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031016f3b382759796634a1d1a188dbc178974c6
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PSOGRAPH.sce
[x]=read("~/Innopolis/Introduction_To_AI/week6/res1.txt",2000,1) x = [x] [y]=read("~/Innopolis/Introduction_To_AI/week6/res2.txt",2000,1) y = [y] for n=0:5:2000 for k=1:5 if k==1 then plot(x(n+k),y(n+k),".r"); elseif k==2 then plot(x(n+k),y(n+k),".g"); elseif k==3 then plot(x(n+k),y(n+k),".o"); elseif k==4 then plot(x(n+k),y(n+k),".b"); elseif k==5 then plot(x(n+k),y(n+k),".y"); end, end sleep(0.01) end
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2020-04-09T02:43:26.499817
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7_8w.sce
//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 7.8w //calculation of the angular speed of rotation //given data L=20*10^-2//length(in m) of the rod = length(in m)of the string theta=30//angle(in degree) made by the string with the vertical g=10//gravitational acceleration(in m/s^2) of the earth //calculation //applying Newton's second law //T*sind(theta) = m*w*w*L*(1+sind(theta)).............(1) //applying Newton's first law in vertical direction //T*cosd(theta) = m*g.................................(2) //from above equations,we get //tand(theta)=((w*w*L*(1+sind(theta)))/g).............(3) w=sqrt((g*tand(theta))/(L*(1+sind(theta)))) printf('the angular speed of rotation is %3.1f rad/s',w)
c3b1fce2065675fc5cd63ae3c56cd6aa477f237d
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/2741/CH6/EX6.1/Chapter6_Example1.sce
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Chapter6_Example1.sce
clc clear //Input data H=80;//The Heat flows into the system in joules W=30;//The Work done by the system in joules //Calculations U=H-W;//The internal energy of the system in joules W1=10;//The work done along the path ADB in joules H1=W1+U;//The heat flows into the system along the path ADB in joules W2=-20;//The work done on the system from B to A in joules H2=W2-U;//The heat liberated from B to A in joules Ua=0;//Internal energy at A in joules Ud=40;//Internal energy at D in joules Wa=10;//Work done from A to D in joules Wd=0;//Work done from D to B in joules Uc=50;//Internal energy at C in joules Had=(Ud-Ua)+Wa;//Heat absorbed in the process AD in joules Hdb=Uc-Ud+Wd;//Heat absorbed in the process DB in joules //Output printf('(a)Heat flows into the system along the path ADB is H = %3.0f joules \n (b)The heat liberated by the system is H = %3.0f joules \n (c)The heat absorbed in the process AD is H = %3.0f joules and \n The heat absorbed in the process DB is H = %3.0f joules ',H1,H2,Had,Hdb)
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mandar15/NLP_Project
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bow.12_6.tst
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Ex2_6.sce
//Ex 2.6 page 70 clc; clear; close; VS=3;// kV IS=750;// A VD=800;// V ID=175;// A dr=30/100;// de-rating factor IB=8;//mA delQ=30;// u Coulomb // dr = 1-IS/np*ID np = round(IS/(1-dr)/(ID)) ; // no. of parallel string ns = round(VS*1000/(1-dr)/(VD)) ; // no. of series string R=(ns*VD-VS*1000)/(ns-1)/(IB/1000)/1000;//kohm C=(ns-1)*delQ*10**-6/(ns*VD-VS*1000) printf('Value of R = %.2f kohm',R) printf('\n Value of C = %.2e F',C)
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/360 krunker strafes .sce
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Ahmad6543/Scenarios
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360 krunker strafes .sce
Name=360 krunker strafes PlayerCharacters=Character Profile BotCharacters=Quaker Bot.bot;Quaker Bot.bot;Quaker Bot.bot;Quaker Bot.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Character Profile AddedBots=Quaker Bot.bot;Quaker Bot.bot PlayerMaxLives=0 BotMaxLives=0;0 PlayerTeam=1 BotTeams=0;0 MapName=flat_field_mini.map MapScale=5.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=100000.0 ScorePerDamage=0.0 ScorePerKill=1.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag= WeaponHeroTag=LG DifficultyTag=4 AuthorsTag=Igglez BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Close tracking training on a slide-hopping target (modified from close krunker strafes) GameVersion=2.0.2.0 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 LockFOVRange=false LockedFOVMin=60.0 LockedFOVMax=120.0 LockedFOVScale=Clamped Horizontal [Aim Profile] Name=At Feet MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Aim Profile] Name=Low Skill MinReactionTime=0.35 MaxReactionTime=0.45 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=20.0 TrackSpeed=3.0 TrackError=5.