144 0.056
20 -0.062 -0.089 0.010 -0.316 0.025
21 0.145 -0.044 0.028 0.150 -0.042
22 -0.135 -0.003 -0.013 -0.041 -0.071
23 -0.013 0.086 -0.022 -0.024 -0.062
24 0.008 -0.138 0.006 0.044 0.038
ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES
16 17 18 19 20
________ ________ ________ ________ ________
16 1.000
17 -0.258 1.000
18 0.030 -0.062 1.000
19 0.041 -0.006 0.136 1.000
20 -0.020 0.018 0.101 -0.025 1.000
21 0.099 -0.010 -0.079 -0.879 0.006
22 -0.038 0.243 -0.579 -0.093 -0.050
23 0.041 0.001 0.032 0.100 0.179
24 -0.018 -0.031 -0.089 -0.063 -0.609
ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES
21 22 23 24
________ ________ ________ ________
21 1.000
22 -0.157 1.000
23 -0.048 -0.095 1.000
24 0.043 0.126 -0.593 1.000
|
21cf4082f38190701ecb747cb2fd40908f887e03 | 99b4e2e61348ee847a78faf6eee6d345fde36028 | /Toolbox Test/blackman/blackman10.sce | f00c48a8c31d9a520ad2dd49f5d47ee695af2cb6 | [] | no_license | deecube/fosseetesting | ce66f691121021fa2f3474497397cded9d57658c | e353f1c03b0c0ef43abf44873e5e477b6adb6c7e | refs/heads/master | 2021-01-20T11:34:43.535019 | 2016-09-27T05:12:48 | 2016-09-27T05:12:48 | 59,456,386 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 168 | sce | blackman10.sce | //no i/p
w=blackman();
disp(w);
//output
//!--error 10000
//Incorrect number of input arguments.
//at line 33 of function blackman called by :
//w=blackman();
|
6f9ccd02f723eb82a19abeefd278c24a926898d0 | 8627886261b3eddf8440c0b470cd9ee25c762d97 | /kr1.sci | 3eda2b9596170c3a35a4514da5c4df0a7bce8a3a | [] | no_license | timurzotov/pvis | ba75cf86fae91b6adc8dd3fe9cd2672eea561cca | d60e8e241d6ce0ad3a9b2a75c8771f92a9b039ba | refs/heads/master | 2020-09-08T07:59:31.719500 | 2019-11-11T21:14:13 | 2019-11-11T21:14:13 | 221,070,925 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 758 | sci | kr1.sci | clc;
d=figure();//создаем окно
set(d,'position',[0,0,420,420]);//местоположение и размеры окна
set(d,'figure_name','билет №1');//заголовок окна
set(d,'BackgroundColor',[0,0.6,0.6]);//цвет окна
button1=uicontrol(d,'style','pushbutton','string','Открыть окно.','position',[30,300,300,60],'BackgroundColor',[0,0.9,0.9],'CallBack','a1');
function a1
f=figure();
button2=uicontrol(f,'style','pushbutton','string','Построить график.','position',[195,375,150,30],'BackgroundColor',[0,0.9,0.9],'CallBack','grafik1');
endfunction
function grafik1
x=1:0.1:10;
scf()
plot(x, sin(x),'-r' );
xgrid(5); xtitle('График функции (sin(x)');
endfunction
|
66cfb1d00856a815e22d1b3599cf791d3ef07897 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1448/CH4/EX4.3.i/I4_3.sce | f47f5b00a3ce5c5f32c93f04f79197d05dad2b75 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 183 | sce | I4_3.sce | clc
//Initialization of variables
SH2O=70 //J/K mol
SH2=131 //J/K mol
SO2=205 //J/K mol
//calculations
deltaS=2*SH2O-2*SH2-SO2
printf('Change in entropy = %d J/K mol',deltaS)
|
aec48c6c6b5e6fc52f95ee9769b7985910f0477d | 449d555969bfd7befe906877abab098c6e63a0e8 | /1910/CH1/EX1.2/Chapter12.sce | 6f7eef26ee9861b2dd89066e87c8825880d1e2f8 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 871 | sce | Chapter12.sce | // Display mode
mode(0);
// Display warning for floating point exception
ieee(1);
clear;
clc;
disp("Introduction to heat transfer by S.K.Som, Chapter 1, Example 2")
//The thermal conductivity(km)of masonry wall is .8 W/(mK)
//The thermal conductivity(kc)of composite wall is .2 W/(mK)
//The thickness of composite wall(Lc) is 100 mm or .1 m
km=.8;
kc=.2;
Lc=.1;
//The thickness of masonry wall(Lm) is to be found.
