pierreqi/scilab_code · Datasets at Hugging Face

60e8db5e854de425363c897914499de7696ff3de

449d555969bfd7befe906877abab098c6e63a0e8

/575/CH6/EX6.3.3/6_3_3.sce

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[]

no_license

FOSSEE/Scilab-TBC-Uploads

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7bc77cb1ed33745c720952c92b3b2747c5cbf2df

refs/heads/master

2020-04-09T02:43:26.499817

2018-02-03T05:31:52

37,975,407

3

12

null

UTF-8

Scilab

false

724

sce

6_3_3.sce

clc pathname=get_absolute_file_path('6_3_3.sce') filename=pathname+filesep()+'633.sci' exec(filename) printf(" All the values in the textbook are Approximated hence the values in this code differ from those of Textbook") P=hr*P75 y=P/Porig ndot=PorigBar*Vdot/(R*T) ndotWater=ndot*y printf(" \n Molar flowrate of Water=%f Kmol/h",ndotWater) ndotBDA=ndot*(1-y) printf(" \n Molar flowrate of Dry Air=%f Kmol/h",ndotBDA) ndotO2=ndotBDA*0.21 printf(" \n Molar flowrate of Oxygen=%f Kmol/h",ndotO2) hm=P/(Porig-P) ha=hm*18/29 hmdot=P75/(Porig-P75) hp=100*hm/hmdot printf(" \n Molal Humidity=%f mol water/mol BDA",hm) printf(" \n Absolute Humidity=%f kg water/kg BDA",ha) printf(" \n Percentage Humidity=%f",hp)

ce3f428de2608c4fa220126e34b364271266e2c1

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/system/kiks_arena_addremoterobot.sci

c5ffad92d0eec7b43221f949de66b013cf632f28

[]

no_license

manasdas17/kiks-scilab

4f4064ed7619cad9e2117a6c0040a51056c938ee

37dc68914547c9d0f423008d44e973ba296de67b

refs/heads/master

2021-01-15T14:18:21.918789

2009-05-11T05:43:11

null

0

null

UTF-8

Scilab

false

1,295

sci

kiks_arena_addremoterobot.sci

function [] = kiks_arena_addremoterobo(xpos,ypos) // Display mode mode(0); // Display warning for floating point exception ieee(1); // ----------------------------------------------------- // (c) 2000-2004 Theodor Storm <theodor@tstorm.se> // http://www.tstorm.se // ----------------------------------------------------- global("KIKS_MMPERPIXEL","KIKS_ROBOT_RADIUS","KIKS_COLOR_ROBOT","KIKS_RBTMASK_COL","KIKS_ARENA_COLORMASK"); [rows,cols] = size(mtlb_double(KIKS_RBTMASK_COL)); //size(KIKS_RBTMASK_COL) minx = mtlb_s(floor(mtlb_double(xpos)/mtlb_double(KIKS_MMPERPIXEL)),floor(mtlb_double(KIKS_ROBOT_RADIUS)/mtlb_double(KIKS_MMPERPIXEL)));// xpos - robot radius miny = mtlb_s(floor(mtlb_double(ypos)/mtlb_double(KIKS_MMPERPIXEL)),floor(mtlb_double(KIKS_ROBOT_RADIUS)/mtlb_double(KIKS_MMPERPIXEL)));// ypos - robot radius maxx = mtlb_a(floor(mtlb_double(xpos)/mtlb_double(KIKS_MMPERPIXEL)),floor(mtlb_double(KIKS_ROBOT_RADIUS)/mtlb_double(KIKS_MMPERPIXEL))); maxy = mtlb_a(floor(mtlb_double(ypos)/mtlb_double(KIKS_MMPERPIXEL)),floor(mtlb_double(KIKS_ROBOT_RADIUS)/mtlb_double(KIKS_MMPERPIXEL))); KIKS_ARENA_COLORMASK(mtlb_imp(miny,maxy),mtlb_imp(minx,maxx)) = mtlb_a(mtlb_double(KIKS_ARENA_COLORMASK(mtlb_imp(miny,maxy),mtlb_imp(minx,maxx))),mtlb_double(KIKS_RBTMASK_COL)); endfunction

2a9dc85817a42808c28c1a95694dd92139cbe8a8

449d555969bfd7befe906877abab098c6e63a0e8

/3793/CH15/EX15.3/exp_15_3.sce

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no_license

FOSSEE/Scilab-TBC-Uploads

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refs/heads/master

2020-04-09T02:43:26.499817

2018-02-03T05:31:52

37,975,407

3

12

null

UTF-8

Scilab

false

277

sce

exp_15_3.sce

clear; clc; E_ll=110; X=10; V_o=(3*sqrt(2)*E_ll)/%pi; U1=15; V_d1=(V_o*(cosd(X)+cosd(U1+X)))/2; printf("\nthe dc output voltage when (U1=15) = %.3f kV",V_d1); U2=20; V_d2=(V_o*(cosd(X)+cosd(U2+X)))/2; printf("\nthe dc output voltage when (U2=20) = %.3f kV",V_d2);

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/dbt air rockets.sce

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[]

no_license

MBHuman/Scenarios

be1a722825b3b960014b07cda2f12fa4f75c7fc8

1db6bfdec8cc42164ca9ff57dd9d3c82cfaf2137

refs/heads/master

2023-01-14T02:10:25.103083

2020-11-21T16:47:14

null

0

null

UTF-8

Scilab

false

29,145

sce

dbt air rockets.sce

Name=dbt air rockets PlayerCharacters=QC no movement BotCharacters=target_decay_midair.bot IsChallenge=true Timelimit=60.0 PlayerProfile=QC no movement AddedBots=target_decay_midair.bot PlayerMaxLives=0 BotMaxLives=100 PlayerTeam=1 BotTeams=2 MapName=boxernobounds.map MapScale=3.5 BlockProjectilePredictors=false BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=100.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=10.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=diabotical WeaponHeroTag=Rocket launcher DifficultyTag=5 AuthorsTag= Ass1st BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Target jumps in random direction and height, starting from different spawns with varying height. Hit it midair. GameVersion=2.0.0.2 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false [Aim Profile] Name=All over noob MinReactionTime=0.1 MaxReactionTime=0.1 MinSelfMovementCorrectionTime=0.0001 MaxSelfMovementCorrectionTime=0.0001 FlickFOV=0.0 FlickSpeed=1.0 FlickError=100.0 TrackSpeed=1.0 TrackError=100.0 MaxTurnAngleFromPadCenter=360.0 MinRecenterTime=0.0 MaxRecenterTime=0.0 OptimalAimFOV=360.0 OuterAimPenalty=0.0 MaxError=90.0 ShootFOV=90.0 VerticalAimOffset=1000.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [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 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=target_decay_midair DodgeProfileNames=Balanced all directions DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=All over noob;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=target_decay_midair SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=QC no movement MaxHealth=100.0 WeaponProfileNames=QC RL no splash;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=160.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=1600.0 Acceleration=32000.0 AirAcceleration=16000.0 Friction=6.0 BrakingFrictionFactor=6.0 JumpVelocity=2700.0 Gravity=10.0 AirControl=0.1 CanCrouch=true CanPogoJump=true CanCrouchInAir=true CanJumpFromCrouch=true 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=Spheroid 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=;;;Launch.abilmelee 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 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=target_decay_midair MaxHealth=200.0 WeaponProfileNames=no damage;;;;;;; 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=2000.0 Gravity=5.0 AirControl=0.2 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=150.0 MainBBRadius=75.0 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=Jump on ground.abilmov;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=10.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Balanced all directions MaxTargetDistance=9000.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=true 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=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.16 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.1 MaxCrouchTime=0.2 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 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 [Weapon Profile] Name=QC RL no splash Type=Projectile ShotsPerClick=1 DamagePerShot=100.0 KnockbackFactor=6.0 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=6787.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=6787.000 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 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Rocket VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=2.0 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=0.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 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 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.1 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 IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Flare ParticleBodyImpact=Flare ParticleProjectileTrail=Smoke ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=true Radius=20.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.0 ExplodesOnContactWithEnemy=true DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=true 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 PBS0=0.0,0.0 [Weapon Profile] Name=no damage Type=Hitscan ShotsPerClick=1 DamagePerShot=0.0 KnockbackFactor=0.0 TimeBetweenShots=0.01 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 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.1 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=0.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=999.0 HitSoundCooldown=999.0 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=0.1 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=false SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=0.1 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false 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=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=None ParticleProjectileTrail=None ParticleHitscanTrace=None ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=0.1 DamageAtCenter=0.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.0 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=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 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=1.0 AAMaxSpeed=360.0 AADeadZone=0.0 AAFOV=360.0 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=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Movement Ability Profile] Name=Jump on ground MaxCharges=1.0 ChargeTimer=0.01 ChargesRefundedOnKill=0.0 DelayAfterUse=0.2 FullyAuto=false AbilityDuration=0.0 LockDirectionForDuration=true NegateGravityForDuration=false MainVelocity=1500.0 MainVelocityCanGoVertical=true MainVelocitySetToMovementKeys=true UpVelocity=2000.0 EndVelocityFactor=1.0 Hurtbox=false HurtboxRadius=50.0 HurtboxDamage=50.0 HurtboxGroundKnockbackFactor=1.0 HurtboxAirKnockbackFactor=1.0 AbilityBlocksTurning=false AbilityBlocksMovement=true AbilityBlocksAttack=false AttackCancelsAbility=false AbilityReloadsWeapon=false HealthRestore=0.0 AIUseInCombat=true AIUseOutOfCombat=true AIUseOnGround=true AIUseInAir=false AIReuseTimer=0.01 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=900000.0 AIMaxTargFOV=360.0 AIDamageReaction=false AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Melee Ability Profile] Name=Launch MaxCharges=1.0 ChargeTimer=1.0 ChargesRefundedOnKill=1.0 DelayAfterUse=0.1 FullyAuto=false AbilityDuration=0.15 HurtboxRadius=4000.0 HurtboxDamage=0.0 HurtboxGroundKnockbackFactor=0.0 HurtboxAirKnockbackFactor=0.0 BlockAttackTimer=0.0 AbilityBlockedWhenAttacking=false AmmoPerShot=0 FlatKnockbackHorizontal=4500.0 FlatKnockbackVertical=7500.0 FlatKnockbackHorizontalMin=-4500.0 FlatKnockbackVerticalMin=4500.0 AIUseInCombat=true AIUseOutOfCombat=false AIUseOnGround=true AIUseInAir=true AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=2000.0 AIMaxTargFOV=15.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices -576.000000 0.000000 256.000000 448.000000 0.000000 256.000000 448.000000 0.000000 -768.000000 -576.000000 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/2939/CH11/EX11.5/Ex11_5.sce

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FOSSEE/Scilab-TBC-Uploads

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Ex11_5.sce

//Ex11_5 clc; //Given: i1=4000;// initial intensity of radiaton i2=2000;// final intensity of radiation density1=8.96;// density of copper l=6.022*10^23;// avogadro constant ue=0.211;// electron absorption coefficent in barn per electron // 1 b=10^(-24) cm^2 //solution: uCu=ue*29;//atomic absorbtion coefficient in b/atom umCu=(6.022*10^23*uCu*10^-24)/63; // mass absorbtion coefficient in cm^2/g ulCu=umCu*density1;// linear absorption coefficient in cm^-1 // we know that, i2=i1*exp(ulCu*x) x=log(i1/i2)/(ulCu);// thickness of the copper plate printf("\n The thickness of copper nedded to reduce the intensity of the radiation in cm is =%f",x)

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/2102/CH1/EX1.10/exa_1_10.sce

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FOSSEE/Scilab-TBC-Uploads

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exa_1_10.sce

// Exa 1.10 clc; clear; close; // Given data format('v',13) Bo= 1.7*10^-5;// in weber/meter^2 miu_o= 4*%pi*10^-7 ;// in weber/amp-meter H= Bo/miu_o;//in A/m disp(H,"The horizontal component of the magnetic intensity in A/m is : ")

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/Metodos/Clase7/ejemplos/integracion/1reglaTrapezoidal.sce

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DavidAlex99/Cursos

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2020-11-14T00:45:57

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1reglaTrapezoidal.sce

clc() clear all function result=f(x) result = 0.2+25*x-200*x^2+675*x^3-900*x^4+400*x^5 endfunction function result=reglaTrapecio(a,b,funcion) result = (b-a)*(funcion(a)+funcion(b))/2 endfunction a = 0 b = 0.8 disp("integral") integral = integrate("0.2+25*x-200*x^2+675*x^3-900*x^4+400*x^5",'x',a,b) disp(integral) aproximacion = reglaTrapecio(a,b,f) disp(aproximacion) disp("error") disp((integral-aproximacion)*100/integral)

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/giarratano/SOURCE/TESTING/testrule.tst

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arranger1044/icse-1516

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2020-12-24T19:04:01.588095

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testrule.tst

(set-dynamic-constraint-checking FALSE) (set-sequence-operator-recognition FALSE) (set-static-constraint-checking TRUE) (set-reset-globals TRUE) (set-auto-float-dividend TRUE) (set-fact-duplication FALSE) (set-incremental-reset TRUE) (set-salience-evaluation when-defined) (set-strategy depth) (open "testrule.rsl" testall "w") (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "example.tst") (printout testall "Completed example.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "memtest.tst") (printout testall "Completed memtest.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "conres.tst") (printout testall "Completed conres.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "fldval50.tst") (printout testall "Completed fldval.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "incrrset.tst") (printout testall "Completed incrrset.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "dynsal.tst") (printout testall "Completed dynsal.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "globltst.tst") (printout testall "Completed globltst.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "rfrshagn.tst") (printout testall "Completed rfrshagn.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "templerr.tst") (printout testall "Completed templerr.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "globlerr.tst") (printout testall "Completed globlerr.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "drtest01.tst") (printout testall "Completed drtest01.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "drtest02.tst") (printout testall "Completed drtest02.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "drtest03.tst") (printout testall "Completed drtest03.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "drtest04.tst") (printout testall "Completed drtest04.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "basicfnx.tst") (printout testall "Completed basicfnx.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "predcfnx.tst") (printout testall "Completed predcfnx.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "multifnx.tst") (printout testall "Completed multifnx.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "strngfnx.tst") (printout testall "Completed strngfnx.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "mathfnx.tst") (printout testall "Completed mathfnx.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "textpro.tst") (printout testall "Completed textpro.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "iofnx.tst") (printout testall "Completed iofnx.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "dffctcmd.tst") (printout testall "Completed dffctcmd.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "dftmpcmd.tst") (printout testall "Completed dftmpcmd.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "dfgblcmd.tst") (printout testall "Completed dfgblcmd.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "factscmd.tst") (printout testall "Completed factscmd.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "memrycmd.tst") (printout testall "Completed memrycmd.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "lgclexe.tst") (printout testall "Completed lgclexe.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "dfrulcmd.tst") (printout testall "Completed dfrulcmd.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "seqop.tst") (printout testall "Completed seqop.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "rulemisc.tst") (printout testall "Completed rulemisc.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) crlf) (batch "pataddtn.tst") (printout testall "Completed pataddtn.tst test" crlf) (clear) (release-mem) (printout testall "Memory use: " (mem-used) 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/68/CH4/EX4.6/ex6.sce

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// Example 4.6; Design of given circuit to obtain I_D=0.5mA and V_D=3V // MOSFET is in saturation V_DD=5; // (V) V_D=3; // (V) I_D=0.5*10^-3; // (A) V_t=-1; // (V) K=1*10^-3; // K=k'_n(W/L) V_OV=sqrt(2*I_D/K); V_GS=V_t+(-V_OV) R_D=V_D/I_D; V_Dmax=V_D-V_t; // - sign as magnitude of V_t is considered R_D=V_Dmax/I_D; disp(R_D,"R_D (ohm)")

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/3669/CH6/EX6.6/6.sce

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//Variable declaration epsilon0=8.85*10**-12; epsilonr=3.75; //dielectric constant gama=1/3; //internal field constant D=2050; //density(kg/m**3) Na=6.02*10**26; //avagadro number M=32; //atomic weight //Calculation N=Na*D/M; //number of atoms(per m**3) alphae=((epsilonr-1)/(epsilonr+2))*3*epsilon0/N; //electronic polarizability(F m**2) //Result printf('electronic polarizability is %0.3f *10**-40 F m**2 \n',(alphae*10**40)) printf('answer varies due to approximating off errors\n')

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/hinfinito1.sce

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sebas220996/lista-de-ejercicios-3-SCA-Caceres

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// CONTROL SUSPENSION DE UN AUTOMOVIL // Alumno: Sebastian Miguel Caceres Huaman // Author: juan C. Cutipa-Luque // Docente: juan C. Cutipa-Luque //Codigo Reutilizado de un ejemplo Mostrado en Clase clf(); // close current figure clear // clear all pasta variables xdel(winsid()) // close all windows //Modelo de la planta k1 = 1; k2 = 4; b1 = 0.2; b2 = 0.1; m1 = 1; m2 = 2; ap = [0 0 1 0; 0 0 0 1; -k1/m1 k1/m1 -b1/m1 b1/m1; k1/m2 -(k1 + k2)/m2 b2/m2 -(b1 + b2)/m2]; bp = [0 0; 0 0; 1/m1 0; 0 1/m2]; cp = [1 0 0 0; 0 1 0 0]; dp = 0*ones (2,2); // Controllability and Observability // Cc=[B, AB, A^2 B,..., A^(n-1) B] Cc = cont_mat(ap,bp) rankCc=rank(Cc) // // O=[C; CA; CA^2;...; CA^(n-1) ] O = obsv_mat(ap, cp) rankO=rank(O) //valores singulares con escalonamiento su = diag( [0.9614, 0.2753] ) sx = diag( [3.157, 11.47, 3.157, 11.47] ) sy = diag( [3.157 3.157] ) ap_ = sx*ap*inv(sx) bp_ = sx*bp*inv(su) cp_ = sy*cp*inv(sx) dp_ = sy*dp*inv(su) //planta aumentada con integradores antes del proyecto de controlador [ns,nc] = size(bp_); //ns = número de entradas; //nc = número de controles; a_1 = [ap_ bp_ ; 0*ones(nc,ns) 0*ones(nc,nc) ]; b_1 = [0*ones(ns,nc); eye(nc,nc)]; c_1 = [cp_ 0*ones(nc,nc)]; d_1 = 0*ones(nc,nc) G = syslin('c', a_1, b_1, c_1, d_1); w = logspace(-3,3); ms=1.7;// 0.3;%1.5; % guarantee overshot Mp < 6dB = 20*log10(2) wbs=0.23;//0.05;%0.23; ee=1e-3;//1e-4 ki=1; // used to give more accurate adjustment to the cut-off frequency wbs // by default set it to 1 // -------- WT Data ------------ mt=1.3;//1.00; % guarantee overshot Mp < 2dB = 20*log10(1.26) wbt=4.1;//9.1;%4.1; ee=1e-3;//1e-4 // -------- WS ------------ s=poly(0,'s'); ws1=(s/ms+wbs)/(s+wbs*ee), ws2=ws1; ws=[ws1,0;0,ws2] //Ws=syslin('c',ws) Ws=blockdiag(ws1,ws2) // -------- WT ------------ s=poly(0,'s'); wt1=(s+wbt/mt)/(ee*s+wbt), wt2=wt1; wt=[wt1,0;0,wt2] //Wt=syslin('c',wt) Wt=blockdiag(wt1,wt2) // -------- WR ------------ s=poly(0,'s'); wr1=s/s, wr2=wr1; wr=[wr1,0;0,wr2] // ------------------ Plot weighting functions svs = svplot(Ws,w); svt = svplot(Wt,w); scf(2); plot2d("ln", w, [-20*log(svs')/log(10) -20*log(svt')/log(10)]) xgrid(12) xtitle("Singular values plot inv(Ws) and inv(Wt)","Frequency (rad/s)", "Amplitude (dB)"); [P,r]=augment(G,'ST'); //[P,r]=augment(g,'SRT'); P = blockdiag(Ws,Wt,eye(G))*P; //P=minreal(P); //trick to tackle when "D12 is not full rank" P.D(1,3)=0.0001; P.D(2,4)=0.0001; r=[2,2] romin=0.0001 romax=2000 nmax=100; //[K,ro]=h_inf(P,r,romin,romax,nmax) // alternatives //[AK,BK,CK,DK,(RCOND)] = hinf(P.A,P.B,P.C,P.D,2,2,4) K = ccontrg(P, [2,2], 1.3) // this is good for me and for this system // -------------- Analysis of the Feeedback Control System [Se,Re,Te]=sensi(G,K) // S=(I+GK)^-1, T=I-S=GK(I+GK)^-1 // ------------------ Plot weighting functions svS = svplot(Se,w); svT = svplot(Te,w); scf(3); plot2d("ln", w,[-20*log(svs')/log(10) 20*log(svS')/log(10)],[-1 -1 2 2],leg="$\overline{\sigma}(W_S^{-1})$@$\underline{\sigma}(W_S^{-1})$@$\overline{\sigma}(S)$@$\underline{\sigma}(S)$") xtitle("","Frequency (rad/s)", "Amplitude (dB)"); xgrid(12) //set(gca(),"auto_clear","off") xtitle("","Frequency (rad/s)", "Amplitude (dB)"); scf(4); plot2d("ln", w,[-20*log(svt')/log(10) 20*log(svT')/log(10)],[-1 -1 2 2],leg="$\overline{\sigma}(W_T^{-1})$@$\underline{\sigma}(W_T^{-1})$@$\overline{\sigma}(T)$@$\underline{\sigma}(T)$") xtitle("","Frequency (rad/s)", "Amplitude (dB)"); xgrid(12) xtitle("","Frequency (rad/s)", "Amplitude (dB)"); // --------------- Open loop and Closed loop analysis -------------- sysOL=G*K sysCL=G*K*inv(eye(2,2)+G*K) // eigenvalues in LHP (Left Half Plane), stable according to RH spec(sysCL.A) sv1= svplot(sysOL,w); sv2= svplot(sysCL,w); scf(5); plot2d("ln", w,[20*log(sv1')/log(10) 20*log(sv2')/log(10)],[2 2 3 3],leg="$\overline{\sigma}(GK)$@$\underline{\sigma}(GK)$@$\overline{\sigma}(T)$@$\underline{\sigma}(T)$") xtitle("","Frequency (rad/s)", "Amplitude (dB)"); xgrid(12) //set(gca(),"auto_clear","off") xtitle("","Frequency (rad/s)", "Amplitude (dB)"); // Time responses in XCOS

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/New LSTMAttn Model/.data/lemma-split/SURPRISE-LANGUAGES/Siouan/dak.tst