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=25.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 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=Quaker Bot DodgeProfileNames=Long Strafes Jumping;Long Strafes Jumping;Long Strafes Jumping;Long Strafes Jumping DodgeProfileWeights=2.0;3.0;1.0;2.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;0.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=At Feet;At Feet;Low Skill;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=Quaker 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=Character Profile MaxHealth=100.0 WeaponProfileNames=LG;;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=0.1 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=1000.0 MaxCrouchSpeed=500.0 Acceleration=16000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=0.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.1 AllowBufferedJumps=false 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=0.25 ThirdPersonCamera=false TPSArmLength=500.0 TPSOffset=X=0.000 Y=125.000 Z=40.000 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=Quaker MaxHealth=275.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.001 MaxRespawnDelay=0.001 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=2600.0 MaxCrouchSpeed=500.0 Acceleration=100000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=1150.0 Gravity=3.0 AirControl=0.0 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=280.0 MainBBRadius=70.0 MainBBHasHead=true MainBBHeadRadius=70.0 MainBBHeadOffset=-30.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=70.0 ProjBBHasHead=true ProjBBHeadRadius=300.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.25 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=700.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=true 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 [Dodge Profile] Name=Long Strafes Jumping MaxTargetDistance=3000.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.5 MaxLRTimeChange=3.0 MinFBTimeChange=0.5 MaxFBTimeChange=1.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.5 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.1 MaxJumpTime=0.1 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 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 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Weapon Profile] Name=LG Type=Hitscan ShotsPerClick=1 DamagePerShot=6.0 KnockbackFactor=2.0 TimeBetweenShots=0.046 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=7.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.05 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 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=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=720.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=false AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices -128.000000 256.000000 640.000000 640.000000 256.000000 640.000000 640.000000 256.000000 -128.000000 -128.000000 256.000000 -128.000000 -128.000000 240.000000 640.000000 640.000000 240.000000 640.000000 640.000000 240.000000 -128.000000 -128.000000 240.000000 -128.000000 faces 0.000000 0.000000 1.000000 1.000000 0.000000 0 1 2 3 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 6 5 4 7 0x00000000 0.000000 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clc // Variable Initialization Vm=240//Supply Voltage in Volts Ra=0.9//Combined Field and Armature circuit resistance in Ohm N=900 //Motor speed in Rpm V=220//Rated voltage of motor in Volts a=45//firing angle in Degree Kaf=0.035 //Constant in N-m/A^2 //Solution //For semi-converter controlled Dc Drive Va=(Vm*1.414)*(1+cosd(a))*(1/%pi)//Average voltage in Volts W=(2*%pi*N)/60 //angular speed in Rad/sec Ia=Va/(Ra+W*Kaf)//Current in Amp T=Kaf*(Ia)^2//Torque in N-m //Results printf('\n\n The motor Current =%0.1f Amp \n\n',Ia) printf('\n\n The motor Torque =%0.1f N-m \n\n',T)