//The steady state heat flow(qm)through masonry wall is km(T1-T2)/L
// The steady state heat flow(qc)through composite wall is kc(T1-T2)/L
//As the steady rate of heat flow through masonry wall is 80% that through composite wall and both the wall have same surface area and same temp. difference so qm/qc=0.8=(km/kc)*(Lc/Lm)
//The thickness of masonry wall is Lm.
disp ("The thickness of masonry wall is Lm in m")
Lm=(km/kc)*(Lc/(0.8))
|
1d5cdae738716173435c68971fb9e9daa2fb51dd | d963a50c09b7380dd7b1b97cd9997e9bd17ea8f3 | /r35/lib/symmetry.tst | 6294ba00d55ff863958e399443b4eed96287a097 | [
"BSD-3-Clause"
] | permissive | reduce-algebra/reduce-historical | 8220e211b116e0e01ff1a38f51917cac9db6069f | e014152729c4d62bb1ce4f5c311a027042a5495a | refs/heads/master | 2023-04-10T22:54:00.796596 | 2021-04-16T08:52:19 | 2021-04-16T08:52:19 | 343,245,204 | 7 | 1 | NOASSERTION | 2021-04-16T08:53:31 | 2021-03-01T00:15:22 | TeX | UTF-8 | Scilab | false | false | 1,430 | tst | symmetry.tst | % test symmetry package
% implementation of theory of linear representations
% for small groups
availablegroups();
printgroup(D4);
generators(D4);
charactertable(D4);
characternr(D4,1);
characternr(D4,2);
characternr(D4,3);
characternr(D4,4);
characternr(D4,5);
irreduciblereptable(D4);
irreduciblerepnr(D4,1);
irreduciblerepnr(D4,2);
irreduciblerepnr(D4,3);
irreduciblerepnr(D4,4);
irreduciblerepnr(D4,5);
rr:=mat((1,0,0,0,0),
(0,0,1,0,0),
(0,0,0,1,0),
(0,0,0,0,1),
(0,1,0,0,0));
sp:=mat((1,0,0,0,0),
(0,0,1,0,0),
(0,1,0,0,0),
(0,0,0,0,1),
(0,0,0,1,0));
rep:={D4,rD4=rr,sD4=sp};
canonicaldecomposition(rep);
character(rep);
symmetrybasis(rep,1);
symmetrybasis(rep,2);
symmetrybasis(rep,3);
symmetrybasis(rep,4);
symmetrybasis(rep,5);
symmetrybasispart(rep,5);
allsymmetrybases(rep);
% Ritz matrix from Stiefel, Faessler p. 200
m:=mat((eps,a,a,a,a),
(a ,d,b,g,b),
(a ,b,d,b,g),
(a ,g,b,d,b),
(a ,b,g,b,d));
diagonalize(m,rep);
% eigenvalues are obvious. Eigenvectors may be obtained with
% the coordinate transformation matrix given by allsymmetrybases.
r1:=mat((0,1,0),
(0,0,1),
(1,0,0));
repC3:={C3,rC3=r1};
mC3:=mat((a,b,c),
(c,a,b),
(b,c,a));
diagonalize(mC3,repC3);
% note difference between real and complex case
on complex;
diagonalize(mC3,repC3);
off complex;
end;
|
3f96d79d4404bcfa82e203fb5af99b2e36be7015 | d8cab241a02c8d06f859a4adbf2748d68c08d385 | /sistema_edo.sce | 4abb8129fc99117673a9e1460f81f73026ddb055 | [] | no_license | eluire/CN | 6327b9619a6e00d2870912830393def2ca82b856 | e2027e0d20c549bb1a79ce830c6affcf4cbe1149 | refs/heads/master | 2021-09-16T07:13:23.367948 | 2018-06-18T10:51:21 | 2018-06-18T10:51:21 | 126,038,180 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 830 | sce | sistema_edo.sce | clc
clear
// FUNÇÃO 1 DO SISTEMA
function z = gL1(t,L1,L2)
z = -0.004918*sqrt(1960*L1)+(0.2218)*7;
endfunction
//function z = gL1(t,L1,L2)
// z = -0.004918*sqrt(1960*L1)+(0.2218)*(8+6*sin(t));
//endfunction
//function z = gL1(t,L1,L2)
// z = -0.004918*sqrt(1960*L1)+(0.2218)*t;
//endfunction
//
// FUNÇÃO 2 DO SISTEMA
function z = gL2(t,L1,L2)
z = -0.0069*sqrt(1960*L2)+ (0.004918)*sqrt(1960*L1);
endfunction
// APLICAÇÃO DO MÉTODO DE EULER
function [t,L1,L2] = eulerSistema(a,b,h,L10,L20)
t = a:h:b; // t é a variável tempo
n = length(t);
L1(1) = L10;
L2(1) = L20;
for i = 1:n-1
kL1 = gL1(t(i),L1(i),L2(i));
kL2 = gL2(t(i),L1(i),L2(i));
L1(i+1) = L1(i) + kL1*h;
L2(i+1) = L2(i) + kL2*h;
end
endfunction
|
b1ffc6b3eada3467f3c1339a769e6c0fd6b300e4 | 9d56190f88be9cd37cd046af65941cab5c1b423b | /week-6/main.tst | 8119610728f2e9cb59f11d0b753920f154b627f1 | [] | no_license | yuva-a/Week-6- | 48039a114355cbcc447207713faf512420fd0e86 | cdc9a10a5de1788e393de2080f7942361beda872 | refs/heads/main | 2023-08-22T15:58:57.978887 | 2021-10-12T17:16:04 | 2021-10-12T17:16:04 | 415,652,964 | 0 | 1 | null | 2021-10-12T15:56:25 | 2021-10-10T17:23:13 | Scilab | UTF-8 | Scilab | false | false | 431 | tst | main.tst | load main.hdl,
output-file main.out,
// compare-to main.cmp,
output-list x%B3.16.3 y%B3.16.3 out%B3.16.3 ;
//same sign
set x %B0011111110010000,
set y %B0011111111000000,
eval,
output;
set x %B1011111111010000,
set y %B1011111111000000,