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héc̣a V;SG;1;PRS héc̣a V;PL;2;PRS héc̣a V;PL;3;PRS héc̣a V;PL;1;PRS héc̣a V;PL;1+INCL;PRS héc̣a V;SG;3;PRS héc̣a V;SG;2;PRS ehnake V;PL;1;PRS ehnake V;PL;3;PRS ehnake V;SG;1;PRS ehnake V;SG;3;PRS ehnake V;PL;2;PRS ehnake V;SG;2;PRS ehnake V;PL;1+INCL;PRS papsuŋ V;PL;2;PRS papsuŋ V;SG;3;PRS papsuŋ V;SG;2;PRS papsuŋ V;SG;1;PRS papsuŋ V;PL;3;PRS papsuŋ V;PL;1;PRS papsuŋ V;PL;1+INCL;PRS yukape V;PL;3;PRS yukape V;PL;1;PRS yukape V;SG;3;PRS yukape V;PL;1+INCL;PRS yukape V;SG;1;PRS yukape V;PL;2;PRS yukape V;SG;2;PRS yatke V;SG;2;PRS yatke V;PL;1+INCL;PRS yatke V;SG;1;PRS yatke V;PL;1;PRS yatke V;SG;3;PRS yatke V;PL;2;PRS yatke V;PL;3;PRS ḣa V;SG;1;PRS ḣa V;SG;2;PRS ḣa V;PL;3;PRS ḣa V;PL;1+INCL;PRS ḣa V;PL;2;PRS ḣa V;SG;3;PRS ḣa V;PL;1;PRS niwe V;SG;2;PRS niwe V;PL;1;PRS niwe V;PL;2;PRS niwe V;SG;1;PRS niwe V;PL;3;PRS niwe V;PL;1+INCL;PRS niwe V;SG;3;PRS hetaŋhaŋ V;PL;1+INCL;PRS hetaŋhaŋ V;SG;2;PRS hetaŋhaŋ V;PL;1;PRS hetaŋhaŋ V;SG;3;PRS hetaŋhaŋ V;SG;1;PRS hetaŋhaŋ V;PL;2;PRS hetaŋhaŋ 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V;PL;1;PRS ġuye V;PL;1+INCL;PRS ġuye V;SG;1;PRS yużuŋ V;SG;2;PRS yużuŋ V;PL;1+INCL;PRS yużuŋ V;SG;1;PRS yużuŋ V;PL;1;PRS yużuŋ V;PL;2;PRS yużuŋ V;PL;3;PRS yużuŋ V;SG;3;PRS ec̣uŋ V;PL;1+INCL;PRS ec̣uŋ V;PL;1;PRS ec̣uŋ V;SG;3;PRS ec̣uŋ V;SG;1;PRS ec̣uŋ V;SG;2;PRS ec̣uŋ V;PL;2;PRS ec̣uŋ V;PL;3;PRS ṭiṭoḳaŋ i V;PL;2;PRS ṭiṭoḳaŋ i V;PL;1;PRS ṭiṭoḳaŋ i V;SG;3;PRS ṭiṭoḳaŋ i V;SG;2;PRS ṭiṭoḳaŋ i V;SG;1;PRS ṭiṭoḳaŋ i V;PL;1+INCL;PRS ṭiṭoḳaŋ i V;PL;3;PRS (ob) wóhdake V;PL;2;PRS (ob) wóhdake V;PL;1+INCL;PRS (ob) wóhdake V;PL;3;PRS (ob) wóhdake V;SG;1;PRS (ob) wóhdake V;SG;3;PRS (ob) wóhdake V;PL;1;PRS (ob) wóhdake V;SG;2;PRS c̣iŋ V;PL;3;PRS c̣iŋ V;SG;2;PRS c̣iŋ V;PL;2;PRS c̣iŋ V;PL;1+INCL;PRS c̣iŋ V;SG;3;PRS c̣iŋ V;SG;1;PRS c̣iŋ V;PL;1;PRS każużu V;SG;2;PRS każużu V;SG;3;PRS każużu V;SG;1;PRS każużu V;PL;2;PRS każużu V;PL;1+INCL;PRS każużu V;PL;1;PRS każużu V;PL;3;PRS manuŋ V;SG;2;PRS manuŋ V;PL;1;PRS manuŋ V;PL;1+INCL;PRS manuŋ V;PL;2;PRS manuŋ V;PL;3;PRS manuŋ V;SG;1;PRS manuŋ V;SG;3;PRS ihdoi V;PL;1+INCL;PRS ihdoi V;SG;3;PRS ihdoi V;PL;2;PRS ihdoi V;SG;2;PRS ihdoi V;PL;1;PRS ihdoi V;SG;1;PRS ihdoi V;PL;3;PRS yuinaḣni V;PL;2;PRS yuinaḣni V;SG;2;PRS yuinaḣni V;PL;1+INCL;PRS yuinaḣni V;PL;3;PRS yuinaḣni V;SG;3;PRS yuinaḣni V;SG;1;PRS yuinaḣni V;PL;1;PRS kaḣdoke V;PL;2;PRS kaḣdoke V;PL;3;PRS kaḣdoke V;SG;2;PRS kaḣdoke V;SG;3;PRS kaḣdoke V;PL;1+INCL;PRS kaḣdoke V;PL;1;PRS kaḣdoke V;SG;1;PRS iyakaṡke V;PL;3;PRS iyakaṡke V;PL;1;PRS iyakaṡke V;SG;2;PRS iyakaṡke V;SG;3;PRS iyakaṡke V;PL;2;PRS iyakaṡke V;PL;1+INCL;PRS iyakaṡke V;SG;1;PRS waṡte V;PL;2;PRS waṡte V;PL;3;PRS waṡte V;SG;1;PRS waṡte V;SG;3;PRS waṡte V;SG;2;PRS waṡte V;PL;1;PRS waṡte V;PL;1+INCL;PRS anaġoptaŋ V;PL;2;PRS anaġoptaŋ V;SG;3;PRS anaġoptaŋ V;PL;3;PRS anaġoptaŋ V;SG;2;PRS anaġoptaŋ V;PL;1;PRS anaġoptaŋ V;PL;1+INCL;PRS anaġoptaŋ V;SG;1;PRS pasdohaŋ V;PL;2;PRS pasdohaŋ V;SG;3;PRS pasdohaŋ V;PL;1;PRS pasdohaŋ V;PL;1+INCL;PRS pasdohaŋ V;SG;1;PRS pasdohaŋ V;SG;2;PRS pasdohaŋ V;PL;3;PRS wayatke V;PL;2;PRS wayatke V;SG;2;PRS wayatke V;PL;3;PRS wayatke V;PL;1;PRS wayatke V;PL;1+INCL;PRS wayatke V;SG;3;PRS wayatke V;SG;1;PRS wac̣i V;PL;3;PRS wac̣i V;PL;2;PRS wac̣i V;SG;1;PRS wac̣i V;PL;1+INCL;PRS wac̣i V;SG;3;PRS wac̣i V;PL;1;PRS wac̣i V;SG;2;PRS hdoku V;PL;1+INCL;PRS hdoku V;PL;2;PRS hdoku V;PL;1;PRS hdoku V;SG;1;PRS hdoku V;SG;3;PRS hdoku V;SG;2;PRS hdoku V;PL;3;PRS iṡtohmuze V;PL;3;PRS iṡtohmuze V;SG;2;PRS iṡtohmuze V;PL;1+INCL;PRS iṡtohmuze V;SG;1;PRS iṡtohmuze V;SG;3;PRS iṡtohmuze V;PL;1;PRS iṡtohmuze V;PL;2;PRS ṡape V;PL;3;PRS ṡape V;PL;2;PRS ṡape V;SG;1;PRS ṡape V;SG;2;PRS ṡape V;PL;1+INCL;PRS ṡape V;SG;3;PRS ṡape V;PL;1;PRS yahomni V;SG;1;PRS yahomni V;PL;1;PRS yahomni V;PL;2;PRS yahomni V;PL;3;PRS yahomni V;SG;2;PRS yahomni V;PL;1+INCL;PRS yahomni V;SG;3;PRS waṡ'agic̣'iye V;SG;3;PRS waṡ'agic̣'iye V;SG;1;PRS waṡ'agic̣'iye V;PL;1+INCL;PRS waṡ'agic̣'iye V;PL;2;PRS waṡ'agic̣'iye V;PL;3;PRS waṡ'agic̣'iye V;SG;2;PRS waṡ'agic̣'iye V;PL;1;PRS o V;SG;3;PRS o V;SG;2;PRS o V;SG;1;PRS o V;PL;2;PRS o V;PL;3;PRS o V;PL;1;PRS o V;PL;1+INCL;PRS kaḳoḳoke V;PL;1+INCL;PRS kaḳoḳoke V;SG;2;PRS kaḳoḳoke V;PL;1;PRS kaḳoḳoke V;PL;2;PRS kaḳoḳoke V;PL;3;PRS kaḳoḳoke V;SG;3;PRS kaḳoḳoke V;SG;1;PRS waṡtedake V;PL;3;PRS waṡtedake V;PL;1;PRS waṡtedake V;SG;1;PRS waṡtedake V;PL;2;PRS waṡtedake V;SG;3;PRS waṡtedake V;PL;1+INCL;PRS waṡtedake V;SG;2;PRS ḣpaŋye V;PL;3;PRS ḣpaŋye V;SG;2;PRS ḣpaŋye V;PL;1+INCL;PRS ḣpaŋye V;PL;2;PRS ḣpaŋye V;SG;3;PRS ḣpaŋye V;SG;1;PRS ḣpaŋye V;PL;1;PRS ókiye V;PL;2;PRS ókiye V;PL;3;PRS ókiye V;SG;2;PRS ókiye V;SG;1;PRS ókiye V;PL;1;PRS ókiye V;PL;1+INCL;PRS ókiye V;SG;3;PRS ṡakiye V;PL;2;PRS ṡakiye V;PL;1+INCL;PRS ṡakiye V;PL;3;PRS ṡakiye V;PL;1;PRS ṡakiye V;SG;3;PRS ṡakiye V;SG;1;PRS ṡakiye V;SG;2;PRS wac̣iŋye V;SG;1;PRS wac̣iŋye V;PL;3;PRS wac̣iŋye V;PL;1;PRS wac̣iŋye V;PL;2;PRS wac̣iŋye V;SG;3;PRS wac̣iŋye V;SG;2;PRS wac̣iŋye V;PL;1+INCL;PRS iwaṡtedaŋ ec̣uŋ V;SG;1;PRS iwaṡtedaŋ ec̣uŋ V;SG;3;PRS iwaṡtedaŋ ec̣uŋ V;PL;1;PRS iwaṡtedaŋ ec̣uŋ V;PL;2;PRS iwaṡtedaŋ ec̣uŋ V;SG;2;PRS iwaṡtedaŋ ec̣uŋ V;PL;3;PRS iwaṡtedaŋ ec̣uŋ V;PL;1+INCL;PRS wayawa hi V;PL;2;PRS wayawa hi V;SG;1;PRS wayawa hi V;PL;3;PRS wayawa hi V;SG;3;PRS wayawa hi V;SG;2;PRS wayawa hi V;PL;1+INCL;PRS wayawa hi V;PL;1;PRS huwe i V;SG;1;PRS huwe i V;PL;2;PRS huwe i V;PL;3;PRS huwe i V;PL;1+INCL;PRS huwe i V;PL;1;PRS huwe i V;SG;3;PRS huwe i V;SG;2;PRS ḣtani hi V;PL;1;PRS ḣtani hi V;PL;2;PRS ḣtani hi V;SG;2;PRS ḣtani hi V;PL;3;PRS ḣtani hi V;SG;1;PRS ḣtani hi V;PL;1+INCL;PRS ḣtani hi V;SG;3;PRS ípuze V;PL;1+INCL;PRS ípuze V;SG;3;PRS ípuze V;PL;1;PRS ípuze V;SG;2;PRS ípuze V;SG;1;PRS ípuze V;PL;3;PRS ípuze V;PL;2;PRS kai V;SG;2;PRS kai V;PL;1+INCL;PRS kai V;PL;2;PRS kai V;SG;3;PRS kai V;PL;3;PRS kai V;PL;1;PRS kai V;SG;1;PRS inaḣme V;SG;3;PRS inaḣme V;PL;3;PRS inaḣme V;SG;1;PRS inaḣme V;PL;1;PRS inaḣme V;SG;2;PRS inaḣme V;PL;1+INCL;PRS inaḣme V;PL;2;PRS hdużaża V;PL;1;PRS hdużaża V;PL;2;PRS hdużaża V;SG;3;PRS hdużaża V;SG;1;PRS hdużaża V;PL;3;PRS hdużaża V;SG;2;PRS hdużaża V;PL;1+INCL;PRS háŋske V;SG;3;PRS háŋske V;PL;2;PRS háŋske V;PL;3;PRS háŋske V;SG;1;PRS háŋske V;SG;2;PRS háŋske V;PL;1+INCL;PRS háŋske V;PL;1;PRS kahdi V;PL;1;PRS kahdi V;SG;3;PRS kahdi V;SG;1;PRS kahdi V;PL;1+INCL;PRS kahdi V;PL;2;PRS kahdi V;SG;2;PRS kahdi V;PL;3;PRS aohaha V;PL;2;PRS aohaha V;PL;1;PRS aohaha V;PL;3;PRS aohaha V;SG;2;PRS aohaha V;SG;1;PRS aohaha V;PL;1+INCL;PRS aohaha V;SG;3;PRS kaḣape V;SG;3;PRS kaḣape V;SG;1;PRS kaḣape V;PL;2;PRS kaḣape V;PL;1;PRS kaḣape V;PL;3;PRS kaḣape V;PL;1+INCL;PRS kaḣape V;SG;2;PRS (ob) wóta V;SG;1;PRS (ob) wóta V;SG;2;PRS (ob) wóta V;PL;1;PRS (ob) wóta V;SG;3;PRS (ob) wóta V;PL;1+INCL;PRS (ob) wóta V;PL;3;PRS (ob) wóta V;PL;2;PRS ihduṡdoke V;PL;2;PRS ihduṡdoke V;PL;1+INCL;PRS ihduṡdoke V;SG;2;PRS ihduṡdoke V;PL;1;PRS ihduṡdoke V;SG;3;PRS ihduṡdoke V;SG;1;PRS ihduṡdoke V;PL;3;PRS hinażiŋ V;SG;1;PRS hinażiŋ V;PL;1;PRS hinażiŋ V;PL;3;PRS hinażiŋ V;SG;2;PRS hinażiŋ V;SG;3;PRS hinażiŋ V;PL;1+INCL;PRS hinażiŋ V;PL;2;PRS yuwiŋze V;PL;3;PRS yuwiŋze V;PL;2;PRS yuwiŋze V;PL;1+INCL;PRS yuwiŋze V;SG;1;PRS yuwiŋze V;SG;2;PRS yuwiŋze V;SG;3;PRS yuwiŋze V;PL;1;PRS wópeṭuŋ V;PL;2;PRS wópeṭuŋ V;PL;1;PRS wópeṭuŋ V;PL;3;PRS wópeṭuŋ V;SG;3;PRS wópeṭuŋ V;PL;1+INCL;PRS wópeṭuŋ V;SG;1;PRS wópeṭuŋ V;SG;2;PRS yuġaŋ V;PL;2;PRS yuġaŋ V;SG;1;PRS yuġaŋ V;SG;2;PRS yuġaŋ V;SG;3;PRS yuġaŋ V;PL;1;PRS yuġaŋ V;PL;1+INCL;PRS yuġaŋ V;PL;3;PRS éokasiŋ V;PL;2;PRS éokasiŋ V;SG;2;PRS éokasiŋ V;SG;1;PRS éokasiŋ V;PL;1;PRS éokasiŋ V;SG;3;PRS éokasiŋ V;PL;1+INCL;PRS éokasiŋ V;PL;3;PRS ahiṭuŋwe V;SG;1;PRS ahiṭuŋwe V;PL;1;PRS ahiṭuŋwe V;PL;2;PRS ahiṭuŋwe V;PL;1+INCL;PRS ahiṭuŋwe V;PL;3;PRS ahiṭuŋwe V;SG;3;PRS ahiṭuŋwe V;SG;2;PRS uŋspeḳiye V;SG;3;PRS uŋspeḳiye V;SG;1;PRS uŋspeḳiye V;PL;1;PRS uŋspeḳiye V;SG;2;PRS uŋspeḳiye V;PL;1+INCL;PRS uŋspeḳiye V;PL;2;PRS uŋspeḳiye V;PL;3;PRS yubaze V;SG;1;PRS yubaze V;PL;3;PRS yubaze V;SG;3;PRS yubaze V;PL;1+INCL;PRS yubaze V;SG;2;PRS yubaze V;PL;1;PRS yubaze V;PL;2;PRS oihdake V;SG;2;PRS oihdake V;PL;1;PRS oihdake V;SG;3;PRS oihdake V;PL;3;PRS oihdake V;SG;1;PRS oihdake V;PL;2;PRS oihdake V;PL;1+INCL;PRS (ob) ye V;SG;1;PRS (ob) ye V;PL;1;PRS (ob) ye V;PL;3;PRS (ob) ye V;SG;2;PRS (ob) ye V;PL;1+INCL;PRS (ob) ye V;PL;2;PRS (ob) ye V;SG;3;PRS ḳadhde V;SG;1;PRS ḳadhde V;PL;3;PRS ḳadhde V;PL;2;PRS ḳadhde V;SG;3;PRS ḳadhde V;PL;1;PRS ḳadhde V;PL;1+INCL;PRS ḳadhde V;SG;2;PRS spaye V;PL;1+INCL;PRS spaye V;SG;2;PRS spaye V;SG;3;PRS spaye V;PL;2;PRS spaye V;PL;1;PRS spaye V;PL;3;PRS spaye V;SG;1;PRS waŋke V;SG;3;PRS waŋke V;PL;1;PRS waŋke V;PL;2;PRS waŋke V;SG;1;PRS waŋke V;PL;3;PRS waŋke V;PL;1+INCL;PRS waŋke V;SG;2;PRS yuṡpuṡpu V;PL;1+INCL;PRS yuṡpuṡpu V;PL;2;PRS yuṡpuṡpu V;PL;1;PRS yuṡpuṡpu V;PL;3;PRS yuṡpuṡpu V;SG;2;PRS yuṡpuṡpu V;SG;3;PRS yuṡpuṡpu V;SG;1;PRS okiwa V;PL;1;PRS okiwa V;SG;2;PRS okiwa V;SG;1;PRS okiwa V;PL;1+INCL;PRS okiwa V;PL;2;PRS okiwa V;PL;3;PRS okiwa V;SG;3;PRS c̣uwita V;PL;3;PRS c̣uwita V;SG;3;PRS c̣uwita V;SG;1;PRS c̣uwita V;SG;2;PRS c̣uwita V;PL;2;PRS c̣uwita V;PL;1+INCL;PRS c̣uwita V;PL;1;PRS amaġażu V;SG;1;PRS amaġażu V;PL;3;PRS amaġażu V;SG;3;PRS amaġażu V;SG;2;PRS amaġażu V;PL;1+INCL;PRS amaġażu V;PL;2;PRS amaġażu V;PL;1;PRS naġiyeye V;PL;1+INCL;PRS naġiyeye V;PL;2;PRS naġiyeye V;PL;3;PRS naġiyeye V;SG;1;PRS naġiyeye V;PL;1;PRS naġiyeye V;SG;3;PRS naġiyeye V;SG;2;PRS ohoda V;SG;2;PRS ohoda V;PL;1+INCL;PRS ohoda V;SG;3;PRS ohoda V;PL;3;PRS ohoda V;PL;2;PRS ohoda V;SG;1;PRS ohoda V;PL;1;PRS c̣oṗa V;SG;1;PRS c̣oṗa V;PL;3;PRS c̣oṗa V;SG;2;PRS c̣oṗa V;SG;3;PRS c̣oṗa V;PL;1;PRS c̣oṗa V;PL;2;PRS c̣oṗa V;PL;1+INCL;PRS yaoṭaŋiŋ V;SG;3;PRS yaoṭaŋiŋ V;PL;2;PRS yaoṭaŋiŋ V;SG;1;PRS yaoṭaŋiŋ V;PL;1+INCL;PRS yaoṭaŋiŋ V;SG;2;PRS yaoṭaŋiŋ V;PL;3;PRS yaoṭaŋiŋ V;PL;1;PRS ozikiye V;PL;1+INCL;PRS ozikiye V;PL;2;PRS ozikiye V;SG;3;PRS ozikiye V;PL;3;PRS ozikiye V;SG;1;PRS ozikiye V;SG;2;PRS ozikiye V;PL;1;PRS ṭokṡu V;PL;3;PRS ṭokṡu V;SG;1;PRS ṭokṡu V;PL;1+INCL;PRS ṭokṡu V;SG;3;PRS ṭokṡu V;PL;2;PRS ṭokṡu V;PL;1;PRS ṭokṡu V;SG;2;PRS wod i V;SG;3;PRS wod i V;PL;3;PRS wod i V;PL;1+INCL;PRS wod i V;PL;1;PRS wod i V;SG;1;PRS wod i V;SG;2;PRS wod i V;PL;2;PRS yac̣aŋze V;PL;1+INCL;PRS yac̣aŋze V;PL;2;PRS yac̣aŋze V;PL;3;PRS yac̣aŋze V;SG;1;PRS yac̣aŋze V;SG;2;PRS yac̣aŋze V;PL;1;PRS yac̣aŋze V;SG;3;PRS tógeḣpekiye V;PL;1;PRS tógeḣpekiye V;PL;3;PRS tógeḣpekiye V;PL;1+INCL;PRS tógeḣpekiye V;PL;2;PRS tógeḣpekiye V;SG;3;PRS tógeḣpekiye V;SG;2;PRS tógeḣpekiye V;SG;1;PRS icaġe V;SG;3;PRS icaġe V;SG;1;PRS icaġe V;PL;2;PRS icaġe V;PL;3;PRS icaġe V;PL;1+INCL;PRS icaġe V;PL;1;PRS icaġe V;SG;2;PRS ayupte V;PL;1+INCL;PRS ayupte V;PL;1;PRS ayupte V;SG;1;PRS ayupte V;PL;3;PRS ayupte V;SG;3;PRS ayupte V;PL;2;PRS ayupte V;SG;2;PRS ihdoye V;PL;2;PRS ihdoye V;SG;3;PRS ihdoye V;PL;1;PRS ihdoye V;PL;3;PRS ihdoye V;SG;1;PRS ihdoye V;SG;2;PRS ihdoye V;PL;1+INCL;PRS ob i V;PL;1+INCL;PRS ob i V;SG;2;PRS ob i V;PL;2;PRS ob i V;SG;3;PRS ob i V;PL;1;PRS ob i V;PL;3;PRS ob i V;SG;1;PRS ihdohi V;SG;1;PRS ihdohi V;PL;1+INCL;PRS ihdohi V;SG;2;PRS ihdohi V;PL;1;PRS ihdohi V;PL;3;PRS ihdohi V;SG;3;PRS ihdohi V;PL;2;PRS kíciyuhe V;SG;3;PRS kíciyuhe V;SG;1;PRS kíciyuhe V;PL;2;PRS kíciyuhe V;SG;2;PRS kíciyuhe V;PL;3;PRS kíciyuhe V;PL;1;PRS kíciyuhe V;PL;1+INCL;PRS uŋspe V;SG;1;PRS uŋspe V;SG;3;PRS uŋspe V;PL;3;PRS uŋspe V;PL;1;PRS uŋspe V;SG;2;PRS uŋspe V;PL;2;PRS uŋspe V;PL;1+INCL;PRS aḣpeya V;SG;3;PRS aḣpeya V;SG;2;PRS aḣpeya V;PL;3;PRS aḣpeya V;PL;2;PRS aḣpeya V;PL;1;PRS aḣpeya V;PL;1+INCL;PRS aḣpeya V;SG;1;PRS yuṡiŋṡiŋ V;PL;3;PRS yuṡiŋṡiŋ V;SG;3;PRS yuṡiŋṡiŋ V;SG;1;PRS yuṡiŋṡiŋ V;PL;1;PRS yuṡiŋṡiŋ V;PL;1+INCL;PRS yuṡiŋṡiŋ V;SG;2;PRS yuṡiŋṡiŋ V;PL;2;PRS awaciŋ V;SG;1;PRS awaciŋ V;PL;1;PRS awaciŋ V;PL;1+INCL;PRS awaciŋ V;SG;2;PRS awaciŋ V;PL;2;PRS awaciŋ V;PL;3;PRS awaciŋ V;SG;3;PRS yuṭaŋka V;PL;3;PRS yuṭaŋka V;SG;3;PRS yuṭaŋka V;PL;1;PRS yuṭaŋka V;SG;1;PRS yuṭaŋka V;SG;2;PRS yuṭaŋka V;PL;2;PRS yuṭaŋka V;PL;1+INCL;PRS iṭuŋṡni V;PL;1+INCL;PRS iṭuŋṡni V;SG;3;PRS iṭuŋṡni V;PL;1;PRS iṭuŋṡni V;SG;1;PRS iṭuŋṡni V;PL;2;PRS iṭuŋṡni V;PL;3;PRS iṭuŋṡni V;SG;2;PRS ic̣apte V;PL;3;PRS ic̣apte V;PL;2;PRS ic̣apte V;SG;3;PRS ic̣apte V;PL;1+INCL;PRS ic̣apte V;SG;2;PRS ic̣apte V;PL;1;PRS ic̣apte V;SG;1;PRS íyotaŋka V;SG;2;PRS íyotaŋka V;SG;3;PRS íyotaŋka V;PL;2;PRS íyotaŋka V;PL;1+INCL;PRS íyotaŋka V;PL;1;PRS íyotaŋka V;SG;1;PRS íyotaŋka V;PL;3;PRS yuḣdeca V;PL;1+INCL;PRS yuḣdeca V;SG;1;PRS yuḣdeca V;SG;2;PRS yuḣdeca V;SG;3;PRS yuḣdeca V;PL;1;PRS yuḣdeca V;PL;2;PRS yuḣdeca V;PL;3;PRS yukse V;SG;2;PRS yukse V;PL;3;PRS yukse V;PL;1+INCL;PRS yukse V;PL;1;PRS yukse V;SG;1;PRS yukse V;PL;2;PRS yukse V;SG;3;PRS hdicu V;PL;3;PRS hdicu V;SG;1;PRS hdicu V;PL;1+INCL;PRS hdicu V;SG;3;PRS hdicu V;PL;1;PRS hdicu V;SG;2;PRS hdicu V;PL;2;PRS odote V;PL;1;PRS odote V;SG;3;PRS odote V;SG;1;PRS odote V;PL;1+INCL;PRS odote V;SG;2;PRS odote V;PL;3;PRS odote V;PL;2;PRS ṡape ṡni V;PL;1+INCL;PRS ṡape ṡni V;PL;3;PRS ṡape ṡni V;SG;3;PRS ṡape ṡni V;PL;2;PRS ṡape ṡni V;SG;1;PRS ṡape ṡni V;SG;2;PRS ṡape ṡni V;PL;1;PRS wayawa i V;PL;1+INCL;PRS wayawa i V;SG;3;PRS wayawa i V;SG;2;PRS wayawa i V;PL;2;PRS wayawa i V;PL;1;PRS wayawa i V;PL;3;PRS wayawa i V;SG;1;PRS sdohaŋ ye V;PL;2;PRS sdohaŋ ye V;SG;1;PRS sdohaŋ ye V;SG;3;PRS sdohaŋ ye V;PL;1+INCL;PRS sdohaŋ ye V;PL;1;PRS sdohaŋ ye V;PL;3;PRS sdohaŋ ye V;SG;2;PRS itohomni V;PL;3;PRS itohomni V;PL;1+INCL;PRS itohomni V;PL;1;PRS itohomni V;SG;2;PRS itohomni V;PL;2;PRS itohomni V;SG;1;PRS itohomni V;SG;3;PRS kau V;PL;1;PRS kau V;PL;3;PRS kau V;PL;1+INCL;PRS kau V;SG;3;PRS kau V;SG;2;PRS kau V;PL;2;PRS kau V;SG;1;PRS yuide V;SG;1;PRS yuide V;SG;2;PRS yuide V;SG;3;PRS yuide V;PL;1+INCL;PRS yuide V;PL;1;PRS yuide V;PL;3;PRS yuide V;PL;2;PRS