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// Exa 6.4 clc; clear; close; // Given Data f= 1;// in kHz f= f*10^3;// in Hz // Vout/Vin= 10 R1= 100;// in k ohm R1=R1*10^3;// in ohm R2= 1000;// in k ohm R2=R2*10^3;// in ohm omega= 2*%pi*f; // Vout/Vin at a 3 dB frequency of 1 kHz = 1/sqrt(2) = omega*R2*C/sqrt(1+omega^2*R1^2*C2) C= sqrt(1/(omega^2*(2*R2^2-R1^2)));// in F disp(R1*10^-3,"Value of R1 in k ohm"); disp(R2*10^-6,"Value of R2 in k ohm"); disp(C,"Value of C in k ohm");
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//Example 2.6.2 page 2.34 clc; clear; t= 0.1*10^-6; L= 10; B_opt= 1/(2*t); B_opt=B_opt/1000000; //converting from Hz to MHz printf("The maximum optical bandwidth is %d MHz.",B_opt); del= t/L; del=del/10^-6; //converting in us... printf("\n\nThe dispersion per unit length is %.2f us/Km",del); BLP= B_opt*L; printf("\n\nThe Bandwidth-Length product is %d MHz.Km",BLP);
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//xdel(winsid()); //Amelioration de contraste clown = double((imread("images/CLOWN_LUMI2.BMP"))); //figure;ShowImage(clown/255, "Clown original"); //Valeurs minimales et maximales de l'image a=min(clown(:)); b=max(clown(:)); //Etalage de l'histogramme CE = ((clown-a)*255)/(b-a); figure; ShowImage(CE/255, "Clown contrasté"); //Histogramme de l'image //figure; histplot(255,clown, normalization = %f); figure; histplot(255,CE, normalization = %f);
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clc //initialisation of variables p= 1 //atm p1= 3 //atm R= 1.987 //cal/mole K T= 27 //C b= 0.0428 //l mole^-1 a= 3.61 //l^2 atm mole^-1 //CALCULATIONS G= R*(273+T)*log(p/p1) A= R*(273+T)*log(p/p1) G1= R*(273+T)*log(p/p1)+(b-(a/(0.08205*(T+273))))*(p-p1)*(R/0.08205) //RESULTS printf (' Gibs free energy= %.f cal',G) printf (' \n Value of A= %.f cal',A) printf (' \n Gibs free energy= %.f cal',G1) printf (' \n Value of A= %.f cal',A)
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//Part B Chapter 4 Example 9 clc; clear; close; d=120;//mm D1=120;//mm D2=60;//mm ThBYTs=(D1^4-D2^4)/d^4; WhBYWs=%pi/4*((D1^2-D2^2)/(%pi/4)/d^2); disp("Strength ratio, Th/Ts is "+string(ThBYTs)); disp("Weight ratio, Wh/Ws is "+string(WhBYWs));
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clc clear //input data Q1=20//Discharge of air to the centrifugal compressor in m^3/s V1=Q1//Volume of rate is equal to the discharge in m^3/s P1=1//Initial pressure of the air to the centrifugal compressor in bar T1=288//Initial temperature of the air to the centrifugal compressor in K P=1.5//The pressure ratio of compression in centrifugal compressor C1=60//The velocity of flow of air at inlet in m/s Cr2=C1//The radial velocity of flow of air at outlet in m/s Dh=0.6//The inlet impeller diameter in m Dt=1.2//The outlet impeller diameter in m N=5000//The speed of rotation of centrifugal compressor in rpm n=1.5//polytropic index constant in the given law PV^n Cp=1005//The specific heat of air at constant pressure in J/kg.K //calculations U1=(3.14*Dh*N)/60//Peripheral velocity of impeller at inlet in m/s b11=atand(C1/U1)//The blade angle at impeller inlet in degree U2=(3.14*Dt*N)/60//Peripheral velocity of impeller top at outlet in m/s T2=T1*(P)^((n-1)/n)//Final temperature of the air to the centrifugal compressor in K Cx2=((Cp*(T2-T1))/U2)//The whirl component of absolute velocity in m/s Wx2=U2-Cx2//The exit relative velocity in m/s a2=atand(Cr2/Cx2)//The blade angle at inlet to casing in degree b22=atand(Cr2/Wx2)//The blade angle at impeller outlet in degree b1=Q1/(2*3.14*(Dh/2)*C1)//The breadth of impeller blade at inlet in m V2=(P1*V1*T2)/(T1*P*P1)//Volume flow rate of air at exit in m^3/s Q2=V2//Volume flow rate is equal to discharge in m^3/s b2=Q2/(2*3.14*(Dt/2)*Cr2)//The breadth of impeller blade at outlet in m //output printf('(a)The blade and flow angles\n (1)The blade angle at impeller inlet is %3.1f degree\n (2)The blade angle at inlet to casing is %3.1f degree\n (3)The blade angle at impeller outlet is %3.2f degree\n(b)Breadth of the impeller blade at inlet and outlet\n (1)The breadth of impeller blade at inlet is %3.3f m\n (2)The Volume flow rate of air at exit is %3.2f m^3/s\n (3)The breadth of impeller blade at outlet is %3.4f m',b11,a2,b22,b1,V2,b2) //comments //error in the first review is not printing the value of V2 which is corrected