eval,
output;
//opposite sign
set x %B1011111111010000,
set y %B0011111111000000,
eval,
output;
set x %B0011111110010000,
set y %B1011111111000000,
eval,
output;
|
4fdc19b2ced6511714928faca1473430118ac07b | 449d555969bfd7befe906877abab098c6e63a0e8 | /1757/CH4/EX4.9/EX4_9.sce | 8526498faf3816b1056dcf2f7e8f1c0610780c80 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 441 | sce | EX4_9.sce | // Example4.9 // Determine the non-inverting input voltage
clc;
clear;
close;
R1 = 10 ; //kilo ohm // input resistance
R2 = 25 ; //kilo ohm // feedback resistance
Voh = 10 ; // volt //output voltage
Vol = -10 ; // volt // output voltage
// upper voltage
V = (R1/(R1+R2)*Voh) ;
disp(' The upper voltage is = '+string(V)+' V ');
// Lower voltage
V = (R1/(R1+R2)*Vol) ;
disp(' The lower voltage is = '+string(V)+' V ');
|
4689e8ace048505b20094ce63460d4e9d289b012 | 449d555969bfd7befe906877abab098c6e63a0e8 | /635/CH10/EX10.2/Ch10Ex2.sci | 6cb868c3a79e49c6bb960426b6e7afadac7f3b64 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 874 | sci | Ch10Ex2.sci | // Scilab Code Ex 10.2 Motion of a ground state Electron in a 3-D Potential Well: Page-329 (2010)
a = 0.5*10^-10; // length of the potential box, m
h = 6.626*10^-34; // Plank's Constant, Js
m = 9.1*10^-31; // Mass of an Electron, kg
// In 3-D, the three quantum numbers nx, ny and nz each will have value equal to 1 for lowest energy state
nx = 1; // Quantum number corresponding to x-direction
ny = 1; // Quantum number corresponding to y-direction
nz = 1; // Quantum number corresponding to z-direction
EG = h^2*(nx^2+ny^2+nz^2)/(8*m*a^2); // Energy eigen value for 3-D potential, J
EeV = EG/1.6D-19; // Convert energy from joule to eV
disp (EeV, "The lowest energy of an electron confined to move in a 3D-potential box, in eV, is : ")
//Result
// The lowest energy of an electron confined to move in a 3D-potential box, in eV, is :
// 452.30641 |
e19a3edd00f50d30a64a848b7bde442d637b4ec8 | 9b68b3d73b63ebcbfe18cc9a4aa8e91c84833a84 | /tests/libs/hdf5/test-env-variables-new/C/H5T/testfiles/110/h5ex_t_convert.tst | b70906a56a2106fe98fac2602855d154d2b32a08 | [
"LicenseRef-scancode-warranty-disclaimer",
"LicenseRef-scancode-llnl",
"LicenseRef-scancode-unknown-license-reference",
"Apache-2.0",
"LicenseRef-scancode-hdf4"
] | permissive | openhpc/ohpc | 17515db5082429eb9f250f12bf242b994beb715f | 725a1f230434d0f08153ba1a5d0a7418574f8ae9 | refs/heads/3.x | 2023-08-19T02:15:14.682630 | 2023-08-18T19:33:51 | 2023-08-18T19:34:18 | 43,318,561 | 827 | 247 | Apache-2.0 | 2023-09-14T01:22:18 | 2015-09-28T18:20:29 | C | UTF-8 | Scilab | false | false | 497 | tst | h5ex_t_convert.tst | sensor[0]:
Serial number : 1153
Location : Exterior (static)
Temperature (F) : 54.840000
Pressure (inHg) : 24.760000
sensor[1]:
Serial number : 1184
Location : Intake
Temperature (F) : 56.630000
Pressure (inHg) : 23.100000
sensor[2]:
Serial number : 1027
Location : Intake manifold
Temperature (F) : 102.690000
Pressure (inHg) : 30.970000
sensor[3]:
Serial number : 1313
Location : Exhaust manifold
Temperature (F) : 1238.270000
Pressure (inHg) : 82.150000
|
096c6941e04f43bdd09b24cd50b7608871a2ecd8 | a5f0fbcba032f945a9ee629716f6487647cafd5f | /Dump/Development backup/Development/Algorithms/Ensemble/Emsemble.sci | ec1162f4488896de754930c3935e16dac3ae8f60 | [] | no_license | SoumitraAgarwal/Scilab-gsoc | 692c00e3fb7a5faf65082e6c23765620f4ecdf35 | 678e8f80c8a03ef0b9f4c1173bdda7f3e16d716f | refs/heads/master | 2021-04-15T17:55:48.334164 | 2018-08-07T13:43:26 | 2018-08-07T13:43:26 | 126,500,126 | 1 | 1 | null | null | null | null | UTF-8 | Scilab | false | false | 524 | sci | Emsemble.sci | // Macro for ensemble of predictors -- Scilab
// Function takes 2 predictions, target vector
// and learning rate as input and creates an
// output for an ensemble
function pred = ensemble(pred1, pred2, y, increment)
bestweight = 0;
besterror = 0.5*sqrt(norm(pred2 - y));
for weight = 0:increment:1
thiserror = 0.5*sqrt(norm(weight*pred1 + (1 - weight)*pred2 - y))
if(besterror > thiserror)
besterror = thiserror;
bestweight = weight;
end
end
pred = bestweight*pred1 + (1 - bestweight)*pred2
endfunction |