b51b17ba32302c1ab26ec8ec8ff48967d19dd2e5

449d555969bfd7befe906877abab098c6e63a0e8

/1949/CH2/EX2.1/2_1.sce

ad0f0a959b336434c5f5469bb472463a289a6865

[]

no_license

FOSSEE/Scilab-TBC-Uploads

948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1

7bc77cb1ed33745c720952c92b3b2747c5cbf2df

refs/heads/master

2020-04-09T02:43:26.499817

2018-02-03T05:31:52

37,975,407

3

12

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Scilab

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306

sce

2_1.sce

//Chapter-2,Example 2_1,Page 2-30 clc() //Given Data: m=4 //order N=1/5000*10^-2 //N=(a+b) grating element //Calculations: //We know, (a+b)*sin(theta)=m*lam //for longest wavelength, sin(theta)=1 lam=N/m //longest wavelength printf('The longest wavelength is =%.10f m',lam)

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/main.sce

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[]

no_license

hansgillis/scigame

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489d2fc4a0c2780ac011ad368c83812881b4b64d

refs/heads/master

2020-12-24T13:21:48.494208

2015-02-04T18:42:02

30,297,370

0

null

UTF-8

Scilab

false

2,610

sce

main.sce

// initialiseert en importeert scigame module exec("scigame/init.sce"); exec("logic.sce"); function main() // maakt een venster window = Window([800, 600]); // laad een afbeelding in een variabele // image = Image(pathfile, [x, y, breedte, hoogte]) bg = Image("img/background.png", [0, 0, 800, 600]); ball = Image("img/ball.png", [384, 284, 32, 32]); stick_player = Image("img/stick.png", [718, 260, 64, 128]); stick_scibot = Image("img/stick.png", [30, 260, 64, 128]); // maak een sprite object aan, // sprite is een extend image object met meer methodes zoals // move(sprite, dx, dy) // render(sprite, position) // collision(sprite1, sprite2) // sprite = Sprite(window, image) sprite_ball = Sprite(window, ball); sprite_player = Sprite(window, stick_player); sprite_scibot = Sprite(window, stick_scibot); CONST_SPEED = 15; speed = 15; delta = [-speed, 0]; // zolang er niet op escape wordt geklikt... while ~event.poll(-27) if is_hitting_right_bound(window, sprite_ball, delta(1)) then speed = CONST_SPEED; set_x(sprite_ball, window.width / 10 * 6 + sprite_ball.image.width / 2) set_y(sprite_ball, window.height / 2 - sprite_ball.image.height / 2) delta(1) = -speed; delta(2) = 0; elseif is_hitting_left_bound(window, sprite_ball, delta(1)) then speed = CONST_SPEED; set_x(sprite_ball, window.width / 10 * 4 - sprite_ball.image.width / 2) set_y(sprite_ball, window.height / 2 - sprite_ball.image.height / 2) delta(1) = speed; delta(2) = 0; end if collision(sprite_ball, sprite_scibot) then delta = bounce(sprite_ball, sprite_scibot, speed); elseif collision(sprite_ball, sprite_player) then delta = bounce(sprite_ball, sprite_player, -speed); end if is_hitting_lower_bound(window, sprite_ball, delta(2)) then delta(2) = delta(2) * (-1) set_y(sprite_ball, 0); elseif is_hitting_upper_bound(window, sprite_ball, delta(2)) then delta(2) = delta(2) * (-1) set_y(sprite_ball, window.height - sprite_ball.image.height); end ps = get_position(sprite_scibot) pb = get_position(sprite_ball) if ps(2) + sprite_scibot.image.height / 4 < pb(2) - sprite_ball.image.height / 2 then move(sprite_scibot, 0, -speed / 2); elseif ps(2) + sprite_scibot.image.height / 4 * 3 > pb(2) - sprite_ball.image.height / 2 then move(sprite_scibot, 0, speed / 2); end move(sprite_ball, delta(1), delta(2)); set_y(sprite_player, window.height - get_mouse_y() - stick_player.height / 2); // regelt de frames per second tick(); end // sluit alles mooi af destroy(window); endfunction main();

21aaf011477491543dcd2ef287b71183743dff1d

449d555969bfd7befe906877abab098c6e63a0e8

/2339/CH5/EX5.12.1/Ex5_12.sce

e1f88b1771b3a3957ed2085d9533321bb02ef0fc

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no_license

FOSSEE/Scilab-TBC-Uploads

948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1

7bc77cb1ed33745c720952c92b3b2747c5cbf2df

refs/heads/master

2020-04-09T02:43:26.499817

2018-02-03T05:31:52

37,975,407

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596

sce

Ex5_12.sce

clc clear Ms=7.3; //kg/kg of fuel Tfw=46; //in C P=10; //in bar FOE=1.17; //Factor of Evaporation Eff=0.79; Me=FOE*Ms; printf('Equivalent Evaporation: %3.2f kg/kg of coal',Me); printf('\n'); Hfw=192.6; //in kJ/kg Hg=2778.1; //in kJ/kg Tsat=179.9; //in C Cps=2.1; //in kJ/kg K H=(2257*FOE)+Hfw; Tsup=((H-Hg)/Cps)+Tsat; printf('Temperature of Superheated Steam: %3.1f C',Tsup); printf('\n'); CV=(Ms*(H-Hfw))/Eff; printf('Calorific Value: %3.1f kJ/kg',CV); printf('\n');

df32d4618f6e639d8168e1a17deb943c145cb985

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/Rez/bivariate-lcmsr-post_mi/bfi_hp8_bfa_mt_d/~BivLCM-SR-bfi_hp8_bfa_mt_d-PLin-VLin.tst

2fd960cb9b0e75c69258c6e47f02ecc42e257609

[]

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

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~BivLCM-SR-bfi_hp8_bfa_mt_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 0.235037D+00 2 -0.340034D-02 0.183337D-02 3 -0.837864D-01 0.635934D-03 0.437632D+00 4 0.266567D-03 -0.604582D-03 -0.563942D-02 0.373489D-02 5 -0.234541D-03 -0.248378D-04 -0.202905D-02 0.774970D-04 0.234874D-02 6 0.660681D-03 0.429560D-05 0.521289D-03 -0.976605D-04 -0.565049D-05 7 0.787290D-03 -0.103484D-04 -0.163753D-02 -0.400162D-04 -0.191050D-03 8 0.224056D-03 -0.603480D-04 -0.645437D-03 0.641814D-04 0.123067D-04 9 -0.259360D+00 0.544292D-03 -0.994243D-01 0.157584D-01 0.367221D-01 10 -0.219795D+00 -0.350717D-02 0.142959D+00 0.522892D-02 0.112070D+00 11 0.267986D+00 -0.132779D-02 0.643797D-01 -0.117500D-01 -0.116666D-01 12 -0.213568D+00 -0.151645D-01 0.683188D+00 0.233905D-01 0.374197D-01 13 -0.165475D-01 -0.400265D-02 0.821428D-01 0.596373D-03 -0.285225D-01 14 -0.118238D+00 -0.944688D-02 0.830508D-01 0.300649D-02 -0.303542D-02 15 -0.996510D+00 0.183223D-01 0.434005D+00 -0.107689D-01 -0.621134D-01 16 -0.202454D-01 -0.263616D-02 0.916931D-02 0.142020D-02 0.373801D-03 17 0.273702D-02 -0.446901D-03 -0.781602D-03 -0.132762D-04 -0.563768D-03 18 0.186298D+00 0.380010D-01 -0.163021D+00 -0.407267D-01 0.163912D-01 19 0.122105D+00 0.458224D-02 0.400079D-01 -0.439947D-03 0.563497D-02 20 0.795550D-01 -0.325798D-01 0.178146D+01 0.202658D-01 -0.118084D-01 21 -0.121554D+00 0.351739D-03 -0.409170D-01 -0.197030D-02 -0.591108D-02 22 0.575054D-03 -0.217992D-03 0.527059D-03 0.509002D-03 0.279396D-03 23 0.465330D-02 -0.223407D-02 -0.167762D-01 0.123027D-01 -0.129714D-02 24 -0.132306D-02 0.516492D-03 0.283600D-02 -0.497288D-03 0.807969D-04 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.593551D-03 7 0.606714D-03 0.355128D-02 8 -0.352140D-03 -0.420837D-04 0.312385D-02 9 -0.811044D-02 -0.225769D-01 0.189001D-01 0.390940D+02 10 -0.544445D-02 -0.404317D-01 -0.113968D-02 0.114398D+01 0.156200D+02 11 0.236166D-01 0.486983D-01 -0.399166D-01 -0.504336D+01 0.432495D+00 12 -0.240208D-01 -0.775302D-01 0.721520D-01 0.487654D+01 0.227162D+01 13 0.523905D-01 0.122752D+00 -0.328023D-01 -0.105176D+01 -0.269386D+01 14 -0.551120D-01 -0.543960D-01 0.402902D+00 0.272857D+01 0.476965D+00 15 -0.125530D-01 0.629244D-02 -0.102172D-01 -0.451795D+01 -0.773375D+01 16 -0.735247D-03 -0.186945D-02 -0.372241D-03 0.657404D+00 -0.699433D-01 17 0.217440D-03 0.215006D-03 -0.261454D-03 -0.763096D-01 -0.197052D-01 18 -0.378127D-01 -0.729173D-01 -0.879044D-03 -0.150404D+01 -0.385358D+00 19 -0.673202D-02 0.161871D-01 -0.694752D-02 -0.291026D+00 0.690290D-01 20 0.678639D-01 0.126768D-01 -0.365219D+00 -0.905239D+01 0.533323D+01 21 0.890853D-02 -0.916757D-02 0.796732D-02 -0.404693D+00 -0.158455D+00 22 -0.250043D-03 -0.651524D-03 0.253469D-03 0.559623D-01 0.242856D-01 23 -0.135834D-02 -0.338991D-02 -0.115267D-02 -0.967037D-01 0.871999D-01 24 0.999810D-04 0.428213D-03 0.253982D-03 0.305557D-01 -0.148495D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.413156D+02 12 -0.213676D+02 0.171076D+03 13 -0.287800D+00 -0.479954D+01 0.155636D+02 14 -0.504088D+01 0.816679D+01 -0.105118D+02 0.116136D+03 15 -0.242857D+01 0.746969D+01 0.948534D+00 -0.220313D+01 0.138648D+03 16 0.978289D-03 -0.825234D-01 -0.183427D+00 0.176900D+00 0.825817D+00 17 0.143330D-01 -0.587891D-01 0.198571D-01 0.374437D-01 -0.750739D+00 18 -0.382201D+01 0.171832D+02 -0.396734D+01 0.190460D+01 -0.434084D+02 19 -0.416674D+00 0.142422D+01 -0.519378D+00 -0.212879D+01 0.187662D+01 20 0.599898D+01 -0.241311D+02 0.883538D+01 -0.763294D+02 0.112108D+02 21 0.917631D+00 -0.167198D+01 0.805890D+00 0.149361D+01 -0.247111D+01 22 -0.455101D-01 -0.326123D-01 -0.494682D-01 0.771130D-01 0.263090D+00 23 -0.216208D+00 0.133755D+01 -0.234610D+00 -0.390151D+00 0.193079D+00 24 0.869323D-02 -0.158451D+00 0.236730D-01 -0.156724D-01 -0.801621D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.221348D+00 17 -0.165856D-01 0.931027D-02 18 -0.465531D+00 0.274308D+00 0.153744D+03 19 0.160019D-02 -0.291680D-01 -0.101691D+00 0.500625D+01 20 -0.155582D+00 -0.280498D-01 -0.873060D+02 -0.294190D+00 0.551796D+03 21 -0.174398D+00 0.422213D-01 0.240554D+01 -0.464764D+01 -0.158805D+01 22 0.792161D-02 -0.378866D-02 -0.718064D+00 0.342713D-02 0.388385D+00 23 0.661327D-02 -0.281557D-02 -0.976533D+00 -0.570372D-01 0.558150D+01 24 -0.161680D-02 0.524722D-03 0.393168D+00 0.148288D-01 -0.240085D+01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.534544D+01 22 -0.534736D-01 0.836078D-02 23 -0.218934D+00 0.150201D-01 0.876324D+00 24 0.123264D-01 -0.427805D-02 -0.783519D-01 0.256387D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.164 1.000 3 -0.261 0.022 1.000 4 0.009 -0.231 -0.139 1.000 5 -0.010 -0.012 -0.063 0.026 1.000 6 0.056 0.004 0.032 -0.066 -0.005 7 0.027 -0.004 -0.042 -0.011 -0.066 8 0.008 -0.025 -0.017 0.019 0.005 9 -0.086 0.002 -0.024 0.041 0.121 10 -0.115 -0.021 0.055 0.022 0.585 11 0.086 -0.005 0.015 -0.030 -0.037 12 -0.034 -0.027 0.079 0.029 0.059 13 -0.009 -0.024 0.031 0.002 -0.149 14 -0.023 -0.020 0.012 0.005 -0.006 15 -0.175 0.036 0.056 -0.015 -0.109 16 -0.089 -0.131 0.029 0.049 0.016 17 0.059 -0.108 -0.012 -0.002 -0.121 18 0.031 0.072 -0.020 -0.054 0.027 19 0.113 0.048 0.027 -0.003 0.052 20 0.007 -0.032 0.115 0.014 -0.010 21 -0.108 0.004 -0.027 -0.014 -0.053 22 0.013 -0.056 0.009 0.091 0.063 23 0.010 -0.056 -0.027 0.215 -0.029 24 -0.017 0.075 0.027 -0.051 0.010 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.418 1.000 8 -0.259 -0.013 1.000 9 -0.053 -0.061 0.054 1.000 10 -0.057 -0.172 -0.005 0.046 1.000 11 0.151 0.127 -0.111 -0.125 0.017 12 -0.075 -0.099 0.099 0.060 0.044 13 0.545 0.522 -0.149 -0.043 -0.173 14 -0.210 -0.085 0.669 0.040 0.011 15 -0.044 0.009 -0.016 -0.061 -0.166 16 -0.064 -0.067 -0.014 0.223 -0.038 17 0.092 0.037 -0.048 -0.126 -0.052 18 -0.125 -0.099 -0.001 -0.019 -0.008 19 -0.123 0.121 -0.056 -0.021 0.008 20 0.119 0.009 -0.278 -0.062 0.057 21 0.158 -0.067 0.062 -0.028 -0.017 22 -0.112 -0.120 0.050 0.098 0.067 23 -0.060 -0.061 -0.022 -0.017 0.024 24 0.026 0.045 0.028 0.031 -0.023 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 -0.254 1.000 13 -0.011 -0.093 1.000 14 -0.073 0.058 -0.247 1.000 15 -0.032 0.049 0.020 -0.017 1.000 16 0.000 -0.013 -0.099 0.035 0.149 17 0.023 -0.047 0.052 0.036 -0.661 18 -0.048 0.106 -0.081 0.014 -0.297 19 -0.029 0.049 -0.059 -0.088 0.071 20 0.040 -0.079 0.095 -0.302 0.041 21 0.062 -0.055 0.088 0.060 -0.091 22 -0.077 -0.027 -0.137 0.078 0.244 23 -0.036 0.109 -0.064 -0.039 0.018 24 0.008 -0.076 0.037 -0.009 -0.043 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.365 1.000 18 -0.080 0.229 1.000 19 0.002 -0.135 -0.004 1.000 20 -0.014 -0.012 -0.300 -0.006 1.000 21 -0.160 0.189 0.084 -0.898 -0.029 22 0.184 -0.429 -0.633 0.017 0.181 23 0.015 -0.031 -0.084 -0.027 0.254 24 -0.021 0.034 0.198 0.041 -0.638 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.253 1.000 23 -0.101 0.175 1.000 24 0.033 -0.292 -0.523 1.000

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// Variable Declaration V = 1.0 //Infinite bus voltage(p.u) E = 1.0 //e.m.f of finite generator behind transient reactance(p.u) X_T = 0.8 //Transfer reactance(p.u) P_i = 0.5 //Input power(p.u) P_i_d = 0.8 //p.u P_0 = 0.5 //Output power(p.u) P = 0.5 //Power(p.u) // Calculation Section P_m = E*V/X_T //Amplitude of power angle curve(p.u) delta_0 = asin(P_i/P_m) //Radians delta = asin(P_i_d/P_m) //Radians delta_m = %pi-delta //Radians A_acc = P_i_d*(delta-delta_0)-P_m*(cos(delta_0)-cos(delta)) //Possible area of a// Result Sectioneleration A_dec = P_m*(cos(delta)-cos(delta_m))-P_i_d*(delta_m-delta) //Possible area of deceleration // Result Section if (A_acc < A_dec) then printf('System is stable') stability = A_dec/A_acc printf('Margin of stability = %.2f' ,stability) else printf('System is not stable') end

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i = imread('test1.jpg'); corners = detectMinEigenFeatures(i,'MinQuality',0.08); disp(corners);

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/* Rieman M9 n -> numero de intervalos h -> comprimento do intervalo a -> intervalo inferior b -> intervalo superior */ function y = f3(x) y = x^2 + exp(x) endfunction a = 0 b = 2 //n = 100 //h = (b - a)/n h = 0.0078125 n = (b - a)/h f = f3 x = linspace(a, b, n+1) S = 0 for i = 1:n x1 = x(i) A1 = 1 dS = (A1*f(x1))*h S = S + dS end disp(S)

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//Chapter-10,Example10_5,pg10_20 P=4 f=50 N=1455 E1line=415 Ns=120*f/P s=(Ns-N)/Ns fr=s*f E1ph=E1line/sqrt(3) E2ph=0.5*E1ph//K=2 E2r=s*E2ph printf("frequency of rotor e.m.f\n") printf("fr=%.2f Hz\n",fr) printf("magnitude of induced e.m.f standstill\n") printf("E2ph=%.2f V\n",E2ph) printf("magnitude of induced e.m.f running\n") printf("E2r=%.3f V",E2r)

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clc; clear; funcprot(0); function V0 = UpOutPut_BS_MC_Richardson (S0, r, sigma, T, K, B, M, m) delta_t = T/(2*m); // Fine mash // generate a Matrix of mxM normaly distributed r.v. with mean = 0 and ... // sd = sqrt(delta_t) delta_W1 = grand(m, M, "nor", 0, sqrt(delta_t)); delta_W2 = grand(m, M, "nor", 0, sqrt(delta_t)); // Initialize matrices for no barrier hit information nobarrier_hit_fine = ones(1,M); nobarrier_hit_coarse = ones(1,M); // Set initial stock values for first time t=0 Euler_fine = S0; Euler_coarse = S0; // Since in the BS model dSt = r*St*dt + sigma*St*delta_W for i=1:m // Calculation matrices of values for fine grid and for coarse grid // Since grid of fine calculation is twice as fine, twice as many // calculation steps are needed Euler_fine = Euler_fine + r*Euler_fine*delta_t +... sigma.*Euler_fine.*delta_W1(i,:); nobarrier_hit_fine = nobarrier_hit_fine.*(Euler_fine<B); Euler_fine = Euler_fine + r*Euler_fine*delta_t +... sigma.*Euler_fine.*delta_W2(i,:); nobarrier_hit_fine = nobarrier_hit_fine.*(Euler_fine<B); // For the coarse grid, stepsize is twice as large: 2*delta_t // and also both brownian motions are needed for this stepsize Euler_coarse = Euler_coarse + r*Euler_coarse*2*delta_t +... sigma.*Euler_coarse.*(delta_W1(i,:)+delta_W2(i,:)); nobarrier_hit_coarse = nobarrier_hit_coarse.*(Euler_coarse<B); end // Define put option function g function y = g(x) y = max((K - x), 0); endfunction // V_fine = nobarrier_hit_fine.*(g(Euler_fine)*exp(-r*T)); V_coarse = nobarrier_hit_coarse.*(g(Euler_coarse)*exp(-r*T)); // Calculating final result for option price at time t=0 by averaging over... // all simulated prices with the MC simulation V0 = mean(2*V_fine-V_coarse); endfunction // Function from Exercise 12 function V_0 = UpOutPut_BinMod(S_0, r, sigma, T, K, B, M) delta_t = T/M; //calculation of delta_t Beta = (exp(-r*delta_t)+exp((r+sigma^2)*delta_t))/2; //calculation of beta for CRR u=Beta+sqrt((Beta^2)-1); //so u>d is true d=u^-1; //because ud=1 q=(exp(r*delta_t)-d)/(u-d); //calculation of succes probability (u) S=zeros(M+1,M+1); //creation stock price matrix S(1,1)=S_0; //Setting stock price at t=0 as initial price in the stock matrix for i=2:M+1 //Initializing algo for computation of stock price for j=1:i S(j,i)=S(1,1)*u^(j-1)*d^(i-j); //with j upwards and i-j downwards movements end end V=-ones(M+1,M+1); //creating option value matrix V(:,M+1)=max((K-S(:,M+1)), 0); //calculation of option values for last column for i=M:-1:1 //Initializing algo for computation of option price //option value is zero if at current point stock price is higher than the barrier V(1:i,i)=exp(-r*delta_t)*(q*V(2:i+1,i+1)+(1-q)*V(1:i,i+1)).*(S(1:i,i) < B); end V_0 = V(1,1); //setting of first element of the option value matrix as option price at time t=0 endfunction // Set values for the input variables S0 = 100; S_0 = S0; r = 0.05; sigma = 0.2; T = 1; K = 100; B = 110; M = 10000; m = 250; // Run functions and display result V0 = UpOutPut_BS_MC_Richardson (S0, r, sigma, T, K, B, M, m) M = 1000; V_0 = UpOutPut_BinMod(S_0, r, sigma, T, K, B, M) disp("Price of UpOutPut BS_MC_Richardson: "+string(V0)) disp("Price of UpOutPut BinMod: "+string(V_0))