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clc;funcprot(0);//Example 8.11 //Initilisation of Variables Tci=20;......//Inlet temparature of oil in degrees celcius Tco=90;......//Outlet temparature of oil in degrees celcius Cpc=2;....//Specific heat of oil in kJ/kgK Thi=140;......//Inlet temparature of steam in degrees celcius Tho=115;......//Outlet temparature of steam in degrees celcius mh=5;....//Mass flow rate of steam in kg/s U=300;..........//Overall heat transfer coefficient in W/m^2K Cph=2;....//Specific heat of steam in kJ/kgK Cpc=2;....//Specific heat of air in kJ/kgK L=2.5;.....//Lemgth of the tube in m Di=0.05;....//Diameter of tube in m //calculations LMTDc=((Thi-Tco)-(Tho-Tci))/log((Thi-Tco)/(Tho-Tci));......//Log mean temparature diffrence of steam in counter flow arrangement in K R2=(Thi-Tho)/(Tco-Tci);....//Resistanfce from counter flow R1=(Tco-Tci)/(Thi-Tci);....//Resistanfce from counter flow F0=0.97;......//From the graph F and R1,R2 Q=mh*Cph*(Thi-Tho);....//Heat transfer water in W A=(Q*1000)/(LMTDc*U*F0);......//Area of heat exchanger in counter flow in m^2 mc=Q/(Cpc*(Tco-Tci));.....//Mass flow rate of oil in kg/s mch=mc/2;........//Mass flow rate of oil is reduced to half Ch=mh*Cph;....//Heat capacity of air by counter flow kW/K Cc=mch*Cpc;....//Heat capacity of water by counter flow kW/K R=Cc/Ch;.....//Resistance NTU=(U*A)/(Cc*1000);....//Number of transfer units E=(1/R)*{1-exp(-R*(1-exp(-NTU)))};.....//Effectiveness Tcoa=Tci+((E*Cc*(Thi-Tci))/Cc);.....// Thoa=Thi-((E*Cc*(Thi-Tci))/Ch);.....// Qact=Cc*(Tcoa-Tci);.....//Actual heat transfer in kW n=A/(%pi*Di*L);.....//Number of tubes Qred=((Q-Qact)-1)*100/Q;.....//Heat transfer rate if the flow rate of oil is reduced to half disp(A,"Surface area of heat exchanger in m^2:") disp(n,"number of tubes of oil flow:") disp(Qred,"Heat transfer rate if the flow rate of oil is reduced to half:")
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//ques-5.32 //Calculating pH of different salt solutions clc Kw=10^-14; //(i)0.02M NH4Cl Kb=1.8*10^-5; c=0.02; p1=(-log10(Kw)+log10(Kb)-log10(c))/2; printf("pH of Ammonium chloride solution is %.2f.\n",p1); //(ii)0.01M CH3COONa Ka=Kb; c=0.01; p2=(-log10(Kw)-log10(Ka)+log10(c))/2; printf(" pH of Sodium acetate solution is %.2f.\n",p2); //(iii)CH3COONH4 p3=(-log10(Kw)-log10(Ka)+log10(Kb))/2; printf(" pH of Ammonium acetate solution is %.1f.",p3);
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//Change in air fuel ratio at altitude clc,clear //Given: ha=5000 //Altitude in m A_F=14 //Air fuel ratio at sea level P1=1.013 //Pressure of air in bar at sea level T1=27+273 //Temperature of air in K at sea level R=0.287 //Specific gas constant in kJ/kgK function t=f1(h),t=ts-0.0065*h,endfunction //Temperature(t in degreeC) as a function of altitude(h in m) function h=f2(P),h=19200*log10(1.013/P),endfunction //Altitude(h in m) as a function of pressure(P in bar) //Solution: ts=T1-273 //Sea level temperature in degreeC T2=f1(ha) //Temperature at altitude(ha = 5000 m) in degreeC T2=T2+273 //in K //Defining, y as a function of P //This function is the difference of function(f2) and ha given function y=f(P),y=f2(P)-ha,endfunction //The function f is solve for zero to get the value of P2 P2=fsolve(1,f) //Pressure at altitude(ha = 5000 m) in bar rho_a=P2/(R*T2) //Density of air at altitude in kg/m^3 rho_s=P1/(R*T1) //Density of air at sea level in kg/m^3 A_F_a=A_F*sqrt(rho_a/rho_s) //Air fuel ratio at altitude //Results: printf("\n The air fuel ratio supplied at 5000 m altitude by a carburettor = %.2f\n\n",A_F_a)
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//Example 1_7 page no:74 clc; //given power = 75;//in kW rpm = 500; energy = 5400; fl_load_torque = (power * 1000 * 60)/(2 * %pi * rpm); str_torque = 2145; acc_torque = 715; stored_energy = energy * power; omega = rpm *(2*%pi/60); I = (2 * stored_energy)/(omega^2); alpha = acc_torque / I; t = omega / alpha; disp(t,"the time taken to start the motor if the load torque is equal to full load torque is (in s)"); //the result vary slightly hence values are rounded off in text book