5b41867db5209a6605f0f7618430756d36cb4544 | 449d555969bfd7befe906877abab098c6e63a0e8 | /275/CH8/EX8.8.48a/Ch8_8_48a.sce | a77924ce13b6678c7a8425cd00f3ed1ac4fdbcee | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 443 | sce | Ch8_8_48a.sce | clc
clear
disp("Example 8.48a")
printf("\n")
disp("Prove the following boolean thereom")
disp("A+AB=A")
disp("A=a,B=b,AB=s,A+AB=d")
a=[0 0 1 1]
b=[0 1 0 1]
for i=1:length(a)
s(i)=a(i)*b(i)
end
for i=1:length(a)
d(i)=s(i)+a(i)
if(d(i)==2)
d(i)=1
end
end
for i=1:length(a)
if(a(i)==d(i))
printf("")
else
printf("not")
abort
end
end
printf("yes") |
5734ce297cb66548803635dccd7ac5129a445d33 | ebfed86dee276110294a4e93fa80377908bbd317 | /macros/imlincomb.sci | 64f01df591d6a17d19d0fef8589b2167090348b5 | [] | no_license | gursimarsingh/FOSSEE-Image-Processing-Toolbox | a9d46b698c98566fec867eb2ce3cfeb427058d5c | 165f6d7d1f20262a1637a923c6aad6e663ad1538 | refs/heads/master | 2021-08-16T19:18:59.591175 | 2017-11-08T17:55:04 | 2017-11-08T17:55:04 | 96,531,802 | 0 | 0 | null | 2017-07-07T11:21:10 | 2017-07-07T11:21:10 | null | UTF-8 | Scilab | false | false | 1,595 | sci | imlincomb.sci | // Copyright (C) 2015 - IIT Bombay - FOSSEE
//
// This file must be used under the terms of the CeCILL.
// This source file is licensed as described in the file COPYING, which
// you should have received as part of this distribution. The terms
// are also available at
// http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt
// Author: Gursimar Singh
// Organization: FOSSEE, IIT Bombay
// Email: toolbox@scilab.in
//
function outImg= imlincomb(x1,A1,varargin)
//Blend two or more images
//
//Calling Sequence
//outImg= imlincomb(x1,A1);
//outImg= imlincomb(x1,A1,A2,A2,x3,A3,x4,A4........,xN,AN);
//
//Parameters
//outImg:Output combined image.
//xN:Input multiplication factor.The multiplication factor and the sum of all the mutiplication factors should be less than 1.
//AN:Input image
//
//Description
//This function returns a linear combination of the input images.
//
//Examples
//im1=imread('images/balls.jpg');
//im2=imread('images/lena.jpeg');
//img=imlincomb(0.5,im1,05,im2);
//
//Authors
//Gursimar Singh
//
//See also
//imimposemin
//imadd
[lhs rhs] = argn(0);
if rhs<1 then
error(msprintf("Not enough input arguments"));
end
if lhs >1
error(msprintf("Too many output arguments"));
end
if modulo(rhs-1,2) == 0 then
error(msprintf("Number of input arguments must be even"));
end
out=x1*A1;
if rhs>2
for i=1:rhs/2 -1
A=varargin(2*i);
x=varargin(2*i-1);
B=x*A;
out=imadd(out,B);
end
end
outImg=out;
endfunction
|
b4acff3b067a1b9ccf3aa496d0355e10bd1bf006 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3756/CH1/EX1.30/Ex1_30.sce | 94b5c1b65822f337b2dc915b26c1b7d3514fe753 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 184 | sce | Ex1_30.sce | clc
//
//
//
//Variable declaration
l=0.0025 //Distance moved
t=0.005 //thickness of mica sheet
//Calculations
mu=((l/t)+1)
//Result
printf("\n The Refractive Index is %0.3f ",mu)
|
9e3a629f47e44a1d2de68baa5ae78ca239852025 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1658/CH25/EX25.11/Ex25_11.sce | 8b91835682fe556a2af4eb3ad8ea23e7462c67ec | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 180 | sce | Ex25_11.sce | clc;
Ptrdc=100*10**-3;
VCC=10;
RL=16;
no=0.5;
Poac=no*Ptrdc;
disp('mW',Poac*10**3,"Poac=");
ICQ=2*Poac/VCC;
disp('A',ICQ,"ICQ=");
RL1=VCC/ICQ;
a=sqrt(RL1/RL);
disp(a);
|
28640b4d6c76556d8c8ad251602a1beb92b0683a | 8baa4268cc19995abb706bcc05c80afb319e1669 | /test/delete.tst | 3df98838a1c9f1569e9768d3158fb9884835a03c | [] | no_license | nicoloison/CPSC471-Project | 53c3362e0251f3c37edf0ab9769277d15670dc21 | db0db7d7be776d6d6958d920596bc708d3347e82 | refs/heads/master | 2020-04-18T13:42:30.599190 | 2014-12-26T10:58:19 | 2014-12-26T10:58:19 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 159 | tst | delete.tst | curl localhost/recipes/delete.php
curl "localhost/recipes/delete.php?recipe_name=ribs"
curl "localhost/recipes/delete.php?recipe_name=ribs&author_name=adjuric" |
62563fde6b7c7bf877c0e7260ed8ca1f97cfeda1 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3554/CH5/EX5.3/Ex5_3.sce | 3262a4955d92c3fb99988c5fa5917d30a0be858c | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 479 | sce | Ex5_3.sce | // Exa 5.3