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clc clear //Input data m=0.5//Mass of the sphere in kg vi=100//Initial velocity in m/s vf=20//Final velocity in m/s //Calculations h=(vi^2-vf^2)/(2*9.8)//Height in m PE=(m*9.8*h)//Potential energy in J //Calculations printf('Potential energy of the sphere is %i J',PE)

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clc disp("Example 1.20") printf("\n") disp("calculate dynamic and substrate resistance") printf("Given\n") disp("forward current=20mA,cut in voltage=0.33v") If=20*10^-3 Vf=0.33 Rf=Vf/If If1=If-(10^-2) //min forward current If2=If+(10^-2) //max forward current Vf1=0.31 Vf2=0.35 rd=(Vf2-Vf1)/(If2-If1) rd1=0.026/If rsub=rd-rd1 printf("static forward resistance=\n%f ohm\n",Rf) printf("Dynamic resistance=\n%f ohm\n",rd) printf("Dynamic resistance using forward current=\n%f ohm\n",rd1) printf("substrate resistance=\n%f ohm\n",rsub)

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// ex2.1 function eq = model(x) x1H2O = x(1) F2 = x(2) F3 = x(3) x3H2O = x(4) eq(1) = F1 + F2 - F3 // material balance of the system eq(2) = x1MeOH * F1 + x2MeOH * F2 - x3MeOH * F3 // MeOH balance eq(3) = x1MeOH + x1H2O - 1 // mass fraction constraint eq(4) = x3MeOH + x3H2O - 1 // mass fraction constraint endfunction F1 = 1234 // kg/h x1MeOH = 0.2 x2MeOH = 0 x2H2O = 1.0 x3MeOH = 0.05 guess = [0.1; 100; 100; 0.1] x = fsolve(guess, model) x1H2O = x(1) F2 = x(2) F3 = x(3) x3H2O = x(4) printf("x1H2O=%.2f\n", x1H2O) printf("F2=%.2f\n", F2) printf("F2=%.2f\n", F3) printf("x3H2O=%.2f\n", x3H2O) // Results: // // x1H2O=0.80 // F2=3702.00 // F2=4936.00 // x3H2O=0.95

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R=16;//radius of bar,in mm T=100000;//applied torque,in N.mm G=76923;//shear modulus,in N/mm^2

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clc C=200*10^-6; //Assigning values to parameters V=230; R=20; L=0.2; temp=(1/(L*C))-(R^2/L^2); fr=(1/20*%pi)*sqrt(temp); Zr=L/(C*R); Ir=V/Zr; Zl=sqrt(R^2+(2*%pi*fr*L)^2); Il=V/Zl; Xc=1/(2*%pi*fr*C); Ic=V/Xc; phi=atan(2*%pi*fr*L/R); disp("Hertz",fr,"Resonant frequency");

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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Engineering Thermodynamics by Onkar Singh,Chapter 1,Example 29") V=2;//volume of vessel in m^3 P1=76;//initial pressure or atmospheric pressure in cm of Hg T=(27+273.15);//temperature of vessel in k p=70;//final pressure in cm of Hg vaccum R=8.314;//universal gas constant in KJ/kg k M=2;//molecular weight of H2 disp("gas constant for H2(R1)in KJ/kg k") disp("R1=R/M") R1=R/M disp("say initial and final ststes are given by 1 and 2") disp("mass of hydrogen pumped out shall be difference of initial and final mass inside vessel") disp("final pressure of hydrogen(P2)in cm of Hg") disp("P2=P1-p") P2=P1-p disp("therefore pressure difference(P)in kpa") disp("P=((P1-P2)*101.325)/76") P=((P1-P2)*101.325)/76 disp("mass pumped out(m)in kg") disp("m=((P1*V1)/(R1*T1))-((P2*V2)/(R1*T2))") disp("here V1=V2=V and T1=T2=T") disp("so m=(V*(P1-P2))/(R1*T)") m=(V*P)/(R1*T) disp("now during cooling upto 10 degree celcius,the process may be consider as constant volume process") disp("say state before and after cooling are denoted by suffix 2 and 3") T3=(10+273.15);//final temperature after cooling in k disp("final pressure after cooling(P3)in kpa") disp("P3=(T3/T)*P2*(101.325/76)") P3=(T3/T)*P2*(101.325/76)

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EX21_23.sce

clc;funcprot(0);//EXAMPLE 21.23 // Initialisation of Variables al=9000;..........//Altitude in m Ca=215;...........//Speed of aircraft in m/s TP=750;.............//Thrust power developed in kW p1=0.32;...........//Inlet pressure of air in bar t1=231;.............//Inlet temperature of air in K t3=963;.............//Temperature of gases leaving the combustion chamber in K rpc=5.2;............//Pressure ratio C=42500;..........//Calorific value of fuel in kJ/kg C41=195;.........//Velocity in ducts etac=0.86;..........//Compressor efficiency ga=1.4;............//Ratio of specific heats for air gag=1.33;............//Ratio of specific heats for gases etat=0.86;..........//Turbine efficiency etajt=0.9;..........//Jet tube efficiency cp=1.005;............//Specific heat at constant pressure in kJ/kgK for air cpg=1.087;............//Specific heat at constant pressure in kJ/kgK for gases R=0.29;..................//Gas constant for exhaust gases in kJ/kgK //Calculations t2=t1*(rpc^((ga-1)/ga)); t21=t1+((t2-t1)/etac); mf=(cpg*(t3-t21))/(C-(cpg*(t3-t21))); afr=1/mf;..........//Air fuel ratio t41=round(t3-((cp*(t21-t1))/(cpg*(1+mf)))); t4=t3-((t3-t41)/etat);p4=rpc; rpt=(t3/t4)^(gag/(gag-1));.............//Expansion pressure ratio in turbine rpj=p4/rpt;....................//Expansion pressure ratio in jet tube t5=t41/(rpj^((gag-1)/gag)); Cj=sqrt(etajt*2*((cpg*1000*(t41-t5))+((C41*C41)/2))); etao=((((1+mf)*Cj)-Ca)*Ca)/(1000*mf*C);......//Overall efficiency disp(etao*100,"Overall efficiency in %:") ma=(TP*1000)/((((1+mf)*Cj)-Ca)*Ca);........//Rate of air consumption in kg/s disp(ma,"Rate of air consumption in kg/s:") P=ma*(1+mf)*cpg*(t3-t41);..............//Power developed by the turbine in kW disp(P,"Power developed by turbine in kW:") t51=t41-(((Cj^2)-(C41^2))/(2*1000*cpg)); rhoe=(p1*10^5)/(R*1000*t51);..........//Density of exhaust gases Ajt=(ma*(1+mf))/(Cj*rhoe);.......//Discharge of jet area in m^2 disp(Ajt,"The outlet area of jet tube in m^2:") sfc=(mf*ma*3600)/(1000*(TP/Ca));..........//Specific fuel consumption in kg/thrust-hour disp(sfc,"Specific fuel consumption in kg per kg of thrust:")

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/source/2.3.1/macros/scicos/do_view.sci

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clg55/Scilab-Workbench

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function wdm=do_view(scs_m) wpar=scs_m(1);wdm=wpar(1) if size(wdm,'*')<4 then wdm(3)=0;wdm(4)=0;end Xshift=wdm(3) Yshift=wdm(4) oxc=Xshift+(wdm(1)-80)/2 oyc=Yshift+(wdm(2))/2 plot2d(oxc,oyc,-1,'000') [btn,xc,yc]=xclick(0) //get center of new view Xshift=Xshift+(xc-oxc) Yshift=Yshift+(yc-oyc) wdm(3)=Xshift;wdm(4)=Yshift; xset('alufunction',3);xbasc();xselect(); xsetech([-1 -1 8 8]/6,[Xshift,Yshift ,Xshift+wdm(1),Yshift+wdm(2)]) xset('alufunction',6)

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/851/CH8/EX8.5/Example8_5.sce

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FOSSEE/Scilab-TBC-Uploads

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Example8_5.sce

//clear// //Caption:Syndrome calculator for the(7,4) Cyclic Hamming Code //Example8.5: Syndrome calculator //message sequence = [0,1,1,1,0,0,1] clc; D = poly(0,'D'); g = 1+D+0+D^3; //generator polynomial C1 = 0+D+D^2+D^3+0+0+D^6;//error free codeword C2 = 0+D+D^2+0+0+0+D^6;//middle bit is error [r1,q1] = pdiv(C1,g); S1 = coeff(r1); S1 = modulo(S1,2); disp(r1,'remainder in polynomial form') disp(S1,'Syndrome bits for error free codeword are:') [r2,q2] = pdiv(C2,g); S2 = coeff(r2); S2 = modulo(S2,2); disp(r2,'remainder in polynomial form for errored codeword') disp(S2,'Syndrome bits for errored codeword are:')

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/Chapter6/Ch_6_Eg_6.33.sci

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arvindrachna/Introduction_to_Scilab

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//A program to illustrate the multiple evaluation of a function with single argument. deff('[z]=f(x)','z=x^2') feval (1:10, f)

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vmm_4by4.sci

function [x,y,typ]=vmm_4by4(job,arg1,arg2) // Copyright INRIA x=[];y=[];typ=[]; select job case 'plot' then standard_draw(arg1); case 'getinputs' then [x,y,typ]=standard_inputs(arg1); case 'getoutputs' then [x,y,typ]=standard_outputs(arg1); case 'getorigin' then [x,y]=standard_origin(arg1); case 'set' then x=arg1; graphics=arg1.graphics; model=arg1.model; exprs=graphics.exprs; while %t do [ok,weight_vec,fix_loc,exprs]=scicos_getvalue('Set VMM 4x4 parameters',['Weight vector name';'Fix_location'],list('str',1,'vec',-1),exprs) if ~ok then break,end if ok then model.in=[1]; model.out=[1]; model.rpar= [fix_loc']; model.opar=list(weight_vec); graphics.exprs=exprs; x.graphics=graphics; x.model=model; break; end end case 'define' then fix_loc=[0;0;0]; weight_vec="weight4x4"; model=scicos_model() model.in=[1]; model.in2=[1]; model.intyp=[-1]; model.out=[1]; model.out2=[1]; model.outtyp=[-1]; model.rpar= [fix_loc']; model.opar=list(weight_vec); model.blocktype='d' model.dep_ut=[%f %t] exprs=[weight_vec;sci2exp(fix_loc)]; gr_i=['txt='' VMM 4x4'';';'xstringb(orig(1),orig(2),txt,sz(1),sz(2),''fill'')']; x=standard_define([7 2],model, exprs,gr_i); end endfunction

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clc //initialisation of variables a= 193 //mole^-1 cm^-1 b= 2 //cm c= 1.55*10^-3 //mole l^-1 //CALCULATIONS r= 100/10^(a*b*c) //RESULTS printf (' perentage = %.2f per cent',r)

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sci

mdaq_uart_config.sci

function [x,y,typ] = mdaq_uart_config(job,arg1,arg2) uart_conf_desc = ["UART Config"; "Configures the parameters of the MicroDAQ UART module for serial"; "communication."; ""; "MODULE:"; " 0 - UART0"; " 1 - UART1"; " 2 - UART2"; ""; "Baud Rate:"; " 0 - 2400"; " 1 - 4800"; " 2 - 9600"; " 3 - 19200"; " 4 - 38400"; " 5 - 58600"; " 6 - 115200"; ""; "Data bits: 5..8"; ""; "Parity:"; " 0 - None"; " 1 - Even"; " 2 - Odd"; ""; "Stop Bits: 1 or 2"; ""; "Flow control:" " 0 - None"; " 1 - Hardware"; ""; "Set UART Config block parameters:"]; x=[];y=[];typ=[]; select job case 'set' then x=arg1 model=arg1.model; graphics=arg1.graphics; exprs=graphics.exprs; while %t do try getversion('scilab'); [ok,module,baud_rate,data_bits,parity,stop_bits,flow_control,exprs]=.. scicos_getvalue(uart_conf_desc,.. ['Module:'; 'Baud rate:'; 'Data bits:'; 'Parity:'; 'Stop bits:'; 'Flow control:'],.. list('vec',1,'vec',1,'vec',1,'vec',1,'vec',1,'vec',1),exprs) catch [ok,module,baud_rate,data_bits,parity,stop_bits,flow_control,exprs]=.. getvalue(uart_conf_desc,.. ['Module:'; 'Baud rate:'; 'Data bits:'; 'Parity:'; 'Stop bits:'; 'Flow control:'],.. list('vec',1,'vec',1,'vec',1,'vec',1,'vec',1,'vec',1),exprs) end; if ~ok then break end if module > 2 | module < 0 then ok = %f; message("Use values 0,1 or 2 to set UART module.") end if baud_rate > 6 | baud_rate < 0 then ok = %f; message("Use values 0,1,2,3,4,5 or 6 to set Baud rate.") end if data_bits > 8 | data_bits < 5 then ok = %f; message("Use values 5,6,7 or 8 to set Data bits.") end if parity > 2 | parity < 0 then ok = %f; message("Use values 0,1 or 2 to set Parity.") end if stop_bits > 2 | stop_bits < 1 then ok = %f; message("Use values 1 or 2 to set Stop bits.") end if flow_control > 1 | flow_control < 0 then ok = %f; message("Use values 0 or 1 to set Flow control.") end if ok then [model,graphics,ok] = check_io(model,graphics, [], [], [], []); graphics.exprs = exprs; model.rpar = []; model.ipar = [module, baud_rate+1, data_bits, parity, stop_bits, flow_control]; model.dstate = []; x.graphics = graphics; x.model = model; break end end case 'define' then module = 0; baud_rate = 6; data_bits = 8; parity = 0; stop_bits = 1; flow_control = 0; model=scicos_model() model.sim=list('mdaq_uart_config_sci_sim',5); model.in =[]; model.in2=[]; model.intyp=[]; model.out=[]; model.evtin=[]; model.rpar=[]; model.ipar=[module, baud_rate+1, data_bits, parity, stop_bits, flow_control] model.dstate=[]; model.blocktype='d' model.dep_ut=[%t %f] exprs=[sci2exp(module), sci2exp(baud_rate), sci2exp(data_bits), sci2exp(parity), sci2exp(stop_bits), sci2exp(flow_control)] gr_i=['xstringb(orig(1),orig(2),['''' ; ],sz(1),sz(2),''fill'');'] x=standard_define([4 3],model,exprs,gr_i) x.graphics.in_implicit=[]; x.graphics.exprs=exprs; end endfunction

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psy007/NNPC-CHEMICAL-SIM-

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patest.tst

# Depeopanizer test (from old Hysim manual) units SI $thermo = VirtualMaterials.Peng-Robinson / -> $thermo thermo + propane isobutane n-butane isopentane n-pentane thermo + n-hexane n-heptane n-octane thermo + n-nonane n-decane stab = Tower.Tower() stab.Stage_0 + 10 # twelve stages stab.LiquidPhases = 2 cd stab.Stage_0 l = Tower.LiquidDraw() l.Port.P = 1000 cond = Tower.EnergyFeed(0) estT = Tower.Estimate('T') estT.Value = 25 reflux = Tower.StageSpecification('Reflux') reflux.Value = 2 cd ../Stage_5 f = Tower.Feed() f.Port.T = 50 f.Port.P = 2000 f.Port.MoleFlow = 1000 f.Port.Fraction = .1702 .1473 .1132 .1166 .1066 .0963 .0829 .0694 .0558 .0417 f.Port cd ../Stage_11 l = Tower.LiquidDraw() l.Port.P = 1100 l.Port.Fraction.n-BUTANE = .02 reb = Tower.EnergyFeed(1) estT = Tower.Estimate('T') estT.Value = 100 cd ../Stage_9 pa_source = Tower.VapourDraw() pa_source.Port.MoleFlow = 200 cd ../Stage_7 pa_dest = Tower.Feed() cd .. Stage_9.pa_source.Port -> Stage_7.pa_dest.Port /overhead = Stream.Stream_Material() /overhead.In -> Stage_0.l.Port /bottoms = Stream.Stream_Material() /bottoms.In -> Stage_11.l.Port TryToSolve = 1 # start calculation /overhead.Out /bottoms.Out L V T # remove feed and draw and install VapourPumpAround object TryToSolve = 0 delete Stage_9.pa_source delete Stage_7.pa_dest Stage_9.pa = Tower.VapourPumpAround(7) Stage_7.pa_paR.Port.MoleFlow = 200 Stage_7.pa_paQ.Port.Energy = 0 TryToSolve = 1 /overhead.Out /bottoms.Out Stage_7.pa_paR.Port L V T # delete the pump around delete Stage_9.pa # add liquid pump down Stage_7.pd = Tower.LiquidPumpAround(10) Stage_7.pd.Port.MoleFlow = 300 Stage_10.pd_paQ.Port.Energy = 1000000 /overhead.Out /bottoms.Out Stage_10.pd_paR.Port L V T #Create some pump around variables cd /stab.Stage_7.pd PADeltaT = Tower.PumpAroundDTSpec() cd PADeltaT cd /stab.Stage_7.pd PAReturnT = Tower.PumpAroundReturnTSpec() cd PAReturnT cd /stab.Stage_7.pd PAReturnCv = Tower.PumpAroundReturnPropSpec("Cv") cd PAReturnCv cd /stab TryToSolve = 0 TryToRestart = 0 /stab.EnergyFeed_10_pd_paQ.Energy = TryToSolve = 1 /stab.Variable_7_PAReturnT.T = 54.53 L V T /stab.Variable_7_PAReturnT.T = /stab.Variable_7_PADeltaT.DT = 60 L V T /stab.Variable_7_PADeltaT.DT = /stab.Stage_10.pd_paQ.Port.Energy = 1000000 #lets see if it balances when using efficiencies /bal = Balance.BalanceOp() /bal.NumberStreamsInMat = 1 /bal.NumberStreamsOutMat = 3 /bal.BalanceType = 2 cd / feed = Stream.Stream_Material() cd feed /feed.Out -> /stab.Feed_5_f CloneOut = Stream.ClonePort(0) /feed.CloneOut -> /bal.In0 cd /overhead CloneIn = Stream.ClonePort() /overhead.CloneIn -> /bal.Out0 cd /bottoms CloneIn = Stream.ClonePort() /bottoms.CloneIn -> /bal.Out1 /bal.Out2 /stab.TryLastConverged = 1 /stab.Efficiencies = 0.9 /bal.Out2 /stab.Efficiencies = 0.8 /bal.Out2 /stab.Efficiencies = 1.0 /stab.TryLastConverged = 0 #Now play with vol fracs /stab.TryToRestart = 1 cd /stab.Stage_11.l VolFracs = Tower.VolFractionSpec() cd VolFracs . + n-HEPTANE n-OCTANE n-NONANE cd /stab cd /stab.Stage_11.l StdLiqVolFlows = Tower.ComponentStdVolFlowSpec() cd StdLiqVolFlows . + n-HEXANE n-HEPTANE n-OCTANE n-NONANE cd /stab.Stage_11.l StdLiqVolRecovery = Tower.StdVolRecoverySpec() cd StdLiqVolRecovery . + n-PENTANE n-HEXANE n-HEPTANE n-OCTANE n-NONANE . - n-PENTANE n-HEXANE n-HEPTANE n-OCTANE n-NONANE . + n-PENTANE n-HEXANE n-HEPTANE . - n-PENTANE n-HEXANE n-HEPTANE cd /stab.Stage_11.l StdLiqVolRatio = Tower.StdVolRatioSpec() cd StdLiqVolRatio . + n-BUTANE ISOPENTANE n-PENTANE n-HEXANE / n-PENTANE n-HEXANE n-HEPTANE n-OCTANE . - n-BUTANE ISOPENTANE n-PENTANE n-HEXANE / n-PENTANE n-HEXANE n-HEPTANE n-OCTANE / . + n-BUTANE ISOPENTANE n-PENTANE n-HEXANE / . - n-BUTANE ISOPENTANE n-PENTANE n-HEXANE / n-HEXANE n-HEPTANE n-OCTANE / . + n-BUTANE ISOPENTANE n-PENTANE n-HEXANE / n-HEXANE n-HEPTANE n-OCTANE cd /stab /stab.Variable_0_reflux.Generic = /stab.Variable_11_StdLiqVolRatio.Fraction = 0.986 TryToRestart = 0 L V T /stab.Variable_11_StdLiqVolRatio.Fraction = /stab.Variable_0_reflux.Generic = 2 L V T #Now delete try deleting the stages with the pump around #The following should not work #A stage with a feed from a pump around can not be deleted /stab.Stage_9 - 1 /stab.Stage_7 - 3 #Finally do it right /stab.Stage_6 - 4 copy / paste / /RootClone.stab.L /RootClone.stab.V /RootClone.stab.T

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function h=%r_v_p(h1,h2) // %r_v_p(h1,h2) computes (I+h1*h2)\h1. h1: rational // h2 polynomial //! // Copyright INRIA [m1,n1]=size(h1(2)) [m2,n2]=size(h2) if abs(n1-m2)+abs(m1-n2)<>0 then error('inconsistent dimensions'),end h=(eye(m1,m1)+h1*h2)\h1

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Ex12_8.sce

// Example 12_8 clc;funcprot(0); // Given data T_O=25;// °C P=1;// atm T_1=1000;// K // The combustion equation C_8H_18(l)+12.5(O_2+3.76N_2)--->8CO_2+9H_2O(l)+47N_2 // For 300% excess theoretical air,the reaction is C_8H_18(l)+50(O_2+3.76N_2)--->8CO_2+9H_2O(l)+37.5O_2+188N_2 N_CO2=8;// mol N_H2O=9;// mol N_N2=188;// mol N_O2=37.5;// mol hbar0_fO=-249910;// kJ/kmol (C_8H18) hbar0_fCO2=-393520;// kJ/kmol hbar_CO2=42770;// kJ/kmol hbar0_CO2=9360;// kJ/kmol hbar0_fH2O=-241810;// kJ/kmol hbar_H2O=35880;// kJ/kmol hbar0_H2O=9900;// kJ/kmol hbar0_fN2=0;// kJ/kmol hbar_N2=30130;// kJ/kmol hbar0_N2=8670;// kJ/kmol hbar0_fO2=0;// kJ/kmol hbar_O2=31390;// kJ/kmol hbar0_O2=8680;// kJ/kmol // Calculation H_P=(N_CO2*(hbar0_fCO2+hbar_CO2-hbar0_CO2))+(N_H2O*(hbar0_fH2O+hbar_H2O-hbar0_H2O))+(N_O2*(hbar0_fO2+hbar_O2-hbar0_O2))+(N_N2*(hbar0_fN2+hbar_N2-hbar0_N2));// The enthalpy of the products of combustion in kJ/kmol fuel H_R=hbar0_fO;// The enthalpy of the reactants of combustion in kJ/kmol fuel Q=H_P-H_R;// The heat transfer in kJ/kmol fuel printf("\nThe heat transfer,Q=%6.0f kJ/kmol fuel",Q);