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clc;clear; //Example 10.7 //given data T0=290; Tsource=1600; Tsink=T0; //from Ex 10.1 qin=2728.6; qout=2018.6; h4=2403; //from steam tables s1=1.2132; s3=6.7450; //calculations s2=s1;s4=s3;//isentropic processes xdest12=0; xdest34=0; xdest23=T0*(s3-s2-(qin/Tsource)); xdest41=T0*(s1-s4+(qout/Tsink)); disp(xdest12,'exergy destruction in 1-2 in kJ/kg'); disp(round(xdest23),'exergy destruction in 2-3 in kJ/kg'); disp(xdest34,'exergy destruction in 3-4 in kJ/kg'); disp(round(xdest41),'exergy destruction in 4-1 in kJ/kg'); xdestcy=xdest12+xdest23+xdest34+xdest41; disp(round(xdestcy),'exergy destruction in cycle in kJ/kg'); //from steam tables //at 290 K and 100 kPa h0=71.355; s0=0.2533; X4=(h4-h0)-T0*(s4-s0); disp(round(X4),'exergy of the leaving steam in kJ/kg')
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clc clear //Page number 486 //Input data t2=7;//The low temperature of reservoir in degree centigrade n1=50;//The efficiency of the carnots engine in percentage n2=70;//The increased efficiency of the carnots engine in percentage //Calculations T2=t2+273;//The low temperature of the reservoir in K T1=T2/(1-(n1/100));//The temperature of the source reservoir in K T11=T2/(1-(n2/100));//The temperature to be maintained by the source reservoir in K T=T11-T1;//The increase in temperature of the source in K or degree centigrade //Output printf('The increase in temperature of the source is %3.1f K (or) %3.1f degree centigrade ',T,T)
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//scilab 5.4.1 clear; clc; printf("\t\t\tProblem Number 10.6\n\n\n"); // Chapter 10 : Refrigeration // Problem 10.6 (page no. 509) // Solution //From Appendix 3,at 120psia,the corresponding saturation temperature is 66 F, enthalpies are h1=116.0; //Unit:Btu/lbm //enthalpy h2=116.0; //Unit:Btu/lbm //Throttling gives h1=h2 //enthalpy h3=602.4; //Unit:Btu/lbm //enthalpy //From the consideration that s3=s4,h4 is found at 15 psia, s3=1.3938; //s=entropy //Unit:Btu/(lbm*F) //Therefore by interpolation in the superheat tables at 120 psia, t4=237.4; //Unit:fahrenheit //temperature h4=733.4; //Unit:Btu/lbm //enthalpy printf("Solution for (a),\n"); COP=(h3-h1)/(h4-h3); //Coefficient of performance printf("Coefficient of performance is %f\n\n",COP); printf("Solution for (b),\n"); printf("The work of compression is %f Btu/lbm\n\n",h4-h3); printf("Solution for (c),\n"); printf("The refrigatering effect is %f Btu/lbm\n\n",h3-h1); printf("Solution for (d),\n"); tons=30; //capacity of 30 tons is desired printf("The pounds per minute of ammonia required for ciculation is %f lbm/min\n\n",(200*tons)/(h3-h1)); printf("Solution for (e),\n"); printf("The ideal horsepower per ton of refrigeration is %f hp/ton\n\n",4.717*((h4-h3)/(h3-h1)));
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clc // Variable Initialization Vm=230//Supply Voltage in Volts Ra=0.5//Armature circuit resistance in Ohm Irms=25 //Armature current in Amp Nr=800 //Motor speed in Rpm Kaf=0.172 //Motor Voltage Constant in V/rpm a=60//firing angle in Degree //Solution //CASE:A //For motoring action Ka=(Kaf*60)/(2*%pi)//Constant in V-s/rad T=Ka*Irms //Torque of motor in N-m Va=(2*Vm*1.414)*cosd(a)*(1/%pi)//Average voltage in Volts Eb=Va-(Irms*Ra)//Back Emf in Volts N=Eb/Kaf//Speed of motor in Rpm //The supply current is square wave if motor current is constant and ripple-free with Amplitude 25A P=Vm*Irms //Supply VA in Watt //Power from supply is real power if losses in converter are neglected Ps=Va*Irms //Power in Watt pf=Ps/P //Power factor lag //CASE:B //For polarity reversal (regeneration action) Eb1=-Eb //Back emf in Volts Va1=Eb1+(Irms*Ra) af=acosd((Va1*%pi)/(2*Vm*1.414))//Firing angle in Degree //Power fed from DC Machine Pdc=Eb*Irms //Power in watt //Power lost in armature resistance PL=((Irms)^2)*Ra //Power in Watt //Power fed back to ac supply is PF=Pdc-PL //Power in watt //Results printf('\n\n The motor Torque=%0.1f N-m \n\n',T) printf('\n\n The motor Speed =%0.1f RPM \n\n',N) printf('\n\n The Supply Power Factor=%0.1f Lag\n\n',pf) printf('\n\n The Firing Angle=%0.1f Degree\n\n',af) printf('\n\n The Power fed back to Supply=%0.1f Watt\n\n',PF) //The answers vary due to round off error