clc;
clear all;
// Given data
// 3 1/2 digit display
V1=1; // Volts
V2=10;//Volts
// Solution
disp("Number of full digits is 3.");
n=3;//Full digits
Reso=1/10^n;
printf(' Resolution = %.3f . Hence, meter cannot distinguish two values if their difference is less than %.3f \n ',Reso,Reso);
printf('For full scale reading of 1V, the resolution is %.3f V \n ',V1*Reso);
printf('For full scale reading of 10V, the resolution is %.2f V \n ',V2*Reso);
|
8f427fbf582263cd59721d0c8182c8d106fe2e35 | 1bc06fa90b5425d41347c90d0c73bb82eb4cbbfe | /scripts/approximer.sci | 0a64ccc6ee6e26818886d77c3df45d59d5655ab1 | [] | no_license | madox35/Filtre-Canny | a0a527ad6be5a1dc5984b2533008f95b1c9663ee | 3a54da9b0ce917c995ea5fbd48e0ed5c3f36748d | refs/heads/master | 2020-03-08T08:57:27.702111 | 2018-04-21T19:39:39 | 2018-04-21T19:39:39 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 717 | sci | approximer.sci | function direction = approximer(angle)
// première condition différente car si l'angle = 176 par exemple,
// on respectera bien >= 157.5 mais pas <= -157.5
// se référer au schéma directions.png
if( ((angle >= -22.5) & (angle <= 22.5)) | (angle <= -157.5) | (angle >= 157.5) ) then
direction = 0;
elseif( ((angle > 22.5) & (angle <= 67.5)) | ((angle > -157.5) & (angle <= -112.5)) ) then
direction = 45;
elseif( ((angle > 67.5) & (angle <= 112.5)) | ((angle > -112.5) & (angle <= -67.5)) ) then
direction = 90;
elseif( ((angle > 112.5) & (angle < 157.5) ) | ((angle > -67.5) & (angle < -22.5)) ) then
direction = 135;
end
endfunction
|
89cfe21f588bd78f86115f1be6e82b4a7b7e6575 | 3073307fa4b6da9371518f0718c199501b8c5c71 | /viejos/fact_cholesky.sci | f659519ea614b300afa02496bc5827eeefda675d | [] | no_license | fern17/CalculoNumerico | 8b04abdf8e1da4b69a1256334a4bc58ff5c9180d | c793733ce17616361dd02f358ef63c1d9be5c99e | refs/heads/master | 2020-06-04T00:06:19.723655 | 2011-12-20T13:47:40 | 2011-12-20T13:47:40 | 2,929,202 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 482 | sci | fact_cholesky.sci | //Realiza la factorizacion LLt de Cholesky, donde
// L es matriz triangular inferior
// y la matriz de entrada es simetrica y definida positiva
function [L] = fact_cholesky(A)
n = size(A,1);
L = zeros(n,n);
for k=1:n
suma = 0;
for s=1:(k-1)
suma = suma + L(k,s)^2;
end
L(k,k) = sqrt(A(k,k) - suma);
for i=(k+1):n
L(i,k) = (A(i,k) - L(i,1:(k-1))*L(k,1:(k-1)))/L(k,k);
end
end
endfunction
|
33ae85b29661dc4105b98a7d132bd648032c5e6f | 36c5f94ce0d09d8d1cc8d0f9d79ecccaa78036bd | /Stralroom Fast Strafes.sce | bdd3abe9a06d77e3566c95b74c13112a6dc7df5d | [] | no_license | Ahmad6543/Scenarios | cef76bf19d46e86249a6099c01928e4e33db5f20 | 6a4563d241e61a62020f76796762df5ae8817cc8 | refs/heads/master | 2023-03-18T23:30:49.653812 | 2020-09-23T06:26:05 | 2020-09-23T06:26:05 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 75,160 | sce | Stralroom Fast Strafes.sce | Name=Stralroom Fast Strafes
PlayerCharacters=Quaker
BotCharacters=Quaker Bot Fast Strafes.bot
IsChallenge=true
Timelimit=60.0
PlayerProfile=Quaker
AddedBots=Quaker Bot Fast Strafes.bot
PlayerMaxLives=0
BotMaxLives=0
PlayerTeam=1
BotTeams=2
MapName=stralroom.map
MapScale=3.8125
BlockProjectilePredictors=true
BlockCheats=true
InvinciblePlayer=true
InvincibleBots=false
Timescale=1.0
BlockHealthbars=false
TimeRefilledByKill=0.0
ScoreToWin=1000.0
ScorePerDamage=3.0
ScorePerKill=0.0
ScorePerMidairDirect=0.0
ScorePerAnyDirect=0.0
ScorePerTime=0.0
ScoreLossPerDamageTaken=0.0
ScoreLossPerDeath=0.0
ScoreLossPerMidairDirected=0.0
ScoreLossPerAnyDirected=0.0
ScoreMultAccuracy=false
ScoreMultDamageEfficiency=true
ScoreMultKillEfficiency=false
GameTag=Quake, Reflex
WeaponHeroTag=LG, Lightning Gun
DifficultyTag=4
AuthorsTag=Stral
BlockHitMarkers=false
BlockHitSounds=false
BlockMissSounds=true
BlockFCT=false
Description=Fast Strafes combat in a room with more vertical fights and stairs.
GameVersion=0.95.0
[Aim Profile]
Name=At Feet
MinReactionTime=0.3
MaxReactionTime=0.4
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=15.0
TrackSpeed=3.5
TrackError=3.5