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Ex5_5.sce

// Example 5_5 clc;funcprot(0); // Given data D=1;// Diameter of hose at inlet in inch d=2;// Diameter of hose at outlet in inch // From example 5.4,F_e=rho*Q*V_out F_e=176.8;// The force in N // Calculation // F_c=rho*Q*V_out*[1/2*((A_in/A_out)+(A_out/A_in)-1]; // A_in=4*A_out F_c=F_e*((1/2)*(4+(1/4))-1);// The force exerted on the nozzle by the coupling in N printf("\n The force exerted on the nozzle by the coupling,F_c=%3.1f N",F_c);

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/2183/CH4/EX4.5.b/Ex_4_5_b.sce

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Ex_4_5_b.sce

// Example 4.5.b:Despersion per unit length clc; clear; close; t=0.1*10^-6;//Time in second L=15;//Distance in km dp=(t/L)*10^6;//Despersion per unit length in micro second per Km disp(dp*10^3,"Despersion per unit length in nano second per km")

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/1853/CH3/EX3.6/Ex3_6.sce

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Ex3_6.sce

//calculate the induced emf in the coil A=4e-4 //cross sectional is a squar side u=1 //air core torroidal ring D=25e-2 l=3.14*D N=500 d=4e-2 //cross sectional diameter s=l/(4*3.14*10^-7*u*A) L=N^2/s // self inductance dI=10 dt=50e-3 e=(L*dI)/dt disp('Induced emf=' +string(e)+' volts' , 'Inductance = '+string(L)+' henry' )

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/3012/CH3/EX3.6/Ex3_6.sce

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2020-04-09T02:43:26.499817

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Ex3_6.sce

// Given:- // State 1 p1 = 20.0 // initial pressure in MPa T1 = 520.0 // initial temperature in degree celcius Z1 = 0.83 // compressibility factor R = 8.314 // universal gas constant in SI unit n = 1000.0/18.02 // number of moles in a kg of water // State 2 T2 = 400.0 // final temperature in degree celcius // From table A-1 Tc = 647.3 // critical temperature in kelvin pc = 22.09 // critical pressure in MPa // Calculations Tr = (T1+273)/Tc // reduced temperature Pr = p1/pc // reduced pressure v1 = (Z1*n*R*(T1+273))/(p1*(10**6)) vr = v1*(pc*(10**6))/(n*R*Tc) Tr2 = (T2+273)/Tc PR = 0.69 // at above vr and Tr2 P2 = pc*PR // Results printf( ' The specific volume in state1 is %f m3/kg and the corresponding value obtained from table A-4 is .01551 m^3/Kg',v1) printf( ' The pressure in MPa in the final state is %f MPa and the corresponding value from the table is 15.16Mpa',P2);

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Ex5_03.sce

// Scilab Code Ex5.3 : Page-173 (2013) clc; clear; m = 9.1e-31; // Mass of the electron, kg h = 6.63e-34; // Planck's constant, Js c = 3e+008; // Speed of light, m/s e = 1.6e-19; // Energy equivalent of 1 eV, J/eV V0 = 54; // Potential difference between electrodes, V lambda = h*c/(sqrt(2*m*c^2/e*V0)*e*1e-009); // de Broglie wavelength of the electron, nm printf("\nThe de Broglie wavelength of the electron used by Davisson and Germer = %5.3f nm", lambda); // Result // The de Broglie wavelength of the electron used by Davisson and Germer = 0.167 nm

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nobody51/AP186

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2021-08-28T09:35:55.488122

2017-12-11T21:34:46

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VIPbigCircle.sce

//convolution //display the image F = (imread("C:\Users\ADMIN\Documents\PHYSICS\6thYear\186\AP186\186A6\VIP.png")); f=scf(); imshow(F); isoview(); G = (imread("C:\Users\ADMIN\Documents\PHYSICS\6thYear\186\AP186\186A6\circleAp2.png")); G = bool2s(G); f=scf(); Matplot(G*255); isoview(); //2D FFT of VIP F = rgb2gray(double(F)); fftF = fft2(F); f=scf(); Matplot(imnorm(abs(fftF))*255); isoview(); f=scf(); imshow(uint8(imnorm(abs(fftF))*255)); isoview(); //fftshift of aperature shiftG = fftshift(G); f=scf(); Matplot(shiftG*255); isoview(); //convolution of VIP and aperature newImg = fftF .* shiftG; iNewImg = fft2(newImg); f=scf(); Matplot(imnorm(abs(iNewImg))*255); isoview(); f=scf(); imshow(uint8(imnorm(abs(iNewImg))*255)); isoview(); //this way is FAIL shortcut = convol2d(F,G) f=scf(); Matplot(imnorm(abs(shortcut))*255); isoview(); f=scf(); imshow(uint8(imnorm(abs(shortcut))*255)); isoview();

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2020-05-20T13:36:05.842840

2013-07-31T06:53:59

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# # Small C Interpreter command shell # char _nr, _nc, _ro, _co, *_cp, *_el, _mhz; putchar(c){return sys(c,2,1);} getchar(){return sys(1,2);} puts(b){return sys(b,2,3);} putd(n){return printf("%d\n",n);} putx(n){return printf("%x\n",n);} puto(n){return printf("%o\n",n);} gets(b){return sys(b,80,1,4);} fputc(c,u){return sys(c,u,1);} fgetc(u){return sys(u,2);} fputs(b,u){return sys(b,u,3);} fgets(b,n,u){return sys(b,n,u,4);} sprintf(a0,a1,a2,a3,a4,a5,a6,a7,a8,a9){sys(a0,a1,a2,a3,a4,a5,a6,a7,a8,a9,5);} printf(a0,a1,a2,a3,a4,a5,a6,a7,a8) {char b[128];sys(b,a0,a1,a2,a3,a4,a5,a6,a7,a8,5);puts(b);} sscanf(a0,a1,a2,a3,a4,a5,a6,a7,a8,a9){sys(a0,a1,a2,a3,a4,a5,a6,a7,a8,a9,6);} scanf(a0,a1,a2,a3,a4,a5,a6,a7,a8) {char b[128];gets(b);sys(b,a0,a1,a2,a3,a4,a5,a6,a7,a8,6);} atoi(b){int v;sys(b,"%d",&v,6);return v;} fopen(f,m){return sys(f,m,7);} fread(s,l,u){return sys(s,l,u,8);} fwrite(s,l,u){return sys(s,l,u,9);} fclose(u){return sys(u,10);} fseek(u,o,w){return sys(u,o,w,11);} ftell(u){return sys(u,12);} bdos(a,b){return sys(a,b,13);} system(s){return sys(s,14);} exit(){sys(15);} strcmp(s,t){return sys(s,t,20);} strncmp(s,t,n){return sys(s,t,n,20);} strcpy(s,t){return sys(s,t,21);} strncpy(s,t,n){return sys(s,t,n,21);} strlen(s){return sys(s,22);} malloc(n){return sys(n,23);} free(p){sys(p,24);} debug(n){sys(n,28);} check(n){sys(1,n,28);} dirscan(p,f){return sys(p,f,29);} int86(i,e,r){return sys(i,e,r,30);} memleft(){return sys(31);} entry main() { int f, t; char buf[24]; char line[81]; char program[ memleft()-1024 ]; puts(sys(0)); puts("\nSCI Shell V1.5 20Oct86 Copyright (C) 1986 Bob Brodt\n"); *program='Z'; _mhz=12; _nr=25; _nc=80; _ro=_co=1; _cp="\033[%d;%dH"; _el="\033[0K"; for(;;) { puts("shell> "); line[5]=0; if(gets(line)) { if (!strncmp(line,"edit",4)) sys(atoi(line+4),program,19); else if (!strncmp(line,"list",4)) { f=1; t=32765; if(line[4]) sscanf(line+4,"%d %d",&f,&t); sys(program,f,t,27); } else if (!strncmp(line,"save",4)) sys(line+5,program,26); else if (!strncmp(line,"load",4)) sys(line+5,program,25); else if (!strncmp(line,"exit",4)) return; else if (!strncmp(line,"dir",3)) { if ( !line[3] ) strcpy(line+4,"*.*"); if ( dirscan(line+4,buf) ) { printf("%s\n",buf); while(dirscan(0,buf)) printf("%s\n",buf); } } else printf("\n%d\n",sys(line,program,16)); } } }

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//Example14.2 // to determine the current drawn from the dual power supply clc; clear; close; V = 10 ; // V P = 500 ; // mW // we assume that each power supply provides half power supply to IC P1 = (P/2); // the total power dissipation of the IC // P1 = V*I ; I = P1/V ; disp('the total power dissipation of the IC is = '+string(I)+' mA ');

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nuc1a=50 ncrc=3 nec1a=nuc1a+ncrc nuc1b=132 nt=4 nec1b=nuc1b+nt nc=nec1a+nec1b FECr=1/2 nce=nc*1/FECr nc2=78 net=nc2+nce Dur=20*10^-3//duration Gcbr=net/Dur//Gross channel bit rate disp(Gcbr,'Gross channel bit rate in bits/sec')

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function []=anim(x,teta) //anim(x,teta) animated plot //! // Copyright INRIA lc=l/4, hc=l/5, maxp=maxi(x+l*sin(teta));minp=mini(x+l*sin(teta)); maxx=maxi([x,maxp]);minx=mini([minp,x]) rect=[minx,-l,maxx,l] xset("thickness",2); [m,n]=size(x); isoview(minx,maxx,-l,l+hc); if driver()<>'Pos' then xset("alufunction",6); for k=1:n,dpnd1(x(k),teta(k));dpnd1(x(k),teta(k));end; xset("alufunction",3); else xset('pixmap',1) rect=[minx,-l,maxx,l+hc] for k=1:3:n, xpoly(rect([1 3 3 1]),rect([2,2,4,4]),'lines',1) dpnd1(x(k),teta(k)) xset('wshow') end xset('pixmap',0) end xset("thickness",1); function []=dpnd() //dpnd() scheme of experiment //! isoview(0,100,0,100); lc=20, hc=10, lb=40, teta=.25, xg=40, y1=25, y2=y1+hc, yg=y1+hc/2, x1=xg-lc/2;x2=xg+lc/2, xpoly([x1 x2 x2 x1 x1],[y1,y1,y2,y2,y1],"lines",1), xsegs([xg,xg+lb*sin(teta)],[y2,y2+lb*cos(teta)]), xarc(x1+lc/10-2.5,y1-2.5+2.5,5,5,0,360*64); xarc(x2-5+lc/10-2.5,y1-2.5+2.5,5,5,0,360*64); xsegs([10 90],[y1-5 y1-5]); xarrows([x2 x2+10],[yg yg],3.0); xstring(x2+20,yg,'u (force)',0,0); xset("dashes",1);xsegs([xg xg],[y2 y2+lb]);xstring(xg,y2+lb,' teta',0,0); xset("default"); function []=dpnd1(x,theta) //dpnd() scheme //! lc=l/4, hc=l/5, xg=x, y1=0, y2=y1+hc, yg=y1+hc/2, x1=xg-lc/2;x2=xg+lc/2, xpoly([x1 x2 x2 x1 x1],[y1,y1,y2,y2,y1],"lines",1), xsegs([xg,xg+l*sin(theta)],[y2,y2+l*cos(theta)]), r=lc/4 xarc(x1+lc/10,y1,r,r,0,360*64); xarc(x2-r-lc/10,y1,r,r,0,360*64); function draw(job) [xxr,yyr]=xgetech(); wdim=xget('wdim'); [xxf]=xget("font"); xbasc(); xset("font",2,0); xset("wdim",850,650); hc=l/5, if job==0 then if driver()<>'Pos' then xsetech([0,0,0.5,0.5]); plot2d1("enn",1,y(1,:)');xtitle(' ','t',' position'); xsetech([0.5,0,0.5,0.5]); plot2d1("enn",1,y(2,:)');xtitle(' ','t',' theta'); xsetech([0,0.5,1.0,0.5]); anim(100*y(1,:),100*y(2,:)), else xset('pixmap',1) x=100*y(1,:);teta=100*y(2,:); maxp=maxi(x+l*sin(teta));minp=mini(x+l*sin(teta)); maxx=maxi([x,maxp])+hc;minx=mini([minp,x]) [m,n]=size(x); for k=1:3:n, xsetech([0,0,0.5,0.5]); plot2d1("enn",1,y(1,:)');xtitle(' ','t',' position'); xsetech([0.5,0,0.5,0.5]); plot2d1("enn",1,y(2,:)');xtitle(' ','t',' theta'); xsetech([0,0.5,1.0,0.5]); isoview(minx,maxx,-l,l); dpnd1(x(k),teta(k)) xset('wshow') end xset('pixmap',0) end else if driver()<>'Pos' then xsetech([0,0,0.5,0.5]); plot2d(t1',(kr*yd(5:8,:))');xtitle(' ','time','control'); xsetech([0.5,0,0.5,0.5]); plot2d([t1;t1]',yd([3,7],:)',[1,2],"121",'theta@theta estimated'); xsetech([0,0.5,1.0,0.5]); anim(yd(1,:),yd(3,:)) else xset('pixmap',1) x=100*yd(1,:);teta=100*yd(2,:); maxp=maxi(x+l*sin(teta));minp=mini(x+l*sin(teta)); maxx=maxi([x,maxp])+hc;minx=mini([minp,x]) [m,n]=size(x); for k=1:3:n, xsetech([0,0,0.5,0.5]); plot2d(t1',(kr*yd(5:8,:))');xtitle(' ','time','control'); xsetech([0.5,0,0.5,0.5]); plot2d([t1;t1]',yd([3,7],:)',[1,2],"121",'theta@theta estimated'); xsetech([0,0.5,1.0,0.5]); isoview(minx,maxx,-l,l); dpnd1(x(k),teta(k)) xset('wshow') end xset('pixmap',0) end end xsetech(xxr); xset("font",xxf(1),xxf(2));

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//find.. clc //soltuion //given P=600*1000//W d=4//m N=90//rpm q=2.8//rad B=22.5//deg u=0.28 m=1.5//kg/m T=2400//N v=(%pi*N*d)/60//m/s Tc=m*v^2//N printf("the centrifugl tension is,%f N\n",Tc) T1=T-Tc//N //log(T1/T2)=u*q*cosec(%pi/180*B)=0.8907 T2=T1/7.78//N Ppb=(T1-T2)*v//W printf("power tranmited per belt is,%f W\n",Ppb) //n=P/Ppb// printf("the number of belts are,%f \n",P/Ppb) printf("number of belts are say 20\n")

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cd / label yyy file_add yyy mnemonics.txt branch objects xxx (289 B) yyy (13.1 kB) file_get yyy test_ods_fsed_5_c.tmp exit

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clc clear //Input data T1=15+273//Inlet temperature of air in K p1=1.03//Inlet pressure of air in kg/cm^2 rp=5//Pressure ratio T3=815+273//Temperature of air entering the turbine in K nc=0.83//Adiabatic efficiency of the compressor nt=0.92//Internal engine efficiency of the turbine nr=0.65//Effectiveness of regenerator p2=2.45//Pressure in kg/cm^2 T6=T1//Temperature in K T9=T3//Temperature in K Cp=0.24//Specific heat at constant pressure in kJ/kg.K g=1.4//Ratio of specific heat //Calculations T2=(T1*rp^((g-1)/g))//Temperature in K T4=(T3/rp^((g-1)/g))//Temperature in K Wt=(Cp*(T3-T4))//Isentropic work done in the turbine in kcal/kg of air Wc=(Cp*(T2-T1))//Isentropic work done in the compressor in kcal/kg of air Wr=(Wt/Wc)//Work ratio qa=(Cp*(T3-T2))//Heat added in kcal/kg of air nth=((Wt-Wc)/qa)*100//Thermal efficiency in percent T2i=(T1+((T2-T1)/nc))//Temperature in K T4i=(T3-(nt*(T3-T4)))//Temperature in K Wti=(Cp*(T3-T4i))//work done in the turbine in kcal/kg of air Wci=(Cp*(T2i-T1))//work done in the compressor in kcal/kg of air Wri=(Wti/Wci)//Work ratio qai=(Cp*(T3-T2i))//Heat added in kcal/kg of air nthi=((Wti-Wci)/qai)*100//Thermal efficiency in percent T2ii=(T2i+((T4i-T2i)*nr))//Temperature in K qaii=(Cp*(T3-T2ii))//Heat added in kcal/kg of air nthii=((Wti-Wci)/qaii)*100//Thermal efficiency in percent T5=(T1*(p2/p1)^((g-1)/g))//Temperature in K T5i=(T1+((T5-T1)/nc))//Temperature in K T7=(T1*((rp*p1)/p2)^((g-1)/g))//Temperature in K T7i=(T6+((T7-T6)/nc))//Temperature in K T7ii=(T7i+((T4i-T7i)*nr))//Temperature in K Wcomp=(Cp*((T5i-T1)+(T7i-T6)))//Compressor work in kcal/kg of air Wratio=(Wti/Wcomp)//Work ratio qaa=(Cp*(T3-T7ii))//Heat added in kcal/kg of air nthe=((Wti-Wcomp)/qaa)*100//Thermal efficiency in percent T8=(T3*(p2/(rp*p1))^((g-1)/g))//Temperature in K T8i=(T3-((T3-T8)*nt))//Temperature in K T10=(T9/(p2/p1)^((g-1)/g))//Temperature in K T10i=(T9-((T9-T10)*nt))//Temperature in K T2iii=(T2i+((T10i-T2i)*nr))//Temperature in K Wturb=(Cp*((T3-T8i)+(T3-T10i)))//Compressor work in kcal/kg of air Wratioi=(Wturb/Wci)//Work ratio qaai=(Cp*((T3-T2iii)+(T9-T8i)))//Heat added in kcal/kg of air nthei=((Wturb-Wci)/qaai)*100//Thermal efficiency in percent T7iii=(T7i+((T10i-T7i)*nr))//Temperature in K Wratioii=(Wturb/Wcomp)//Work ratio qaaii=(Cp*((T3-T7iii)+(T9-T8i)))//Heat added in kcal/kg of air ntheii=((Wturb-Wcomp)/qaaii)*100//Thermal efficiency in percent //Output printf('Condition Work ratio Thermal efficiency(in percent)\n (a) %3.3f %3.1f\n (b) %3.2f %3.1f\n (c) %3.2f %3.1f\n (d) %3.2f %3.1f\n (e) %3.3f %3.1f\n (f) %3.3f %3.1f',Wr,nth,Wri,nthi,Wri,nthii,Wratio,nthe,Wratioi,nthei,Wratioii,ntheii)

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Ex3_6.sce

clear // //variable declaration AB=2.0 //length of beam AB,m BD=2.0 //length of beam BD,m DF=2.0 //length of beam DF,m FH=3.0 //length of beam FH,m FG=4.0 //length of beam FG,m PF=12.0 //Vertical Load at point F,KN PH=20.0 //Vertical Load at point H,KN //mistake in book FG=4.0 , given FG=2.0 theta1=atan(FG/(AB+BD+DF)) theta3=atan(FG/FH) theta2=theta3 //sum of all vertical forces & sum of all horizotal forces is zero //joint H FHG=PH/sin(theta3) printf("\n FHG= %0.0f KN (Comp.)",FHG) FHF=FHG*cos(theta2) printf("\n FHF= %0.0f KN (Tension)",FHF) //taking moment at G RA=PH*FH/(AB+BD+DF) RG=RA+PF+PH //joint A //sum of all vertical forces & sum of all horizotal forces is zero FAC=RA/sin(theta1) printf("\n FAC= %0.4f KN (Comp.)",FAC) FAB=FAC*cos(theta1) printf("\n FAB= %0.0f KN (Tension)",FAB) //joint B //sum of all vertical forces & sum of all horizotal forces is zero FBC=0 printf("\n FBC= %e ",FBC) FBA=FAB FBD=FBA printf("\n FBD=FBA %0.0f KN (Tension)",FBD) //Joint C: Sum of Forces normal to AC = 0, gives FCD =0 since FBC = 0 ,sum of Forces parallel to CE =0 FCA=FAC FCE=FCA printf("\n FCE=FCA %0.4f KN (Comp.)",FCE) //joint D //sum of all vertical forces & sum of all horizotal forces is zero FDE=0 printf("\n FDE= %e ",FDE) FDB=FBD FDF=FDB printf("\n FDF=FDB %0.0f KN (Tension)",FDF) //Joint E: sum of Forces normal to CG = 0, gives FEF = 0 and sum of Forces in the direction of CG = 0, gives FEF=0 FEG=FCE printf("\n FEG=FCE= %0.4f KN (Comp.)",FEG) //Joint F: //sum of all vertical forces & sum of all horizotal forces is zero FFG=PF printf("\n FFG= %0.0f KN (Tension)",FFG)

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2021-08-23T05:30:24.864657

2017-12-03T17:05:35

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sci

rotation.sci

function X_rot=rotation(X,R) [n,l]=size(X) for i = 1:n X_rot(i,:)=X(i,:)*R; end endfunction

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/scilab/physique/elec/1er_ordre.sce

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scls19fr/openphysic

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refs/heads/master

2021-04-30T23:16:26.197961

2020-11-16T20:21:17

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sce

1er_ordre.sce

clear(); xbasc(); xdel(); tau = 5; t=0:0.1:30; u=exp(-t/tau); legends('tau = 5s',2,1); xtitle('1er ordre','t (s)','U (V)') plot(t,u,t,0);

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/1835/CH2/EX2.4/Ex2_4.sce

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FOSSEE/Scilab-TBC-Uploads

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2018-02-03T05:31:52

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sce

Ex2_4.sce

//CHAPTER 2,ILLUSTRATION 4 PAGE 59 //TITLE:TRANSMISSION OF MOTION AND POWER BY BELTS AND PULLEYS clc clear //==================================================================================== //INPUT D1=.5// DIAMETER OF 1ST SHAFT IN m D2=.25// DIAMETER OF 2nd SHAFT IN m C=2// CENTRE DISTANCE IN m N1=220// SPEED OF 1st SHAFT T1=1250// TENSION ON TIGHT SIDE IN N U=.25// COEFFICIENT OF FRICTION PI=3.141 e=2.71 //==================================================================================== //CALCULATION L=(D1+D2)*PI/2+((D1+D2)^2/(4*C))+2*C F=(D1+D2)/(2*C) ALPHA=asind(F) THETA=(180+(2*ALPHA))*PI/180// ANGLE OF CONTACT IN radians T2=T1/(e^(U*THETA))// TENSION ON SLACK SIDE IN N V=PI*D1*N1/60// VELOCITY IN m/s P=(T1-T2)*V/1000// POWER IN kW //==================================================================================== //OUTPUT printf('\nLENGTH OF BELT REQUIRED =%f m',L) printf('\nANGLE OF CONTACT =%f radians',THETA) printf('\nPOWER CAN BE TRANSMITTED=%f kW',P)