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//Given that Vi = 12 //in L Ti = 20+273 //in K Pi = 15 //in atm Tf = 35+273 //in K Vf = 8.5 //in L R = .0821 //in atm.lit/(mol.K) //Sample Problem 20-1 printf("**Sample Problem 20-1**\n") Pf = (Pi*Vi/(R*Ti))/(Vf/(R*Tf)) printf("The final pressure of the gas is %fatm", Pf)
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// Copyright (C) 2015 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Author: Shreyash Sharma // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in function new_image = sobel(image, ddepth, dx, dy, ksize, scale, delta) // This function is used to calculate the first, second, third, or mixed image derivatives using an extended Sobel operator. // // Calling Sequence // B = sobel(A,ddepth,dx,dy,ksize,scale,delta) // // Parameters // A: image matrix of the source image. // ddepth : output image depth; the following combinations of src.depth() and ddepth are supported such as ,src.depth() = CV_8U, ddepth = -1/CV_16S/CV_32F/CV_64F,src.depth() = CV_16U/CV_16S, ddepth = -1/CV_32F/CV_64F,src.depth() = CV_32F, ddepth = -1/CV_32F/CV_64F,src.depth() = CV_64F, ddepth = -1/CV_64F,when ddepth=-1, the destination image will have the same depth as the source; in the case of 8-bit input images it will result in truncated derivatives. // dx: order of the derivative x. // dy: order of the derivative y. // ksize: size of the extended Sobel kernel; it must be 1, 3, 5, or 7. // scale: optional scale factor for the computed derivative values; by default, no scaling is applied (see getDerivKernels() for details). // delta: optional delta value that is added to the results prior to storing them in dst. // B : output image with it's histogram matching similar to a given reference image. // // Description // This function is used to calculate the first, second, third, or mixed image derivatives using an extended Sobel operator.In all cases except one, the ksize X ksize separable kernel is used to calculate the derivative. When ksize = 1 , the 3 X 1 or 1 X 3 kernel is used (that is, no Gaussian smoothing is done). ksize = 1 can only be used for the first or the second x- or y- derivatives. // // Examples // i = imread('lena.jpeg',0); // ii = sobel(i,"CV_8U",1,0,3,1,0); // image_list = mattolist(image) out = raw_sobel(image_list, ddepth, dx, dy, ksize, scale, delta) sz = size(out) for i=1:sz new_image(:, :, i) = out(i) end endfunction
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//CHAPTER 7- SINGLE PHASE TRANSFORMER //Example 1 clc; disp("CHAPTER 7"); disp("EXAMPLE 1"); //VARIABLE INITIALIZATION I_0=10; //no load current in Amperes pf=0.25; //power factor v1=400; //in Volts f=50; //in Hertz //SOLUTION //solution (a) //magnetizing component //Iphi=I0.sin theta theta=acos(pf); //taking value of theta from the given power factor I_phi=I_0*sin(theta); disp(sprintf("(a) The magnetizing component of no load current is %.2f A",I_phi)); //solution (b) //iron loss //Pc=V1.Ic //Ic=I0.cos theta & also Ic=I0.pf as pf=cos theta p_c=v1*I_0*pf; disp(sprintf("(b) The iron loss is %d W",p_c)); //solution (c) N1=500; // number of turns in primary given phi_m=v1/(sqrt(2)*%pi*f*N1); disp(sprintf("(c) The maximum value of flux in the core is %.2f mWb",phi_m*1000)); //END
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//Example 17_13 clc(); clear; //To find the values of e, R and I i1=2 //Units in A i2=0.5 //Units in A i=i1+i2 //Units in A v1=6 //Units in V v2=16 //Units in V r=-(v1-v2)/0.5 //Units in Ohms v3=25 //Units in V e=v2+v3 //Units in V printf("The current I=%.1f A\n Resistance is R=%d Ohms\n The value E is=%d V",i,r,e)
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Quote from Chapter 27 of book "Etudes for Programmer" by Charles Wetherell: Easy is a general-purpose, procedural, algebraic programming language. Its roots lie in ALGOL, ALGOL 68, and PASCAL. Like them, it is designed to be compiled, loaded, and executed reasonably conventional computer. The syntax is described by a context-free grammar suitable for parsing by LR(1) techniques. The semantics are similar to the languages described above, and we will let an informal description suffice, trusting to the reader’s skill to fill any gaps. In the text below, logically connected portions of the grammar are described with the associated semantics.