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=40.0
ShootFOV=15.0
VerticalAimOffset=-200.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Aim Profile]
Name=Low Skill At Feet
MinReactionTime=0.35
MaxReactionTime=0.45
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=20.0
TrackSpeed=3.0
TrackError=5.0
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=60.0
ShootFOV=25.0
VerticalAimOffset=-200.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Aim Profile]
Name=Low Skill
MinReactionTime=0.35
MaxReactionTime=0.45
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=20.0
TrackSpeed=3.0
TrackError=5.0
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=60.0
ShootFOV=25.0
VerticalAimOffset=0.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Aim Profile]
Name=Default
MinReactionTime=0.3
MaxReactionTime=0.4
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=15.0
TrackSpeed=3.5
TrackError=3.5
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=40.0
ShootFOV=15.0
VerticalAimOffset=0.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
[Bot Profile]
Name=Quaker Bot Fast Strafes
DodgeProfileNames=Short Strafes
DodgeProfileWeights=1.0
DodgeProfileMaxChangeTime=5.0
DodgeProfileMinChangeTime=1.0
WeaponProfileWeights=1.0;1.0;2.0;1.0;1.0;1.0;1.0;1.0
AimingProfileNames=At Feet;Low Skill At Feet;Low Skill;Default;Default;Default;Default;Default
WeaponSwitchTime=3.0
UseWeapons=false
CharacterProfile=Quaker
SeeThroughWalls=false
[Character Profile]
Name=Quaker
MaxHealth=300.0
WeaponProfileNames=LG;Rocket Launcher;Railgun;;;;;
MinRespawnDelay=1.0
MaxRespawnDelay=5.0
StepUpHeight=75.0
CrouchHeightModifier=0.5
CrouchAnimationSpeed=2.0
CameraOffset=X=0.000 Y=0.000 Z=80.000
HeadshotOnly=false
DamageKnockbackFactor=4.0
MovementType=Base
MaxSpeed=1300.0
MaxCrouchSpeed=500.0
Acceleration=9000.0
AirAcceleration=16000.0
Friction=4.0
BrakingFrictionFactor=2.0
JumpVelocity=800.0
Gravity=3.0
AirControl=0.25
CanCrouch=true
CanPogoJump=false
CanCrouchInAir=true
CanJumpFromCrouch=false
EnemyBodyColor=X=0.771 Y=0.000 Z=0.000
EnemyHeadColor=X=1.000 Y=1.000 Z=1.000
TeamBodyColor=X=1.000 Y=0.888 Z=0.000
TeamHeadColor=X=1.000 Y=1.000 Z=1.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=0.0
MainBBType=Cylindrical
MainBBHeight=320.0
MainBBRadius=58.0
MainBBHasHead=false
MainBBHeadRadius=45.0
MainBBHeadOffset=0.0
MainBBHide=false
ProjBBType=Cylindrical
ProjBBHeight=230.0
ProjBBRadius=55.0
ProjBBHasHead=false
ProjBBHeadRadius=45.0
ProjBBHeadOffset=0.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.2
JetpackFullFuelTime=4.0
JetpackFuelIncPerSec=1.0
JetpackFuelRegensInAir=false
JetpackThrust=6000.0
JetpackMaxZVelocity=400.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=false
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=0.0
BlockSpawnFOV=0.0
BlockSpawnDistance=0.0
RespawnAnimationDuration=0.5
[Dodge Profile]
Name=Short Strafes
MaxTargetDistance=2500.0
MinTargetDistance=750.0
ToggleLeftRight=true
ToggleForwardBack=false
MinLRTimeChange=0.2
MaxLRTimeChange=0.5
MinFBTimeChange=0.2
MaxFBTimeChange=0.5
DamageReactionChangesDirection=false
DamageReactionChanceToIgnore=0.5
DamageReactionMinimumDelay=0.125
DamageReactionMaximumDelay=0.25
DamageReactionCooldown=1.0
DamageReactionThreshold=50.0
DamageReactionResetTimer=0.5
JumpFrequency=0.1
CrouchInAirFrequency=0.0
CrouchOnGroundFrequency=0.0
TargetStrafeOverride=Ignore
TargetStrafeMinDelay=0.125
TargetStrafeMaxDelay=0.25
MinProfileChangeTime=0.0
MaxProfileChangeTime=0.0
MinCrouchTime=0.3
MaxCrouchTime=0.6
MinJumpTime=0.3
MaxJumpTime=0.6
LeftStrafeTimeMult=1.0
RightStrafeTimeMult=1.0
StrafeSwapMinPause=0.0
StrafeSwapMaxPause=0.0
BlockedMovementPercent=0.5
BlockedMovementReactionMin=0.125
BlockedMovementReactionMax=0.2
[Weapon Profile]
Name=LG
Type=Hitscan
ShotsPerClick=1
DamagePerShot=6.0
KnockbackFactor=2.0
TimeBetweenShots=0.046
Pierces=false
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=false
HeadshotMultiplier=2.0
CooldownType=InfiniteUse
MagazineMax=0
AmmoPerShot=1
ReloadTimeFromEmpty=0.5
ReloadTimeFromPartial=0.5
CooldownTimer=5.0
MaxCharges=3
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=7.0
DelayBeforeShot=0.0
HitscanVisualEffect=Tracer