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/866/CH14/EX14.2/14_2.sce

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2021-01-22T04:15:15.512674

2017-09-19T11:51:56

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2017-05-25T21:09:19

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sce

14_2.sce

clc //initialisation of variables load= 50000 //N torque= 1200 //Nm d= 60//mm t= 1.5 //mm alpha= 60 //degrees //CALCULATIONS BM= load*t axialload= (load*4)/(%pi*d^2) bendingmoment= (BM*d*64)/(%pi*d^4*2) Ts= axialload+bendingmoment shearstress= (torque*10^3*d*32)/(2*%pi*d^4) sigman= -Ts*(cosd(alpha-30))^2+shearstress*cosd(alpha-30)*sind(alpha-30)+shearstress*cosd(alpha-30)*sind(alpha-30) T= -Ts*sind(alpha)*cosd(alpha)-shearstress*(sind(alpha))^2+shearstress*(cosd(alpha)^2) //RESULTS printf ('direct stress= %.1f N/mm^2',sigman) printf (' \n Shear stress=%.1f N/mm^2',T)

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/3638/CH11/EX11.3/Ex11_3.sce

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2020-04-09T02:43:26.499817

2018-02-03T05:31:52

37,975,407

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sce

Ex11_3.sce

//Introduction to Fiber Optics by A. Ghatak and K. Thyagarajan, Cambridge, New Delhi, 1999 //Example 11.3 //OS=Windows XP sp3 //Scilab version 5.5.2 clc; clear; //given R1=0.99;//reflection coefficient of mirror 1 R2=0.9;//reflection coefficient of mirror 2 l=10;//Distance between the two mirrors in cm alpha=0;//average loss coefficient per unit length of resonator in cm^(-1) Vth=alpha-log(R1*R2)/(2*l);//Corresponding threshold gain coefficient in cm^(-1) mprintf("\n The threshold gain coefficient = %e cm^-1",Vth);//The answers vary due to round off error

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/3012/CH13/EX13.5/Ex13_5.sce

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2020-04-09T02:43:26.499817

2018-02-03T05:31:52

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1,125

sce

Ex13_5.sce

// Given:- // When expressed on a per mole of fuel basis, the balanced chemical equation obtained in the solution to Example 13.2 takes the form // CH4 + 2.265O2 + 8.515N2 ----- .951CO2 + .049CO + .289O2 + 8.515N2 + 2H2O cpbar = 38.00 // specific heat in KJ/kmol.K // From table A-25 hfnotbar = -74850.00 // enthalpy of formation for methane // From table A-23 deltahbarO2 = 14770-8682 deltahbarN2 = 14581-8669 // Calculations hRbar = hfnotbar + cpbar*(400-298) + 2.265*deltahbarO2 + 8.515*deltahbarN2 // in kj/kmol // With enthalpy of formation values for CO2, CO, and H2O(g) from Table A-25 and enthalpy values from Table A-23 hpbar = .951*(-393520 + (88806 - 9364)) + .049*(-110530 + (58191 - 8669)) + .289*(60371 - 8682) + 8.515*(57651 - 8669) + 2*(-241820 + (72513 - 9904)) Qcvdot = hpbar - hRbar // in kj/kmol // Result printf( ' The rate of heat transfer from the combustion chamber in kJ per kmol of fuel is: %.2f',Qcvdot)

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2021-01-17T12:38:05.661769

2019-01-03T12:03:53

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sci

parallel.sci

function [varargout]=parallel(varargin) //function parallel //Parallel connection of two input/output models. // |--------| // | |--------->z1 // v1-------->| SYS1 | // u1 +-->| |----+ y1 // | |--------| | // | o------>y // u---->+ | // | |--------| | // u2 +-->| |----+ y2 // | SYS2 | // v2------->| |---------->z2 // |--------| // //SYS=PARALLEL(SYS1,SYS2) connects the input/output models SYS1 and SYS2 in // parallel.All the inputs SYS1 and SYS2 are connected correspondingly and corresponding // O/P are summed.If one of the system is SISO and other is MIMO then for every MIMO // corresponding system for i/p and o/p the SISO system is paralleled. // // SYS = PARALLEL(SYS1,SYS2,IN1,IN2,OUT1,OUT2) connects the input/output models // SYS1 and SYS2 in parallel. The inputs specified by IN1 and IN2 are connected // and the outputs specified by OUT1 and OUT2 are summed.The vectors IN1 and IN2 contain // indices into the input vectors of M1 and M2, respectively, and define // the input channels u1 and u2 in the diagram. Similarly, the vectors // OUT1 and OUT2 contain indexes into the outputs of M1 and M2. // //[A,B,C,D] = PARALLEL(A1,B1,C1,D1,A2,B2,C2,D2) produces a state- // space system consisting of the parallel connection of systems 1 // and 2 that connects all the inputs together and sums all the // outputs of the two systems, Y = Y1 + Y2 (o/p of SYS1(A1,B1,C1,D1) and SYS2(A2,B2,C2,D2)). // //[A,B,C,D] = PARALLEL(A1,B1,C1,D1,A2,B2,C2,D2,IN1,IN2,OUT1,OUT2) // connects the two systems in parallel such that the inputs // specified by IN1 and IN2 are connected and the outputs specified // by OUT1 and OUT2 are summed. The vectors IN1 and IN2 contain // indexes into the input vectors of system 1 and system 2, // respectively. Similarly, the vectors OUT1 and OUT2 contain // indexes into the outputs of the systems. The parallel connection // is performed by appending the two systems, summing the specified // inputs and outputs, and removing the, now redundant, inputs and // outputs of system 2. // // [NUM,DEN] = PARALLEL(NUM1,DEN1,NUM2,DEN2) produces a parallel // connection of the two transfer function systems. // // SYS=PARALLEL(SISOarray,'v',SYS2) // SYS=PARALLEL(SYS2,SISOarray,'v') // connects the input/outputs of every element in siso array with SYS2 in // parallel. // // SYS=PARALLEL(SISOarray1,SISOarray2) // connects all the tf of first SISO array to second SISO array element wise in parallel. //Examples:- // s=%s;sys1=syslin('c',1/(500*s^2));sys2=syslin('c',(s+1)/(s+2)); //sys=parallel(sys1,sys2); //a1=[1 2;3 4];b1=[2 3;4 5];c1=[3 4;5 6];d1=[4 5;6 7];a2=[1 4;3 4];b2=[2 6;4 5];c2=[7 4;5 6];d2=[4 9;6 7]; //aa=syslin('c',a1,b1,c1,d1);bb=syslin('c',a2,b2,c2,d2); // sys=parallel(aa,bb,1,2,2,1); //[a b c d]=parallel(a1,b1,c1,d1,a2,b2,c2,d2,1,2,2,1); // //Author:-Paresh Yeole emailid:-yeoleparesh@students.vnit.ac.in [lhs,rhs]=argn(0); ni=length(varargin); nd=length(varargout); kk=1; select rhs //-----------------------------------------------------two systems case without vectors ---------------------------------------------// case 2 then if (and(typeof(varargin(1))<>['rational','state-space']) & and(typeof(varargin(2))<>['rational','state-space'])) then error("parallel:Wrong type of input arguments for given no. of input arguments"); end for i=1:2 if (varargin(i).dt=='d') then varargin(i).dt=1; end end if ((varargin(1).dt)<>(varargin(2).dt)) then error("parallel:sampling time must agree"); end if(size(varargin(1))<>[1 1] & size(varargin(2))<>[1 1]) then if(size(varargin(1))<>size(varargin(2))) then error("Incompatible sizes of the systems"); else varargout(1)=varargin(1)+varargin(2); end elseif(size(varargin(1))==[1 1] & size(varargin(2))==[1 1]) then varargout(1)=varargin(1)+varargin(2); elseif((size(varargin(1))==[1 1] | size(varargin(2))==[1 1]) & (typeof(varargin(1))=='state-space' | typeof(varargin(2))=='state-space')) then //disp("remain to code"); [ny1,nu1] = size(varargin(1)); [ny2,nu2] = size(varargin(2)); if(size(varargin(1))==[1 1]) then if(typeof(varargin(1))=='state-space') then sys=(varargin(1)); else sys=minss(tf2ss(varargin(1))); end a=sysdiag(sys.a,varargin(2).a); sys.b=sys.b*ones(size(sys.b,'c'),size(varargin(2).b,'c')); b=cat(1,sys.b,varargin(2).b); sys.c=ones(size(varargin(2).c,'c'),size(sys.c,'r'))*sys.c; c=cat(2,sys.c,varargin(2).c); d=varargin(2).d elseif(size(varargin(2))==[1 1]) then if(typeof(varargin(2))=='state-space') then sys=(varargin(2)); else sys=minss(tf2ss(varargin(2))); end a=sysdiag(varargin(1).a,sys.a); sys.b=sys.b*ones(size(sys.b,'c'),size(varargin(1).b,'c')); b=cat(1,varargin(1).b,sys.b); // disp(b); sys.c=ones(size(varargin(1).c,'c'),size(sys.c,'r'))*sys.c; c=cat(2,varargin(1).c,sys.c); d=varargin(1).d; end varargout(1)=syslin(varargin(1).dt,a,b,c,d); else varargout(1)=varargin(1)+varargin(2); end //-----------------------------------------------two systems case with polynomials case---------------------------------// case 4 then num1 = coeff(varargin(1)); den1 =coeff(varargin(2)); num2 = coeff(varargin(3)); den2 = coeff(varargin(4)); if((length(num1)<=length(den1)) & (length(num2)<=length(den2)) ) then [nn,mn] = size(num1); for k=1:nn a(k,:) = conv(num1(k,:),den2) + conv(num2(k,:),den1); b = conv(den1,den2); end varargout(1)=a; varargout(2)=b; else error("parallel:input transfer function must be proper"); end //----------------------------------------------two systems case with vector i/ps and o/ps--------------------------------------------// case 6 then /////case-parallel(sys1,sys2,inp1,inp2,out1,out2) if (and(typeof(varargin(1))<>['rational','state-space']) & and(typeof(varargin(2))<>['rational','state-space'])) then error("parallel:Wrong type of input arguments for given no. of input arguments"); end for i=1:2 if (varargin(i).dt=='d') then varargin(i).dt=1; end end if ((varargin(1).dt)<>(varargin(2).dt)) then error("parallel:sampling time must agree"); end [e f g h]=varargin(3:6); [ny1,nu1] = size(varargin(1)); [ny2,nu2] = size(varargin(2)); //State space systems with selection vectors if(e>ny1 | f>ny2) then error("parallel:specified inputs are out of range"); end if(g>nu1 | h>nu2) then error("parallel:specified outputs are out of range"); end inputs1 = e; outputs1 = g; inputs2 = f+nu1; outputs2 = h+ny1; // [a b c d]=abcd(varargin(1)); // [a1 b1 c1 d1]=abcd(varargin(2)); // //Check sizes if (length(inputs1)<>length(inputs2)) then error('Input sizes don''t match.'); elseif (length(outputs1)<>length(outputs2)) then error('Output sizes don''t match.'); end if(typeof(varargin(1))=='state-space' | typeof(varargin(2))=='state-space') then if((typeof(varargin(1))<>'state-space') & (size(varargin(1),'*')<>1 | size(varargin(2),'*')<>1 ) ) then varargin(1)=minss(tf2ss(varargin(1))); elseif (typeof(varargin(2))<>'state-space' & (size(varargin(1),'*')<>1 | size(varargin(2),'*')<>1) ) then varargin(2)=minss(tf2ss(varargin(2))); end sys=sysdiag(varargin(1),varargin(2)); a=sys.a;b=sys.b;c=sys.c;d=sys.d; b(:,inputs1)=b(:,inputs1)+b(:,inputs2); d(:,inputs1)=d(:,inputs1)+d(:,inputs2); c(outputs1,:)=c(outputs1,:)+c(outputs2,:); d(outputs1,:)=d(outputs1,:)+d(outputs2,:); b(:,inputs2) = []; d(:,inputs2) = []; c(outputs2,:) = []; d(outputs2,:) = []; varargout(1)=syslin('c',a,b,c,d); else sys=sysdiag(varargin(1),varargin(2)); sys(:,inputs1)=sys(:,inputs1)+sys(:,inputs2); sys(outputs1,:)=sys(outputs1,:)+sys(outputs2,:); sys(:,inputs2) = []; sys(outputs2,:) = []; varargout(1)=sys; end //-----------------------------------------------------------state-space case of 8------------------------------------------------------------------// case 8 then //disp("hi") ////state space systems [a b c d]=varargin(1:4); [a1 b1 c1 d1]=varargin(5:8); if(size(b)<>[mtlb_size(a,1),mtlb_size(d,2)] | size(c)<>[mtlb_size(d,1),mtlb_size(a,2)] | size(d)<>[mtlb_size(c,1),mtlb_size(b,2)] | issquare(a)==%F) then error('wrong size of matrices given for state space model'); end if(size(b1)<>[mtlb_size(a1,1),mtlb_size(d1,2)] | size(c1)<>[mtlb_size(d1,1),mtlb_size(a1,2)] | size(d1)<>[mtlb_size(c1,1),mtlb_size(b1,2)] | issquare(a1)==%F) then error('wrong size of matrices given for state space model'); end [ny1,nu1] = size(d); [ny2,nu2] = size(d1); // State space systems w/o selection vectors inputs1 = [1:nu1]; outputs1 = [1:ny1]; inputs2 = [1:nu2]; outputs2 = [1:ny2]; //Check sizes if (length(inputs1)<>length(inputs2)) then error('Input sizes don''t match.'); elseif (length(outputs1)<>length(outputs2)) then error('Output sizes don''t match.'); end sys1=syslin('c',a,b,c,d); sys2=syslin('c',a1,b1,c1,d1); sys=sys1+sys2; varargout(1)=sys.a; varargout(2)=sys.b; varargout(3)=sys.c; varargout(4)=sys.d; //-------------------------------------------------------Case of 12 - state-space matrices--------------------------------------------------------------------------------// case 12 then [a b c d]=varargin(1:4); [a1 b1 c1 d1]=varargin(5:8); if(size(b)<>[mtlb_size(a,1),mtlb_size(d,2)] | size(c)<>[mtlb_size(d,1),mtlb_size(a,2)] | size(d)<>[mtlb_size(c,1),mtlb_size(b,2)] | issquare(a)==%F) then error('wrong size of matrices given for state space model'); end if(size(b1)<>[mtlb_size(a1,1),mtlb_size(d1,2)] | size(c1)<>[mtlb_size(d1,1),mtlb_size(a1,2)] | size(d1)<>[mtlb_size(c1,1),mtlb_size(b1,2)] | issquare(a1)==%F) then error('wrong size of matrices given for state space model'); end [ny1,nu1] = size(d); [ny2,nu2] = size(d1); [e f g h]=varargin(9:12); if(e>ny1 | f>ny2) then error("parallel:specified inputs are out of range"); end if(g>nu1 | h>nu2) then error("parallel:specified outputs are out of range"); end //State space systems with selection vectors inputs1 = e; outputs1 = g; inputs2 = f+nu1; outputs2 = h+ny1; //Check sizes if (length(inputs1)<>length(inputs2)) then error('Input sizes don''t match.'); elseif (length(outputs1)<>length(outputs2)) then error('Output sizes don''t match.'); end sys1=syslin('c',a,b,c,d); sys2=syslin('c',a1,b1,c1,d1); //sys=sys1+sys2; sys=sysdiag(sys1,sys2);a=sys.a;b=sys.b;c=sys.c;d=sys.d; b(:,inputs1)=b(:,inputs1)+b(:,inputs2); d(:,inputs1)=d(:,inputs1)+d(:,inputs2); c(outputs1,:)=c(outputs1,:)+c(outputs2,:); d(outputs1,:)=d(outputs1,:)+d(outputs2,:); b(:,inputs2) = []; d(:,inputs2) = []; c(outputs2,:) = []; d(outputs2,:) = []; varargout(1)=a; varargout(2)=b; varargout(3)=c; varargout(4)=d; case 3 then if (and(typeof(varargin(1))<>['rational','state-space']) & and(typeof(varargin(2))<>['rational','state-space','string']) & and(typeof(varargin(3))<>['rational','state-space','string'])) then error("parallel:Wrong type of input arguments and string v is expected to pass with SISO array with MIMO/SISO "); end // if(typeof(varargin(2))<>'rational') then // error("parallel:to pass SISO array with MIMO SISO array must be the 2nd i/p argument"); // end for i=1:3 if(typeof(varargin(i))=='string') then sisoindex=i; continue; end if (varargin(i).dt=='d') then varargin(i).dt=1; end end if(varargin(sisoindex)<>'v') then error("parallel:string v is expected as after SISO array with MIMO/SISO systems"); end sisoarray=varargin(sisoindex-1); if(sisoindex==2) then if ((varargin(1).dt)<>(varargin(3).dt)) then error("parallel:sampling time must agree"); end mimo=varargin(3); if(typeof(varargin(3))=='rational') then mimo=minss(tf2ss(varargin(3))); end elseif(sisoindex==3) then if ((varargin(1).dt)<>(varargin(2).dt)) then error("parallel:sampling time must agree"); end mimo=varargin(1); if(typeof(varargin(1))=='rational') then mimo=minss(tf2ss(varargin(1))); end end for i=1:size(sisoarray,'r') for j=1:size(sisoarray,'c') for k=1:size(sisoarray,3) sys=minss(tf2ss(sisoarray(i,j,k))); a=sysdiag(mimo.a,sys.a); sys.b=sys.b*ones(size(sys.b,'c'),size(mimo,'c')); b=cat(1,mimo.b,sys.b); sys.c=ones(size(mimo,'c'),size(sys.c,'r'))*sys.c; c=cat(2,mimo.c,sys.c); d=sys.d+mimo.d; t=syslin(varargin(1).dt,a,b,c,d); disp(msprintf(gettext("OUTPUT--%d*%d*%d"),i,j,k)) disp(t); //kk=kk+1; end end end varargout(1)=(msprintf(gettext("%d*%d*%d state-space array"),size(sisoarray,'r'),size(sisoarray,'c'),size(sisoarray,3))); else error("Wrong No. of i/p arguments"); end; endfunction // //_________________________________________________________

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s=%s ;// convert to state space TFcont=syslin ('c',20*(4*s+2)/(s^3+5*s^2+8*s+2)) SScont=tf2ss (TFcont ) [Ac ,Bc ,U, ind ]=canon( SScont( 2 ) , SScont( 3 ) ) disp(Ac,"Matrix A=") disp(Bc,"Matrix B=")

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clear; clc; close; x=poly(0,'x'); p1=3/(x-2); p2=5/(x-1); // given, 3/(x-2)=5/(x-1) for x=0.0:0.1:10.0 if(3*(x-1)==5*(x-2)) format(7) x break end end

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//Finding the values of LC filter for the Buck Regulator //Example 5.5(Page No- 190) clc clear //given data Vs = 12;//V del_V = 20*10^-3;//V del_I = 0.8;//A f = 25*10^3;//Hz Va = 5;//V R = 500;//Ohm //part(a) k = Va/Vs; k_per = k*100; printf('(a)\t The duty cycle: %0.4f or %0.2f %%',k,k_per); //part(b) L = ((Va*(Vs-Va))/(f*del_I*Vs)); printf('\n (b)\t filter inductance: %.2f uH',L*10^6); //part(c) C = (del_I/(8*f*del_V)); printf('\n (c)\t The filter Capacitance: %d uF',C*10^6); //part(d) Lc = (((1-k)*R)/(2*f)); printf('\n (d)\t The Critical inductance : Lc %.2f mH',Lc*10^3); Cc = (1-k)/(16*L*f^2); printf('\n \t The critical Capacitance Cc : %.1f uF',Cc*10^6);

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clc; //page 466 //Given r=90;//mm, radius of half circle b=240;//mm, width h=120;//mm, height //Moment of inertia of rectangle Ixr=1/3*b*h^3;//mm^4 //Moment of inertia of half circle a=4*r/(3*%pi);//mm b=h-a;//mm, Distance b from centroid c to X axis I_AA=1/8*%pi*r^4;//mm^4, Moment of inertia of half circle with respect to AA' A=1/2*%pi*r^2;//mm^2, Area of half circle Ix1=I_AA-A*a^2;//mm^4, Parallel axis theorem Ixc=Ix1+A*b^2;//mm^4, Parallel axis theorem //Moment of inertia of given area Ix=Ixr-Ixc;//mm^4 printf("Moment of inertia of area about X axis is Ix= %2.2e mm^4\n",Ix);

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//chapter 2 Ex 1 clc; clear; close; n1=2^3*3^2*5*7^4; n2=2^2*3^5*5^2*7^3; n3=2^3*5^3*7^2; V=int32([n1 n2 n3]); Lcm=gcd(V); mprintf("The LCM of given numbers is %d.",Lcm);

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clc clear clf() x = [0:0.1:2*%pi]'; plot(x, [sin(x) sin(2*x) sin(3*x)]) legend('sin x','sin 2*x','sin 3*x') xlabel('x')

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${ using Typewriter.Extensions.WebApi; Template(Settings settings) { settings .IncludeProject("CMS.Web"); settings.OutputExtension = ".ts"; settings.OutputFilenameFactory = file => { return $"outputApi/{file.Name.Replace("Controller", "Api").Replace(".cs", ".ts")}"; }; } string apiName(Class c) { return c.Name.Replace("Controller", "Api"); } string ImportModels(Class c) { IEnumerable<Type> types = c.Methods .Select(p => p.Type) .Where(t => !t.IsPrimitive || t.IsEnum) .Select(t => t.IsGeneric ? t.TypeArguments.First() : t) .Where(t => t.Name != c.Name && t.Name != "DbGeography") .Distinct(); return string.Join(Environment.NewLine, types.Select(t => $"import {{ {t.Name} }} from './{t.Name}';").Distinct()); } string ImportsList(Class objClass) { var ImportsOutput = ""; // Get the methods in the Class var objMethods = objClass.Methods; // Loop through the Methdos in the Class foreach(Method objMethod in objMethods) { // Loop through each Parameter in each method foreach(Parameter objParameter in objMethod.Parameters) { // If the Paramater is not prmitive we need to add this to the Imports if(!objParameter.Type.IsPrimitive){ ImportsOutput = objParameter.Type.Name; } } } // Notice: As of now this will only return one import return $"import {{ { ImportsOutput } }} from '@/models/{ImportsOutput}';"; } string ReturnType(Method m) { if (m.Type.Name == "IHttpActionResult") { foreach (var a in m.Attributes) { // Checks to see if there is an attribute to match returnType if (a.Name == "ResponseType") { string type = string.Empty; bool isArray = a.Value.Contains("<"); bool isPaginatedResponse = a.Value.Contains("PaginatedResponse"); string formattedType = a.Value.Replace("<", "") .Replace(">", "") .Replace("typeof(", "") .Replace(")", ""); string[] ar; ar = formattedType.Split('.'); type = ar[ar.Length - 1]; if(isPaginatedResponse) { type = "PaginatedResponse<" + type + ">"; } else if (isArray) { type += "[]"; } // mismatch on bool vs boolean if (type == "bool") { type = "boolean"; } return type; } } return "void"; } return m.Type.Name; } string NullAble(Parameter p) { return p.Type.IsNullable? "?":""; } } $Classes(:BaseApiController)[ import { HTTP } from '@/HTTPServices'; import { BaseApi } from '@/apiResources/BaseApi'; import { PaginatedResponse, Pagination } from '@/apiResources/PaginatedResponse'; $ImportsList module APIs { class $apiName extends BaseApi { $Methods[ $name($Parameters[$Name$NullAble: $Type][, ]) { return new Promise<$ReturnType>((resolve: any, reject: any) => { HTTP({ url: `$Url`, method: "$HttpMethod", data: $RequestData }) .then((response) => { resolve(response.data); }).catch((error) => { reject(error); }) }); }] }] }

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/ScilabFromTheoryToPractice/GettingStarted/testpwd.sce