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function [arena,colormask] = kiks_kad2arena(a) // Ouput variables initialisation (not found in input variables) arena=[]; colormask=[]; // Display mode mode(0); // Display warning for floating point exception ieee(1); a = double(mtlb_double(a)); arena = []; colormask = []; xs = double(a(1)); ys = double(a(2)); // ! L.9: real(ys) may be replaced by: // ! --> ys if ys is Real // ! L.9: real(xs) may be replaced by: // ! --> xs if xs is Real colormask = zeros(real(ys),real(xs)); i = 3; while i<max(size(a)) no_vert = a(i); i = i+1; x = a(i:i+no_vert-1); i = i+no_vert; y = a(i:i+no_vert-1); i = i+no_vert; col = a(i); i = i+1; // ! L.20: real(mtlb_a(mtlb_s(mtlb_max(y,"m"),mtlb_min(y,"m")),1)) may be replaced by: // ! --> mtlb_a(mtlb_s(mtlb_max(y,"m"),mtlb_min(y,"m")),1) if mtlb_a(mtlb_s(mtlb_max(y,"m"),mtlb_min(y,"m")),1) is Real // ! L.20: real(mtlb_a(mtlb_s(mtlb_max(x,"m"),mtlb_min(x,"m")),1)) may be replaced by: // ! --> mtlb_a(mtlb_s(mtlb_max(x,"m"),mtlb_min(x,"m")),1) if mtlb_a(mtlb_s(mtlb_max(x,"m"),mtlb_min(x,"m")),1) is Real mask = zeros(real(mtlb_a(mtlb_s(mtlb_max(y,"m"),mtlb_min(y,"m")),1)),real(mtlb_a(mtlb_s(mtlb_max(x,"m"),mtlb_min(x,"m")),1))); [yix,xix] = mtlb_find(bool2s(mtlb_logic(mask,"==",0))); // !! L.22: Matlab function inpolygon not yet converted, original calling sequence used in = inpolygon(xix,yix,mtlb_a(mtlb_s(x,mtlb_min(x,"m")),1),mtlb_a(mtlb_s(y,mtlb_min(y,"m")),1)); mask(mtlb_e(yix,mtlb_find(bool2s(mtlb_logic(mtlb_double(in),">",0)))),mtlb_e(xix,mtlb_find(bool2s(mtlb_logic(mtlb_double(in),">",0))))) = 1; colormask(mtlb_imp(mtlb_min(y,"m"),mtlb_max(y,"m")),mtlb_imp(mtlb_min(x,"m"),mtlb_max(x,"m"))) = mask*col; // colormask(min(y):max(y),min(x):max(x))=mask*round(rand*100); % visible polygons // !! L.26: Unknown function kiks_progress not converted, original calling sequence used kiks_progress(i/max(size(a)),"rendering arena "); end; arena = mtlb_logic(colormask,">",0); endfunction
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//Example 1_28 clc; clear; close; format('v',5); //given data : V1=15;//V V2=4;//V R1=4;//ohm R2=3;//ohm R3=2;//ohm R4=5;//ohm I1=6;//A RL=R4;//ohm //solution Req=R1*R3/(R1+R3)+R2;//ohm //Converting current source into Voltage source V2=I1*R3;//V//Converted source //writing KVL equation for the loop I=poly(0,'I'); eqn=V1-R1*I-R3*I-V2;//KVL equation I=roots(eqn);//A //Potential at point A with respect to B VAB=V2+R3*I;//V //Thevenin equivalent current I=VAB/(Req+RL);//A disp(I,"Current through 5 ohm resistor(A)");
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clc; r=0.05; // in m eo=8.85*10^-12; //constant q=10^-9; //charge at point P in Coulomb E=q/(4*(%pi)*eo*(r^2)); //calculating electric field disp(E,"Electric field in v/m = "); //displaying result r1=0.2; //in m V1=q/(4*(%pi)*eo*r1); //calculating potential difference disp(V1," Potential difference between two points in Volt = "); //displaying result
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clc e = 20 // M,A.R.R. i = e // interest rste i = i/100 n = 5 // life in years s = 32000 // annual net savings in Rs p = 100000 // present worth in Rs S = 20000 // salvage value in Rs a = (p-S)*(i/((1+i)^n-1)) // (p-s)(A/F,e%,n) E = (s-a)/p // E.R.R.R printf("\n ERRR = %0.2f percent", E*100) disp("Since E.R.R.R is > M.A.R.R. therefore project is feasible.")
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// Exa 4.1 clc; clear; close; format('v',6) // Given data R = 10;// inohm V = 230;// in V f = 50;// in Hz I = V/R;// in A disp(I,"The currrent in A is"); P =V*I;// in W disp(P,"The power consumed in W is"); Vm = sqrt(2)*V;// in V Im =sqrt(2)*I;// in A omega = 2*%pi*f;// in rad/sec //Equation for voltage: V = Vm*sind(omega*t) //Equation for current: i = Im*sind(omega*t) disp("Voltage equation : v = "+string(Vm)+" sin ("+string(round(omega))+" t)") disp("Current equation : i = "+string(Im)+" sin ("+string(round(omega))+" t)")