ProjectileGraphic=Ball
VisualLifetime=0.05
WallParticleEffect=None
HitParticleEffect=None
BounceOffWorld=false
BounceFactor=0.0
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileWorldHitRadius=1.0
ProjectileEnemyHitRadius=1.0
CanAimDownSight=false
ADSZoomFactor=0.7
ADSZoomDelay=0.0
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
ShootSound=Shot
HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=9.0
RecoilNegatable=false
DecalType=0
DecalSize=30.0
DelayAfterShooting=0.0
BeamTracksCrosshair=true
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
ProjectileTrail=None
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=true
AimPunchAmount=0.0
AimPunchResetTime=0.05
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=true
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=0
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=0.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,0.0
SpreadSCA=1.0,1.0,-1.0,0.0
SpreadMSA=1.0,1.0,-1.0,0.0
SpreadMCA=1.0,1.0,-1.0,0.0
SpreadSSH=1.0,1.0,-1.0,0.0
SpreadSCH=1.0,1.0,-1.0,0.0
SpreadMSH=1.0,1.0,-1.0,0.0
SpreadMCH=1.0,1.0,-1.0,0.0
MaxRecoilUp=0.0
MinRecoilUp=0.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=false
TimeToRecoilPeak=0.05
TimeToRecoilReset=0.35
AAMode=0
AAPreferClosestPlayer=false
AAAlpha=0.05
AAMaxSpeed=1.0
AADeadZone=0.0
AAFOV=30.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.095
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
[Weapon Profile]
Name=Rocket Launcher
Type=Projectile
ShotsPerClick=1
DamagePerShot=120.0
KnockbackFactor=5.0
TimeBetweenShots=0.8
Pierces=false
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=5090.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=5090.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=100.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=0.0
HeadshotCapable=false
HeadshotMultiplier=2.0
CooldownType=InfiniteUse
MagazineMax=0
AmmoPerShot=1
ReloadTimeFromEmpty=0.5
ReloadTimeFromPartial=0.5
CooldownTimer=5.0
MaxCharges=3
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=25.0
DelayBeforeShot=0.0
HitscanVisualEffect=Tracer
ProjectileGraphic=Rocket
VisualLifetime=0.1
WallParticleEffect=Flare
HitParticleEffect=Flare
BounceOffWorld=false
BounceFactor=0.0
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileWorldHitRadius=1.0
ProjectileEnemyHitRadius=2.0
CanAimDownSight=false
ADSZoomFactor=0.7
ADSZoomDelay=0.0
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
ShootSound=Shot
HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=5.0
RecoilNegatable=false
DecalType=0
DecalSize=30.0
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
ProjectileTrail=None
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=true
AimPunchAmount=0.0
AimPunchResetTime=0.05
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=true
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=0
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
Explosive=true
Radius=500.0
DamageAtCenter=120.0
DamageAtEdge=0.1
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=true
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,0.0
SpreadSCA=1.0,1.0,-1.0,0.0
SpreadMSA=1.0,1.0,-1.0,0.0
SpreadMCA=1.0,1.0,-1.0,0.0
SpreadSSH=1.0,1.0,-1.0,0.0
SpreadSCH=1.0,1.0,-1.0,0.0
SpreadMSH=1.0,1.0,-1.0,0.0
SpreadMCH=1.0,1.0,-1.0,0.0
MaxRecoilUp=0.0
MinRecoilUp=0.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=false
TimeToRecoilPeak=0.05
TimeToRecoilReset=0.35
AAMode=2
AAPreferClosestPlayer=false
AAAlpha=0.5
AAMaxSpeed=0.5
AADeadZone=0.0
AAFOV=180.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=true
TriggerBotDelay=0.001
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.095
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
[Weapon Profile]
Name=Railgun
Type=Hitscan
ShotsPerClick=1
DamagePerShot=80.0
KnockbackFactor=9.0
TimeBetweenShots=1.0
Pierces=true
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=false
HeadshotMultiplier=2.0
CooldownType=InfiniteUse
MagazineMax=0
AmmoPerShot=1
ReloadTimeFromEmpty=0.5
ReloadTimeFromPartial=0.5
CooldownTimer=5.0
MaxCharges=3
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=25.0
DelayBeforeShot=0.0
HitscanVisualEffect=Tracer