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2017-04-22T12:39:21

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testpwd.sce

path=pwd(); // current directory cd SCI // go to the Scilab installation directory pwd // value of current directory cd contrib // go to the SCI/contrib/ directory cd '../' // "move up" to the SCI directory chdir('contrib') // go to the SCI/contrib/ directory pwd // value of current directory chdir(TMPDIR) // go to the temporary directory mkdir('test') // create the directory test/ ls('te*') //list the elements starting with "te" rmdir('test') // remove the test/ directory dir('te*') // this is the content of the current directory which is empty [] chdir(path) // return to the initial current directory

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/biased_random.sce

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amoghpj/random_walk

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biased_random.sce

clc; clear; rand('seed',getdate('s')); X=[1]; Y=[1]; count=1; while(X(count)>0 & Y(count)>0 & X(count)<6 & Y(count)<6 & count<50000) x=X(count); y=Y(count); if(~(((x-6)^2+(y-6)^2)<=16)) then // if( (x^2+y^2)<36) then if(rand()<0.5) then X(count+1)=x+0.1; else X(count+1)=x-0.1; end; if(rand()<0.5) then Y(count+1)=y+0.1; else Y(count+1)=y-0.1; end; else if((6-x)>0) then X(count+1)=x+0.1; else X(count+1)=x-0.1 end; if((6-y)>0) then Y(count+1)=y+0.1; else Y(count+1)=y-0.1; end; if(x==6 & y==6) then break; end; // if(rand()<1) then //%%%%%%%%%%%%%%%%%%%%%%%%%%%%% // X(count+1)=x+0.1; // else // X(count+1)=x-0.1; // end; //%Biased when line 10 is modified to restr // if(rand()<1) then //%-ict unbiased random walk to a specified // Y(count+1)=y+0.1; //%region // else // Y(count+1)=y-0.1; // end; //%%%%%%%%%%%%%%%%%%%%%%%%%%%%% //// X(count+1)=x+0.1; // Y(count+1)=y+0.1; //%Biased to 45 degree line end; //%%%%%%%%%%%%%%%%%%%%%%%%%%% count=count+1; if((X(count)<=0) | (Y(count)<=0)) then X(count)=x; Y(count)=y; end; end; theta=0:%pi/50:2*%pi; xcent=6; ycent=6; r=4; xdash=xcent+r*cos(theta); ydash=ycent+r*sin(theta); figure(1); plot(xdash,ydash,'r'); i=1; //plot(a,(16-(a-6)^2)^0.5+6,'g'); //plot(a,(36-a.^2)^0.5,'g'); comet(X(:),Y(:)); plot(X(1),Y(1),"o"); h_compound = gce(); h_compound.children.mark_size = 10; h_compound.children.mark_background = 2; h_axes = gca(); h_axes.data_bounds=[0,0;10,10]; //i=100; //while i<=length(X) // plot(X(i),Y(i)); //end //// Animation Loo //Another comment i = 1; while i<=length(X) xs2bmp(0, 'i.bmp'); drawlater(); h_compound.children.data = [X(i),Y(i)]; drawnow(); i = i+1; end ///This is a new comment to test git/

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/1970/CH6/EX6.11/Ch06Exa11.sce

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// Scilab code Exa6.11: : Page-244 (2011) clc; clear; t_p = 33/0.92*365*84800; // Partial half life for beta emission, sec E_0 = 0.51; // Kinetic energy Z = 55; // Atomic number of cesium log_fb = 4.0*log10(E_0)+0.78+0.02*Z-0.005*(Z-1)*log10(E_0); // Comparitive half life log_ft1 = log_fb+log10(t_p); // Forbidden tansition // For 8 percent beta minus emission t_p = 33/0.08*365*84800; // Partial half life, sec E_0 = 1.17; // Kinetic energy Z = 55; // Atomic energy log_fb = 4.0*log10(E_0)+0.78+0.02*Z-0.005*(Z-1)*log10(E_0); // Comparitive half life log_ft2 = log_fb+log10(t_p); // Forbidden transition // Check the degree of forbiddenness !!!!! if log_ft1 <= 10 then printf("\nFor 92 percent beta emission :") printf("\n\tTransition is once forbidden and parity change"); end if log_ft2 >= 10 then printf("\nFor 8 percent beta emission :") printf("\n\t ransition is twice forbidden and no parity change"); end // Result // For 92 percent beta emission : // Transition is once forbidden and parity change // For 8 percent beta emission : // Transition is twice forbidden and no parity change

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Ex14_2.sce

//Example 14.2 M=10000;//Mass of truck (kg) g=9.80;//Acceleration due to gravity (m/s^2) h=75;//Vertical displacement (m) delta_PE=M*g*h;//Change in gravitational potential energy (J) Q=delta_PE;//Heat transferred (J) m=100;//Mass of brake material (kg) c=800;//Specific heat of brake material (J/kg.C) delta_T=Q/(m*c);//Temperature increase (C) printf('Temperature increase of brake material = %0.2f C',delta_T) //Answer varies due to round off error //Openstax - College Physics //Download for free at http://cnx.org/content/col11406/latest

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/experiments/sl-eeg-expt/presentation/Scenarios/Passive Auditory Oddball MMN - Touch.sce

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2021-06-01T17:38:51.634923

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Passive Auditory Oddball MMN - Touch.sce

# -------------------------- Header Parameters -------------------------- scenario = "MMN"; write_codes = EXPARAM( "Write Codes" ); screen_width_distance = EXPARAM( "Physical Screen Width" ); screen_height_distance = EXPARAM( "Physical Screen Height" ); screen_distance = EXPARAM( "Viewing Distance" ); default_background_color = EXPARAM( "Default Background Color" ); default_font = EXPARAM( "Default Font" ); default_font_size = EXPARAM( "Default Font Size" ); default_text_color = EXPARAM( "Default Font Color" ); active_buttons = 1; response_matching = simple_matching; stimulus_properties = event_name, string, trial_number, number, stim_number, number, stim_type, string, p_code, number, ISI_duration, number; event_code_delimiter = ";"; # ------------------------------- SDL Part ------------------------------ begin; ellipse_graphic { color = EXPARAM( "Fixation Point Color" ); ellipse_height = EXPARAM( "Fixation Point Size" ); ellipse_width = EXPARAM( "Fixation Point Size" ); } fix_ellipse; trial { #monitor_videos = false; stimulus_event { sound { wavefile { preload = false; }; }; } stim_event; } stim_trial; trial { trial_type = specific_response; terminator_button = 1; trial_duration = forever; picture{ text { caption = "rest"; preload = false; } instruct_text; x = 0; y = 0; } instruct_pic; } instruct_trial; trial { #monitor_videos = false; stimulus_event { picture {} ISI_pic; code = "ISI"; } ISI_event; } ISI_trial; trial { picture { text { caption = "Ready"; preload = false; } ready_text; x = 0; y = 0; } ready_pic; } ready_trial; # ----------------------------- PCL Program ----------------------------- begin_pcl; include_once "../../Library/lib_visual_utilities.pcl"; include_once "../../Library/lib_utilities.pcl"; # --- CONSTANTS --- # string STIM_EVENT_CODE = "Stim"; int STD_IDX = 1; int DEV_IDX = 2; int MAX_PORT_VAL = 255; string VIDEO_CODE = "Video"; string STD_COND = "Standard"; string DEV_COND = "Deviant"; string CHARACTER_WRAP = "Character"; # --- Set up fixed stimulus parameters --- string language = parameter_manager.get_string( "Language" ); language_file lang = load_language_file( scenario_directory + language + ".xml" ); bool char_wrap = ( get_lang_item( lang, "Word Wrap Mode" ).lower() == CHARACTER_WRAP.lower() ); double font_size = parameter_manager.get_double( "Default Font Size" ); # --- Stimulus setup --- if ( parameter_manager.get_bool( "Show Fixation Point" ) ) then ISI_pic.add_part( fix_ellipse, 0, 0 ); end; # Make some sounds array<sound> stim_snds[2]; stim_snds[STD_IDX] = parameter_manager.get_sound( "Standard Sound" ); stim_snds[DEV_IDX] = parameter_manager.get_sound( "Deviant Sound" ); stim_snds[STD_IDX].get_wavefile().load(); stim_snds[DEV_IDX].get_wavefile().load(); if ( parameter_manager.get_bool( "Generate Sounds" ) ) then # Initialize some values double ramp_up_time = parameter_manager.get_double( "Rise Time" ); double ramp_down_time = parameter_manager.get_double( "Fall Time" ); # Make the rise/fall ramps asg::line ramp_down = new asg::line( ramp_down_time, 1.0, 0.0 ); asg::line ramp_up = new asg::line( ramp_up_time, 0.0, 1.0 ); # Make the waveform data double std_duration = parameter_manager.get_double( "Standard Duration" ); double dev_duration = parameter_manager.get_double( "Deviant Duration" ); asg::sine std_data = new asg::sine( std_duration, parameter_manager.get_double( "Standard Frequency" ), 0.0 ); asg::sine dev_data = new asg::sine( dev_duration, parameter_manager.get_double( "Deviant Frequency" ), 0.0 ); asg::waveform_data std_wf = new asg::waveform_data( std_data ); asg::waveform_data dev_wf = new asg::waveform_data( dev_data ); # Check that the rise and fall times are legal double ramp_time = ramp_up_time + ramp_down_time; if ( ramp_time > std_duration ) || ( ramp_time > dev_duration ) then exit( "The total rise and fall time is greater than the sound duration." ); end; # Multiply by the rise/fall times std_wf.multiply_segment( ramp_up, 0.0 ); std_wf.multiply_segment( ramp_down, std_wf.duration() - ramp_down_time ); dev_wf.multiply_segment( ramp_up, 0.0 ); dev_wf.multiply_segment( ramp_down, dev_wf.duration() - ramp_down_time ); # Now make the sound objects stim_snds[STD_IDX] = new sound( new wavefile( std_wf, std_wf ) ); stim_snds[DEV_IDX] = new sound( new wavefile( dev_wf, dev_wf ) ); end; # Set the attenuation on the sounds begin double std_atten = 1.0 - ( double( parameter_manager.get_int( "Standard Volume" ) ) / 100.0 ); double dev_atten = 1.0 - ( double( parameter_manager.get_int( "Deviant Volume" ) ) / 100.0 ); stim_snds[STD_IDX].set_attenuation( std_atten ); stim_snds[DEV_IDX].set_attenuation( dev_atten ); end; # --- sub present_instructions --- sub present_instructions( string instruct_string ) begin full_size_word_wrap( instruct_string, font_size, char_wrap, instruct_text ); instruct_trial.present(); default.present(); end; # --- sub ready_set_go --- trial_refresh_fix( ready_trial, parameter_manager.get_int( "Ready Duration" ) ); array<string> ready_caps[3]; ready_caps[1] = get_lang_item( lang, "Ready Caption" ); ready_caps[2] = get_lang_item( lang, "Set Caption" ); ready_caps[3] = get_lang_item( lang, "Go Caption" ); sub ready_set_go begin loop int i = 1 until i > ready_caps.count() begin ready_text.set_caption( ready_caps[i], true ); ready_trial.present(); i = i + 1; end; end; # --- sub show_video --- /*sub show_video( array<video,1>& vids, int vid_number ) begin video_player.play( vids[vid_number], VIDEO_CODE + string( vid_number ) ); end;*/ # --- Make a trial sequence array<int> trial_sequence[0]; int min_start = parameter_manager.get_int( "Min Standards at Start" ); begin # Get some trial counts int total_trials = parameter_manager.get_int( "Total Trials" ); int std_trials = int( ceil( parameter_manager.get_double( "Standard Proportion" ) * double(total_trials) ) ); int dev_trials = total_trials - std_trials; # Figure out some of the restrictions int min_end = parameter_manager.get_int( "Min Standards at End" ); int min_between = parameter_manager.get_int( "Min Standards between Deviants" ); # Make sure there are enough trials to meet the restrictions int set_aside_stds = min_start + min_end + ( dev_trials * min_between ); int remaining_stds = std_trials - set_aside_stds; if ( remaining_stds < 0 ) then exit( "There are not enough standard trials to create a legal sequence with the current settings." ); end; # First we'll build a short sequence that ensures there are # enough targets between each distractor. For every distractor # we add "min_between" targets array<int> distractor_seq[min_between + 1]; distractor_seq.fill( 1, 0, STD_IDX, 0 ); distractor_seq[distractor_seq.count()] = DEV_IDX; # Set up a sequence of targets at the start array<int> start_seq[min_start]; start_seq.fill( 1, 0, STD_IDX, 0 ); # Set up a sequence of targets at the end array<int> end_seq[min_end]; if ( min_end > 0 ) then end_seq.fill( 1, 0, STD_IDX, 0 ); end; # Now build a temporary tgt/dist sequence. # This will get "expanded" later because for each distractor that # comes up, we'll add in "min_between" targets preceding it array<int> temp_seq[remaining_stds + dev_trials]; temp_seq.fill( 1, 0, DEV_IDX, 0 ); temp_seq.fill( 1, remaining_stds, STD_IDX, 0 ); temp_seq.shuffle(); # Now build the actual sequence. Add the initial target sequence, # then add in the temp sequence that contains the distractors, # then add in the final target sequence at the end trial_sequence.append( start_seq ); loop int i = 1 until i > temp_seq.count() begin if ( temp_seq[i] == STD_IDX ) then trial_sequence.add( STD_IDX ); else trial_sequence.append( distractor_seq ); end; i = i + 1; end; trial_sequence.append( end_seq ); end; # --- Video setup --- # Grab the videos bool show_vids = parameter_manager.get_bool( "Show Videos" ); bool preload_vids = parameter_manager.get_bool( "Preload Videos" ); /*array<video> my_vids[0]; parameter_manager.get_videos( "Video Files", my_vids );*/ /*if ( show_vids ) then # Exit if they didn't specify a video if ( my_vids.count() == 0 ) then exit( "You must specify at least one video in 'Video Files'" ); end; # Initialize some values bool use_audio = parameter_manager.get_bool( "Use Audio from Video" ); double vid_height = parameter_manager.get_double( "Video Height" ); double vid_width = parameter_manager.get_double( "Video Width" ); # Prepare the videos and set the audio if requested loop int i = 1 until i > my_vids.count() begin my_vids[i].set_use_audio( use_audio ); if ( vid_height > 0.0 ) then my_vids[i].set_height( vid_height ); end; if ( vid_width > 0.0 ) then my_vids[i].set_width( vid_width ); end; if ( preload_vids ) then my_vids[i].prepare(); end; i = i + 1; end; end;*/ # --- Main Sequence --- # string instructions = get_lang_item( lang, "Instructions" ); if ( !show_vids ) then instructions = get_lang_item( lang, "No Video Instructions" ); end; # Get the ISI array<int> ISI_range[0]; parameter_manager.get_ints( "ISI Range", ISI_range ); if ( ISI_range.count() != 2 ) then exit( "You must specify exactly two values in 'ISI Range'" ); end; # Get the port codes array<int> port_codes[2]; port_codes[STD_IDX] = parameter_manager.get_int( "Standard Port Code" ); port_codes[DEV_IDX] = parameter_manager.get_int( "Deviant Port Code" ); # Get the event codes array<string> event_codes[2]; event_codes[STD_IDX] = STD_COND; event_codes[DEV_IDX] = DEV_COND; # Prepare a video if necessary /*if ( show_vids ) then my_vids[1].prepare(); end;*/ # Show the instructions present_instructions( instructions ); ready_set_go(); # Start the video running /*if ( show_vids ) then show_video( my_vids, 1 ); else ISI_pic.present(); end;*/ # Loop to present trial sequence loop array<int> ctrs[2] = { 1,1 }; bool next_prepared = false; int vid_ctr = 1; int i = 1 until i > trial_sequence.count() begin # Check if this video is still playing, and play the # subsequent video if there is one, and increment the ctr if ( show_vids ) then /*if ( !my_vids[vid_ctr].playing() ) && ( vid_ctr < my_vids.count() ) then vid_ctr = vid_ctr + 1; show_video( my_vids, vid_ctr ); next_prepared = false; end;*/ end; # Check whether std or deviant int this_stim = trial_sequence[i]; # Set the ISI trial_refresh_fix( ISI_trial, random( ISI_range[1], ISI_range[2] ) ); # Set the ISI duration and the stimulus stim_event.set_stimulus( stim_snds[this_stim] ); # Set the port code; we add a special prefix for the first stimulus presentation int p_code = port_codes[this_stim]; if ( i <= min_start ) then p_code = p_code + 100; end; stim_event.set_port_code( p_code ); # Set the event code stim_event.set_event_code( STIM_EVENT_CODE + ";" + string( i ) + ";" + string( ctrs[this_stim] ) + ";" + event_codes[this_stim] + ";" + string( p_code ) + ";" + string( ISI_trial.duration() ) ); # Present the trial stim_trial.present(); # Use some ISI time to prepare the next video if necessary /*if ( show_vids ) then if ( !next_prepared ) && ( !preload_vids ) then int start = clock.time(); if ( vid_ctr < my_vids.count() ) then my_vids[vid_ctr + 1].prepare(); end; next_prepared = true; int ttime = clock.time() - start; if ( ttime < ISI_trial.duration() ) then ISI_trial.set_duration( ISI_trial.duration() - ttime ); else ISI_trial.set_duration( ISI_trial.STIMULI_LENGTH ); end; end; end;*/ # Show the ISI ISI_trial.present(); ctrs[this_stim] = ctrs[this_stim] + 1; i = i + 1; end; present_instructions( get_lang_item( lang, "Completion Screen Caption" ) );

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clc clear //Input data tw3=30;//The inlet temperature of water in degree centigrade wc=1.15;//Mass flow rate of cooling water in kg per kg air tdb1=20;//The dry bulb temperature of air in degree centigrade R1=60;//Relative humidity of air while entering in percentage tdb2=28;//The dry bulb temperature while leaving in degree centigrade R2=90;//Relative humidity of air while leaving in percentage tm=20;//The temperature of makeup water in degree centigrade Cpc=4.187;//The specific heat of water in kJ/kgK G=1;//Mass flow rate of dry air in kg/s //Calculations twb1=15.2;// from psychrometric chart The wet bulb temperature while entering in degree centigrade twb2=26.7;// from psychrometric chart The wet bulb temperature while leaving in degree centigrade h1=43;//The enthalpy from chart for dry air in kJ/kg dry air h2=83.5;//The enthalpy from chart in kJ/kg dry air W1=0.0088;//Humidity in kg water vapour/kg dry air W2=0.0213;//Humidity in kg water vapour/kg dry air hw3=125.8;//Enthalpy of water entering the tower in kJ/kg hw=84;//Enthalpy of makeup water in kJ/kg hwc=[(G/wc)*[(h2-h1)-(W2-W1)*hw]];//The change in enthalpy of water in kJ/kg tw4=tw3-(hwc/Cpc);//The exit temperature of water in degree centigrade ta=tw4-twb1;//The approach temperature in degree centigrade tr=tw3-tw4;//The range temperature in degree centigrade x=G*(W2-W1);//Fraction of water evaporated in kg/kg dry air //Output printf(' (a) The temperature of water leaving the tower = %3.1f degree centigrade \n (b) The fraction of water evaporated = %3.4f kg/kg dry air \n (c) The approach of the cooling tower = %3.1f degree centigrade \n The Range of the cooling tower = %3.1f degree centigrade ',tw4,x,ta,tr)

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MatrixAdd.sce

clc m=input("Enter number of rows:") n=input("Enter number of columns:") a=zeros(m,n) b=zeros(m,n) c=zeros(m,n) disp("Enter the elements of matrix A:"); for i=1:m for j=1:n a(i,j)=input(""); end; end; disp("Enter the elements of matrix B:"); for i=1:m for j=1:n b(i,j)=input(""); end; end; for i=1:m for j=1:n c(i,j)=a(i,j)+b(i,j); end; end; disp("Matrix A:"); disp(a); disp("Matrix B:"); disp(b); disp("Addition Matrix C:"); disp(c);

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/3293/CH3/EX3.16/Ex3_16.sce

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Ex3_16.sce

//page 92 //Example 3.16 clc; clear; close; disp('T is a linear operator on R^2 defined as T(x1,x2) = (x1,0)'); disp('So, the matrix T in standard ordered basis B = {e1,e2} is '); T = [1 0 ;0 0]; disp(T,'[T]B = '); disp('Let B'' is the ordered basis for R^2 consisting of vectors:'); E1 = [1 1]; E2 = [2 1]; disp(E1,'E1 = '); disp(E2,'E2 = '); P = [E1;E2]' disp(P,'So, matrix P = '); Pinv = inv(P); disp(Pinv,'P inverse = '); T1 = Pinv*T*P; disp(T1,'So, matrix T in ordered basis B'' is [T]B'' = '); //end

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/881/CH10/EX10.1/exa10_1.sce

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exa10_1.sce

clc; //Example 10.1 //Page No 395 //Solution i=10*10^-4; dt=10*10^-9; dv=10; disp("The expression for the current through a capacitor is "); disp("i = C dv/dt"); disp("Rearranging and solving for c yields, "); c=i*dt/dv; disp('F',c,"C = "); disp("t = RC","The charge time constant for C when Q1 in on is "); disp("Therefore, rearranging the above equation and substituting the value of chaging time yields"); C=dt/(4.6*20); disp('F',C/100,"C = ");

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Ex15_3.sce

//Example 15.3 //Hodography //Page No. 517 clc;clear;close; alpha=60; //in degrees mu=1/sind(alpha); p_2k=mu*5/2; printf('Pressure = %g',p_2k);

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/964/CH5/EX5.6/5_6.sce

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5_6.sce

clc; clear; function y=f(x) y=x^10 - 1; endfunction x1=0; x2=1.3; xt=1; //using bisection method disp("BISECTION METHOD:") xr=(x1+x2)/2; et=abs(xr-xt)/xt*100;//error disp(1,"Iteration:") disp(x1,"xl:") disp(x2,"xu:") disp(xr,"xr:") disp(et,"et(%):") disp("----------------------------------------") for i=2:5 if f(x1)*f(xr)>0 then x1=xr; xr=(x1+x2)/2; ea=abs(xr-x1)/xr*100; et=abs(xr-xt)/xt*100; else if f(x1)*f(xr)<0 then x2=xr; xr=(x1+x2)/2; ea=abs(xr-x2)/xr*100; et=abs(xr-xt)/xt*100; end end if f(x1)*f(xr)==0 then break; end disp(i,"Iteration:") disp(x1,"xl:") disp(x2,"xu:") disp(xr,"xr:") disp(et,"et(%):") disp(ea,"ea(%)") disp("----------------------------------------") end //using false position method disp("FALSE POSITION METHOD:") x1=0; x2=1.3; xt=1; xr=x1-(f(x1)*(x2-x1))/(f(x2)-f(x1));; et=abs(xr-xt)/xt*100;//error disp(1,"Iteration:") disp(x1,"xl:") disp(x2,"xu:") disp(xr,"xr:") disp(et,"et(%):") disp("----------------------------------------") for i=2:5 if f(x1)*f(xr)>0 then x1=xr; xr=x1-(f(x1)*(x2-x1))/(f(x2)-f(x1)); ea=abs(xr-x1)/xr*100; et=abs(xr-xt)/xt*100; else if f(x1)*f(xr)<0 then x2=xr; xr=x1-(f(x1)*(x2-x1))/(f(x2)-f(x1)); ea=abs(xr-x2)/xr*100; et=abs(xr-xt)/xt*100; end end if f(x1)*f(xr)==0 then break; end disp(i,"Iteration:") disp(x1,"xl:") disp(x2,"xu:") disp(xr,"xr:") disp(et,"et(%):") disp(ea,"ea(%)") disp("----------------------------------------") end

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Ex5_17.sce

clc //initialization of new variables clear D=0.5 //m H=0.5 //m d=1 //m g=9.8 //m/s^2 //calculations Cd=0.399+0.0598*H/D Q=Cd*d/2*sqrt(2*g)*H^(3/2) //results printf('Flow rate is Q = %.3f m^3/s',Q)

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/2789/CH9/EX9.12/Ex9_12.sce

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Ex9_12.sce

clear; clc; //page no. 312 d = 12;// in D = 24;//in theta = 20;//degrees G = 10;//cfs p = 20;//psi V12 = G/(0.25*%pi); V24 = V12/4; K_L = 0.43; p24 = ((p*144/62.4) + (V12^2 /(2*32.2)) - ((V24^2)/(2*32.2)) - K_L*(V12-V24)^2 /(2*32.2))/2.314; printf('Pressure in the larger pipe = %.1f psi',p24);

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qei_sim.sce

function y = qei_sim(u1) in = u1; out = u1; if in > %pi then out = modulo(in-%pi, 2*%pi) - %pi; end if in < -%pi then out = modulo(in+%pi, 2*%pi) + %pi; end y = out*1/%pi; endfunction

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/Replication 2/Dave_RIFData/Dave_RIFData/Sub18/VP18_OneBack.sce

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rettopnivek/Wimber_et_al_replication_3

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VP18_OneBack.sce

array <int> finalSeq[432] = {68,68,9,9,36,36,31,33,52,23,13,43,65,13,50,28,28,42,72,5,51,64,64,48,63,72,63,63,15,15,42,38,31,10,6,66,43,17,6,55,35,29,37,66,49,7,50,50,56,56,14,52,61,4,9,67,4,5,34,70,55,55,64,47,32,32,26,43,46,46,55,55,4,4,19,26,4,12,29,34,34,54,27,26,21,12,60,37,56,21,10,58,58,15,70,54,24,42,42,50,20,20,40,71,39,31,31,67,59,59,43,43,68,49,45,21,67,8,45,68,14,2,1,1,29,22,70,70,32,32,18,25,32,44,71,60,60,46,66,35,35,57,57,47,69,69,13,33,54,16,6,28,28,70,37,58,12,14,33,30,33,9,19,18,72,25,38,40,39,7,7,24,24,53,25,25,53,58,66,23,16,11,11,49,58,35,1,1,29,29,63,30,58,32,12,48,42,2,36,52,66,66,43,65,60,60,36,17,47,60,38,20,20,11,11,71,28,19,25,59,62,56,62,26,26,34,26,34,34,24,45,39,2,41,22,6,41,42,49,27,30,30,27,27,12,7,5,37,5,38,5,45,7,47,23,51,51,3,33,31,61,13,65,14,49,49,59,12,10,10,54,40,8,69,8,8,48,46,17,4,23,72,46,65,21,21,41,51,3,50,38,6,19,19,27,57,57,18,14,57,35,23,47,53,59,61,17,29,2,40,48,64,13,39,24,2,53,28,67,8,40,71,71,63,64,27,54,3,30,13,11,16,62,22,22,52,53,10,37,45,67,39,52,51,68,20,39,31,47,53,30,19,21,44,2,36,18,68,3,38,61,22,10,67,7,62,44,48,65,65,9,18,71,54,69,35,44,59,51,62,55,62,40,24,18,15,15,61,25,6,23,64,48,14,46,5,41,41,22,36,17,17,57,61,3,72,72,37,15,45,56,16,16,33,8,63,16,41,69,69,50,9,44,56,52,11,20,3,70,44,1,1}; array <int> buttons[432] = {0,1,2,1,2,1,2,2,2,2,2,2,2,2,2,2,1,2,2,2,2,2,1,2,2,2,2,1,2,1,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,1,2,1,2,2,2,2,2,2,2,2,2,2,2,1,2,2,2,1,2,2,2,1,2,1,2,1,2,2,2,2,2,2,1,2,2,2,2,2,2,2,2,2,2,2,1,2,2,2,2,2,1,2,2,1,2,2,2,2,1,2,2,1,2,1,2,2,2,2,2,2,2,2,2,2,2,1,2,2,2,1,2,1,2,2,2,2,2,2,1,2,2,2,1,2,1,2,2,1,2,2,2,2,2,2,1,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,1,2,1,2,2,1,2,2,2,2,2,2,1,2,2,2,2,1,2,1,2,2,2,2,2,2,2,2,2,2,2,1,2,2,2,1,2,2,2,2,2,2,1,2,1,2,2,2,2,2,2,2,2,2,1,2,2,2,1,2,2,2,2,2,2,2,2,2,2,2,2,1,2,1,2,2,2,2,2,2,2,2,2,2,2,2,1,2,2,2,2,2,2,2,2,1,2,2,2,1,2,2,2,2,2,1,2,2,2,2,2,2,2,2,2,1,2,2,2,2,2,2,2,1,2,2,1,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,1,2,2,2,2,2,2,2,2,2,2,2,1,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,1,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,2,1,2,2,2,2,2,2,2,2,2,2,1,2,2,2,1,2,2,2,2,1,2,2,2,2,2,1,2,2,2,2,2,2,1,2,2,2,2,2,2,2,2,2,2,0,0}; array <int> nullEvents[145] = {4,5,8,13,14,17,23,25,34,35,36,40,49,50,54,55,75,79,80,81,85,86,90,95,102,104,106,112,118,125,126,127,132,134,140,142,147,148,150,151,153,154,160,167,168,173,179,192,194,195,205,212,215,222,224,226,228,230,235,236,242,247,248,251,257,259,262,268,270,272,277,279,297,300,304,305,310,320,322,325,326,330,335,336,342,344,353,354,364,367,368,369,370,371,377,381,394,396,401,404,406,408,409,414,415,417,429,430,434,435,439,440,443,448,454,457,459,464,470,472,481,482,500,501,502,506,512,516,519,522,526,527,529,530,532,541,542,543,555,557,560,567,574,575,577}; array <int> selPic[36] = {1,5,9,13,17,21,25,29,33,37,41,45,49,53,57,61,65,69,4,8,12,16,20,24,28,32,36,40,44,48,52,56,60,64,68,72};

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/944/CH6/EX6.14/example6_14_TACC.sce

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example6_14_TACC.sce

//example 6.14 clear; clc; //Given: m1=0.01;//molality[m] v11=1; v12=2; Y1=0.71; m2=0.005;//molality[m] v21=1; v22=1; Y2=0.53; //To find the activity , molality of the electrolytes v1=(v11)+(v12); v2=(v21)+(v22); a1=(m1^v1)*(v11^v11)*(v12^v12)*(Y1^v1); a2=(m2^v2)*(v21^v21)*(v22^v22)*(Y2^v2); x=1/v1; a1m=a1^x; m1m=m1*(v11^v11*v12^v12)^x;//molality[m] y=1/v2; m2m=m2*(v21*v21*v22^v22)^y;//molality[m] a2m=a2^y; disp(a1,'The activity of the electrolyte ZnCl2 is'); disp(a1m,'The mean activity of ZnCl2 is '); disp(m1m,'The mean molality of ZnCl2 in [m] '); disp(a2,'The activity of the electrolyte CuSO4 is '); disp(a2m,'The mean activity of CuSO4 is '); disp(m2m,'The mean molality of CuSO4 in [m] ');

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/181/CH3/EX3.12/example3_12.sce

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example3_12.sce

// Determine maximum and average values of power // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 3-12 in page 159 clear; clc; close; // Given data V1=230; // Input voltage in V N=1/3; // Turn ratio Rl=200; // Load resistance in ohms // Calculation V2=V1*N; Vm=sqrt(2)*V2; Im=Vm/Rl; P=Im^2*Rl; Vdc=0.318*Vm; Idc=Vdc/Rl; Pdc=Idc^2*Rl; printf("Maximum load power = %0.2f W\n",P); printf("Average load power = %0.2f W",Pdc); // Result // Maximum power = 58.78 W // Average power = 5.94 W

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MS_4.sce

errcatch(-1,"stop");mode(2);// sum 3-4 ; ; P=40*10^3; A=60*18; sig=P/A; r1=12; b1=60; SCF1=1.7; sigmax1=sig*SCF1; r2=24; b2=60; SCF2=1.5; sigmax2=sig*SCF2; // printing data in scilab o/p window printf("sigmax1 is %f N/mm^2 ",sigmax1); printf("\n sigmax2 is %f N/mm^2 ",sigmax2); exit();

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example4_4.sce

// Calculate beta for the BJT // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 4-4 in page 209 clear; clc; close; // Given Data Ib=20*10^-6; // Base current in micro-A Ic=5*10^-3; // Collector Current in mA // Calculations beta_bjt=Ic/Ib; printf("The Current gain beta for the Device is %0.0f \n",beta_bjt); // Results // The Current Gain beta for the Device is 250

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ex4_25.sce

// Exa 4.25 clc; clear; close; // Given data V_CC = 16;// in V V_BE = 0.7;// in V R_B = 470;// in kohm R_B= R_B*10^3;// in ohm bita = 120; R_C = 3.6;// in kohm R_C= R_C*10^3;// in ohm R_E = 0.51;// in kohm R_E= R_E*10^3;// in ohm I_B = (V_CC - V_BE)/(R_B+bita*(R_C+R_E));// in A disp(I_B*10^6,"The base current in µA is"); I_C = bita*I_B;// in A disp(I_C*10^3,"The collector current in mA is"); V_C = V_CC - I_C*R_C;// in V disp(V_C,"The collector voltage in V is");

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/3574/CH10/EX10.1/EX10_1.sce

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FOSSEE/Scilab-TBC-Uploads

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EX10_1.sce

// Example 10.1 // Computation of (a) Induced emf (b) Frequency of the rectangular voltage // wave in the armature winding // Page No. 394 clc; clear; close; // Given data E1=136.8; // Generated emf P=6; // Number of poles n=1180; // Operating speed of machine // (a) Induced emf E2=E1*0.75*2; // (b) Frequency of the rectangular voltage wave in the armature winding f=P*n*0.75/120; //Display result on command window printf("\n Induced emf = %0.1f V ",E2); printf("\n Frequency of the rectangular voltage wave = %0.2f Hz ",f);

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/1952/CH12/EX12.3/Ex3.sce

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FOSSEE/Scilab-TBC-Uploads

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Ex3.sce

// Additional solved examples , Example 3 , pg 331 T=260+273 //temperature(in kelvin) (converting celsius into kelvin) h=6.625*10^-34//plancks constant(in Js) c=3*10^8//speed of light(in m/s) lam=590*10^-9//wavelength(in m) k=1.38*10^-23//boltzman constant (in (m^2*Kg)/(s^2*k)) N=1/(exp((h*c)/(lam*k*T))-1) //N=((n21)'/(n21)) ratio of stimulated emission to spontaneous emission printf("Ratio of stimulated emission to spontaneous emission is") disp(N)

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/1991/CH2/EX2.14/14.sce

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FOSSEE/Scilab-TBC-Uploads

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14.sce

clc clear //input m1=1//mass of object 1 v1=25//velocity of object 1 m2=2//mass of object 2 v2=0//body at rest,velocity =0 v3=10 //caclulation u=((m1*v1)+(m2*v2)-(m2*v3))/2//applying princilpe of conservation of linear momentum //output printf("\n the value of u is %3.3f ms^-1",-u)

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/src/menu.sci

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samverneck/RealTimeMonitor

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refs/heads/master

2020-12-02T18:09:27.752225

2017-06-21T19:52:00

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sci

menu.sci

mAcq=uimenu(f,'label', 'Acquisition'); mSetup=uimenu(f,'label', "Setup"); mExport=uimenu(f,'label', "Export Data", "callback", "exportValues"); // mAcq1=uimenu(mAcq,'label', "Start", "callback", "launchSensor"); mAcq2=uimenu(mAcq,'label', "Stop", "callback", "stopSensor"); mAcq3=uimenu(mAcq,'label', "Reset", "callback", "resetDisplay"); // mSensor1=uimenu(mSetup,'label', "Sensor 1"); mSensor2=uimenu(mSetup,'label', "Sensor 2"); mStability=uimenu(mSetup,'label', "Stability"); // mBuffer1=uimenu(mSensor1,'label', "Time Buffer", "callback", "changeBuffer(1)"); mMinTemp1=uimenu(mSensor1,'label', "Min Temp Display", "callback", "setupMinTemp(1)"); mMaxTemp1=uimenu(mSensor1,'label', "Max Temp Display", "callback", "setupMaxTemp(1)"); // mBuffer2=uimenu(mSensor2,'label', "Time Buffer", "callback", "changeBuffer(2)"); mMinTemp2=uimenu(mSensor2,'label', "Min Temp Display", "callback", "setupMinTemp(2)"); mMaxTemp2=uimenu(mSensor2,'label', "Max Temp Display", "callback", "setupMaxTemp(2)"); // mStabilityValue=uimenu(mStability,'label', "Stability value", "callback", "setupStability(1)"); mStabilityTime=uimenu(mStability,'label', "Stability time", "callback", "setupStability(2)"); // function changeBuffer(id) newBuffer=evstr(x_dialog('Set new time buffer value (seconds): ','300')) // if newBuffer == [] then return elseif id == 1 then global timeBuffer timeBuffer = newBuffer; a = findobj("tag", "sensor1Axes"); e = findobj("tag", "sensor1NewAxes"); // a.data_bounds = [0, minTempDisplay; timeBuffer, maxTempDisplay]; e.data_bounds = [0, minRegulationDisplay; timeBuffer, maxRegulationDisplay]; elseif id == 2 then global timeBuffer2 timeBuffer2 = newBuffer; a = findobj("tag", "sensor2Axes"); e = findobj("tag", "sensor2NewAxes"); // a.data_bounds = [0, minTempDisplay2; timeBuffer2, maxTempDisplay2]; e.data_bounds = [0, minRegulationDisplay2; timeBuffer2, maxRegulationDisplay2]; end endfunction // function setupMinTemp(id) newMinTemp=evstr(x_dialog('Set new min temperature value: ','15')) // if newMinTemp == [] then return elseif id == 1 then global minTempDisplay global minRegulationDisplay minTempDisplay = newMinTemp; minRegulationDisplay = minTempDisplay + 273.15; a = findobj("tag", "sensor1Axes"); e = findobj("tag", "sensor1NewAxes"); l = findobj("tag", "liveAxes"); minS = findobj("tag", "minTempSlider"); maxS = findobj("tag", "maxTempSlider"); // a.data_bounds = [0, minTempDisplay; timeBuffer, maxTempDisplay]; e.data_bounds = [0, minRegulationDisplay; timeBuffer, maxRegulationDisplay]; l.data_bounds = [0, minTempDisplay; 1, maxTempDisplay]; minS.min = minTempDisplay; maxS.min = minTempDisplay; elseif id == 2 then global minTempDisplay2 global minRegulationDisplay2 minTempDisplay2 = newMinTemp; minRegulationDisplay2 = minTempDisplay2 + 273.15; a = findobj("tag", "sensor2Axes"); e = findobj("tag", "sensor2NewAxes"); l = findobj("tag", "liveAxes2"); minS = findobj("tag", "minTempSlider2"); maxS = findobj("tag", "maxTempSlider2"); // a.data_bounds = [0, minTempDisplay2; timeBuffer2, maxTempDisplay2]; e.data_bounds = [0, minRegulationDisplay2; timeBuffer2, maxRegulationDisplay2]; l.data_bounds = [0, minTempDisplay2; 1, maxTempDisplay2]; minS.min = minTempDisplay2; maxS.min = minTempDisplay2; end endfunction // function setupMaxTemp(id) newMaxTemp=evstr(x_dialog('Set new max temperature value: ','50')) // if newMaxTemp == [] then return elseif id == 1 then global maxTempDisplay global maxRegulationDisplay maxTempDisplay = newMaxTemp; maxRegulationDisplay = maxTempDisplay + 273.15; a = findobj("tag", "sensor1Axes"); e = findobj("tag", "sensor1NewAxes"); l = findobj("tag", "liveAxes"); minS = findobj("tag", "minTempSlider"); maxS = findobj("tag", "maxTempSlider"); // a.data_bounds = [0, minTempDisplay; timeBuffer, maxTempDisplay]; e.data_bounds = [0, minRegulationDisplay; timeBuffer, maxRegulationDisplay]; l.data_bounds = [0, minTempDisplay; 1, maxTempDisplay]; minS.max = maxTempDisplay; maxS.max = maxTempDisplay; elseif id == 2 then global maxTempDisplay2 global maxRegulationDisplay maxTempDisplay2 = newMaxTemp; maxRegulationDisplay2 = maxTempDisplay2 + 273.15; a = findobj("tag", "sensor2Axes"); e = findobj("tag", "sensor2NewAxes"); l = findobj("tag", "liveAxes2"); minS = findobj("tag", "minTempSlider2"); maxS = findobj("tag", "maxTempSlider2"); // a.data_bounds = [0, minTempDisplay2; timeBuffer2, maxTempDisplay2]; e.data_bounds = [0, minRegulationDisplay2; timeBuffer2, maxRegulationDisplay2]; l.data_bounds = [0, minTempDisplay2; 1, maxTempDisplay2]; minS.max = maxTempDisplay2; maxS.max = maxTempDisplay2; end endfunction // function setupStability(opt) if opt == 1 then newStability=evstr(x_dialog('Set new stability value: ','0.3')) // if newStability == [] then return else global %stability_value %stability_value = newStability; end elseif opt == 2 then newStability=evstr(x_dialog('Set new stability time value (seconds): ','30')) // if newStability == [] then return else global %stability_time global %warning // %warning = [%t, %t]; %stability_time = newStability; end end endfunction

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/k1.sce

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KomalT/tryout60

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2016-08-12T19:05:56.548794

2016-05-02T06:15:37

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k1.sce

P1s = 0.43596 P2s = 0.23738 x=[0:0.1:1]; P=P2s+((P1s-P2s)*x); y=x*P1s ./P ; plot(x,P,'b') Amar=0.5196743 gama1=exp(Amar*(1-x)^2); gama2=exp(Amar*x^2); Pmar=(P1s*gama1.*x)+(P2s*gama2.*(1-x)); ymar=(P1s*gama1.*x)./Pmar; plot(x,Pmar,'g') xexp=[.0819 .2192 .3584 .3831 .5256 .8478 .9872] gmaexp1=[1.4187 1.3598 1.2773 1.2615 1.1714 1.021 1.00] gmaexp2=[1.006 1.043 1.1052 1.1184 1.2033 1.3925 1.4342] Pexp=(P1s*gmaexp1.*xexp)+(P2s*gmaexp2.*(1-xexp)); ymar=(P1s*gmaexp1.*xexp)./Pexp; plot(xexp,Pexp,'+') title("P Vs x","x","P"); legend("Prl","Pmar")

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/3137/CH12/EX12.20/Ex12_20.sce

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FOSSEE/Scilab-TBC-Uploads

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Ex12_20.sce

//Initilization of variables theta=45 //degrees l=0.5 //m w=10 //rad/s //Calculations //PART a //Here the theta derivative with respect to time is angular speed w Vp1=l*(secd(theta)^2)*w //m/s //Part b //Radial Component r=l*secd(theta)*tand(theta)*w //m/s //Transverse Component t=l*secd(theta)*w //m/s //Total Vp2=sqrt(r^2+t^2) //m/s //Result clc printf('The velocity is:%fm/s\n',Vp1) printf('The velocity in part b is %fm/s',Vp2)

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/842/CH7/EX7.2/Example7_2.sce

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FOSSEE/Scilab-TBC-Uploads

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Example7_2.sce

//clear// //Example7.2:Digital Differentiator syms t n; T = 0.1; //Sampling time in seconds xct = sin(%pi*t/T)/(%pi*t); yct = diff(xct,t); disp(yct,'yc(t)='); t = n*T; xdn = sin(%pi*t/T)/(%pi*t); ydn = diff(xdn,n); disp(ydn,'yd[n]='); hdn = T*ydn; disp(hdn,'hd[n]='); //Result //yc(t) = (10*cos(31.415927*t)/t)-(0.3183099*sin(31.415927*t)/(t^2)) //yd[n]=(10*cos(3.1415927*n)/n)-3.183*sin(3.1415927*n)/(n^2) //hd[n]=(cos(3.1415927*n)/n)-0.3183*sin(3.1415927*n)/(n^2)

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/Snehdeep-queuesystem.sce

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arpits2/PP

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2022-07-06T07:14:46.223798

2020-05-10T13:47:40

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Snehdeep-queuesystem.sce

AR=10/24 SR=6 Po=1/(1+(AR/SR)+((AR/SR)^2)*(SR/((2*SR)-AR))) Pb=(1/2)*((AR/SR)^2)*(2*SR/((2*SR)-AR))*Po Lq=(AR*SR*((AR/SR)^2)*Po)/(((2*SR)-AR)^2) L=Lq+(AR/SR) Wq=(SR*((AR/SR)^2)*Po)/(((2*SR)-AR)^2) W=Wq+(1/SR) printf("\nProbability that system is empty=") disp(Po) printf("Probability that both server are busy-") disp(Pb) printf("avg. number in queue=") disp(Lq) printf("avg. number in system=") disp(L) printf("avg. time in queue=") disp(Wq) printf("avg. time in system=") disp(W)

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/858/CH3/EX3.24/example_24.sce

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FOSSEE/Scilab-TBC-Uploads

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2018-02-03T05:31:52

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example_24.sce

clc clear printf("example 3.24 page number 112\n\n") //to find volumetric composition of flue glass wt_H2 = 0.15; wt_C = 0.85; O2_H2 = wt_H2*(16/2); O2_C = wt_C*(32/12); total_O2 = O2_H2+O2_C; wt_air = total_O2/0.23; air_supplied = 1.15*(wt_air); N2_supplied = 0.77*air_supplied/28; O2_supplied = 0.23*(air_supplied-wt_air)/32; moles_CO2 = 0.85/12; printf("moles of CO2 = %f kmol\n\n",moles_CO2) printf("moles of N2 = %f kmol \n\n",N2_supplied) printf("moles of O2 = %f kmol\n\n",O2_supplied) total_moles = N2_supplied+O2_supplied+moles_CO2; printf("percentage of CO2 = %f\n\n",(moles_CO2/total_moles)*100) printf("percentage of N2 = %f\n\n",(N2_supplied/total_moles)*100) printf("percentage of O2 = %f",(O2_supplied/total_moles)*100)

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/1673/CH2/EX2.9/2_9.sce

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FOSSEE/Scilab-TBC-Uploads

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2020-04-09T02:43:26.499817

2018-02-03T05:31:52

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2_9.sce

//example 2.9 //false position method //page 30 clc;clear;close deff('y=f(x)','y=4*exp(-x)*sin(x)-1'); a=0,b=0.5;//f(0) is negative and f(0.5)is positive d=0.00001; printf('succesive iterations \ta\t b\t f(a)\t f(b)\t\ x1\n'); for i=1:25 x1=b*f(a)/(f(a)-f(b))+a*f(b)/(f(b)-f(a)); if(f(a)*f(x1))>0 b=x1; else a=x1; end if abs(f(x1))<d break end printf(' \t%f %f %f %f %f\n',a,b,f(a),f(b),x1); end printf('the root of the equation is %f',x1);

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/317/CH5/EX5.10/example10.sce

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FOSSEE/Scilab-TBC-Uploads

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example10.sce

// find maximum allowable series resistance // Electronic Principles // By Albert Malvino , David Bates // Seventh Edition // The McGraw-Hill Companies // Example 5-10, page 157 clear;clc; close; // Given data Rlmin=140;// minimum load resistance in ohms Vsmin=22;// minimum input voltage in volts Vz=12;// zener voltage in volts // Calculations Rsmax=((Vsmin/Vz)-1)*Rlmin;// maximum series resistance in ohms disp("ohms",Rsmax,"Series resistance=") // Result // maximum series resistance is 117 ohms