ProjectileGraphic=Ball
VisualLifetime=0.5
WallParticleEffect=None
HitParticleEffect=Blood
BounceOffWorld=false
BounceFactor=0.0
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileWorldHitRadius=1.0
ProjectileEnemyHitRadius=1.0
CanAimDownSight=false
ADSZoomFactor=0.7
ADSZoomDelay=0.0
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
ShootSound=Shot
HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=9.0
RecoilNegatable=false
DecalType=1
DecalSize=30.0
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
ProjectileTrail=None
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=true
AimPunchAmount=0.0
AimPunchResetTime=0.05
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=true
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=0
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=0.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,5.0
SpreadSCA=1.0,1.0,-1.0,5.0
SpreadMSA=1.0,1.0,-1.0,5.0
SpreadMCA=1.0,1.0,-1.0,5.0
SpreadSSH=1.0,1.0,-1.0,5.0
SpreadSCH=1.0,1.0,-1.0,5.0
SpreadMSH=1.0,1.0,-1.0,5.0
SpreadMCH=1.0,1.0,-1.0,5.0
MaxRecoilUp=0.0
MinRecoilUp=0.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=false
TimeToRecoilPeak=0.05
TimeToRecoilReset=0.35
AAMode=0
AAPreferClosestPlayer=false
AAAlpha=0.05
AAMaxSpeed=1.0
AADeadZone=0.0
AAFOV=30.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=true
TriggerBotDelay=0.01
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.095
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Map Data]
reflex map version 8
global
entity
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type PlayerSpawn
Vector3 position -104.000000 0.000000 -192.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position 64.000000 0.000000 -192.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position -40.000000 0.000000 -72.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position 32.000000 0.000000 -72.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position 304.000031 96.000000 -240.000000
Vector3 angles 270.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position -303.999969 96.000000 -224.000000
Vector3 angles 450.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position 128.000000 232.000000 40.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position -128.000000 232.000000 40.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position -128.000000 368.000000 200.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position 128.000000 368.000000 200.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position 312.000031 192.000000 -496.000000
Vector3 angles 270.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position 296.000031 384.000000 -344.000000
Vector3 angles 270.000000 0.000000 0.000000
Bool8 teamA 0
entity
type PlayerSpawn
Vector3 position -311.999969 376.000000 -328.000000
Vector3 angles 450.000000 0.000000 0.000000
Bool8 teamA 0
|
5faf0b2a5ba888b53ea21b73809655b0f6385a69 | b28d322423f92a98c5f668a83528993b114fd3f3 | /sci_gateway/builder_gateway.sce | de09d9c0f68daa71833988b5045a7d7d66590a14 | [] | no_license | FOSSEE/FOSSEE-Optim-toolbox-development | 6757ca00f521032feb7177531a5143b021ea2fad | c43f04d302bfe9c4b7d11f6af1712dda1c8b38c2 | refs/heads/master | 2020-08-05T13:24:20.604620 | 2016-10-07T11:51:01 | 2016-10-07T11:51:01 | 67,248,229 | 0 | 2 | null | 2016-10-07T11:51:02 | 2016-09-02T19:09:26 | HTML | UTF-8 | Scilab | false | false | 670 | sce | builder_gateway.sce | // Copyright (C) 2015 - IIT Bombay - FOSSEE
//
// This file must be used under the terms of the CeCILL.
// This source file is licensed as described in the file COPYING, which
// you should have received as part of this distribution. The terms
// are also available at
// http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt
// Author: Harpreet Singh
// Organization: FOSSEE, IIT Bombay
// Email: toolbox@scilab.in
sci_gateway_dir = get_absolute_file_path('builder_gateway.sce');
tbx_builder_gateway_lang('cpp', sci_gateway_dir);
tbx_build_gateway_loader(['cpp'], sci_gateway_dir);
clear tbx_builder_gateway_lang tbx_build_gateway_loader;
clear sci_gateway_dir;
|
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