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THE OPTIMIZATION ALGORITHM HAS CHANGED TO THE EM ALGORITHM. ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 0.490667D+00 2 -0.708501D-02 0.404499D-02 3 -0.499371D-01 0.198661D-02 0.334941D+00 4 0.292955D-02 -0.496624D-03 -0.297639D-02 0.277259D-02 5 -0.165301D-02 0.112886D-03 -0.902879D-03 0.509411D-04 0.254581D-02 6 -0.672752D-03 0.336797D-04 -0.180342D-03 0.140863D-03 0.199302D-03 7 -0.896201D-03 0.778276D-04 0.371819D-03 -0.315654D-04 -0.140137D-03 8 0.309209D-03 -0.292445D-03 0.442362D-03 0.466486D-05 0.771840D-05 9 -0.248684D+00 -0.483390D-02 0.744037D+00 -0.425778D-01 0.105136D+00 10 0.950082D-01 0.387402D-02 0.201517D-01 0.203721D-01 0.135696D+00 11 -0.206091D+00 0.238290D-01 -0.993971D-01 -0.109079D-01 -0.175734D-02 12 0.481043D+00 0.131026D-01 -0.129232D+01 0.528079D-01 0.174154D-01 13 -0.526541D-01 0.138504D-01 -0.285813D-01 0.105925D-01 0.184512D-03 14 0.640779D-01 -0.128395D-01 -0.344387D+00 0.105853D-01 0.160141D-02 15 0.668614D+00 0.442350D-02 0.261847D+00 0.296171D-01 -0.205832D+00 16 0.420211D-01 0.634540D-02 0.393806D-02 0.146921D-02 -0.301349D-02 17 0.591004D-02 0.109746D-02 -0.121967D-02 -0.139502D-03 0.291203D-03 18 0.987311D-01 -0.409831D-01 0.175266D+00 -0.410226D-01 -0.602753D-02 19 -0.266492D+00 0.100848D-01 -0.100183D+00 0.265729D-02 -0.302495D-02 20 -0.543822D-01 -0.559075D-01 -0.334693D+01 -0.207544D-01 -0.970999D-02 21 0.252554D+00 -0.355517D-02 0.788106D-01 -0.235106D-02 -0.140774D-02 22 0.362173D-02 -0.128869D-05 0.151803D-02 0.406912D-03 -0.955306D-05 23 -0.760342D-02 0.466331D-03 -0.146343D-01 -0.129163D-01 -0.126875D-02 24 0.122410D-02 0.649503D-03 0.407577D-02 -0.476107D-03 0.159221D-03 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.121887D-02 7 0.801370D-03 0.252725D-02 8 0.248366D-03 0.157120D-03 0.269473D-02 9 -0.108088D-01 -0.525185D-01 0.477371D-01 0.154192D+03 10 0.518313D-02 -0.147398D-01 -0.114091D-01 0.756643D+01 0.307827D+02 11 0.503251D-01 0.854210D-01 -0.141676D-01 -0.180840D+02 -0.160844D+01 12 -0.497804D-02 -0.362603D-01 -0.511567D-01 0.592415D+01 0.355577D+01 13 0.709115D-01 0.119299D+00 0.819390D-03 -0.402116D+01 -0.278636D+01 14 0.192100D-02 -0.439163D-02 0.252357D+00 0.102886D+02 0.209900D+01 15 0.467678D-01 0.154142D-01 -0.250378D-02 -0.267124D+02 -0.285923D+02 16 0.143190D-03 -0.294960D-02 -0.178444D-02 0.226449D+01 -0.512651D+00 17 -0.368052D-03 0.275026D-03 -0.412501D-03 -0.372122D+00 0.627676D-01 18 -0.489647D-01 -0.728219D-01 0.816597D-01 0.102019D+02 0.185768D+01 19 -0.108635D-02 0.285255D-01 0.118436D-01 -0.151792D+01 0.907413D+00 20 0.340495D-01 0.398126D-01 -0.149963D+00 0.439363D+01 0.180884D+01 21 -0.141735D-03 -0.286230D-01 -0.141379D-01 0.932406D+00 -0.121357D+01 22 -0.224151D-03 -0.357802D-03 -0.414159D-03 -0.982090D-02 -0.169373D-02 23 -0.191208D-02 -0.364518D-05 0.173956D-02 0.301727D+00 0.165474D-01 24 -0.114622D-03 -0.279978D-03 -0.334487D-03 -0.681132D-01 -0.182968D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.548196D+02 12 -0.128170D+02 0.893347D+02 13 -0.166181D+01 0.133564D+00 0.176352D+02 14 -0.641495D+01 -0.373880D+01 -0.829446D+00 0.560618D+02 15 0.837939D+01 -0.503623D+01 0.428891D+01 -0.426567D+01 0.575771D+03 16 -0.193287D+00 0.760164D+00 -0.766339D-01 -0.107538D+00 0.506974D+01 17 0.378977D-02 -0.112850D-01 -0.102977D-02 -0.272564D-01 -0.284459D+01 18 -0.319161D+01 -0.756367D+01 -0.513338D+01 0.137638D+02 -0.421188D+02 19 0.158645D+00 -0.235593D+00 0.115355D+01 0.133560D+01 -0.499080D+00 20 0.986796D+01 -0.188355D+01 0.410220D+01 -0.201968D+02 0.195381D+02 21 0.836778D+00 0.766910D-01 -0.120492D+01 -0.158413D+01 0.254177D+01 22 -0.841346D-01 0.515262D-02 -0.363416D-01 -0.602747D-01 -0.505767D-02 23 -0.257079D+00 -0.540686D+00 -0.112495D+00 0.367980D+00 -0.506335D+00 24 0.163524D-02 -0.943238D-01 -0.345249D-01 -0.922300D-01 -0.851731D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.801204D+00 17 -0.693044D-01 0.299766D-01 18 0.924522D+00 -0.144695D-01 0.255918D+03 19 -0.118440D+00 0.703046D-02 0.223841D+01 0.637804D+01 20 0.119797D+00 -0.894278D-01 -0.675729D+02 0.399508D+01 0.397363D+03 21 0.154181D-01 -0.407103D-02 0.600862D+00 -0.571209D+01 -0.378338D+01 22 0.722926D-03 0.631624D-03 -0.122871D+01 -0.299010D-01 0.295726D+00 23 0.382682D-01 0.474515D-02 0.254120D+00 0.439644D-01 0.326684D+01 24 -0.499790D-03 0.174216D-02 0.290786D+00 -0.398451D-01 -0.195131D+01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.675360D+01 22 -0.240194D-01 0.146377D-01 23 -0.216545D+00 0.136468D-01 0.546392D+00 24 0.702586D-01 -0.282900D-02 -0.314794D-01 0.215288D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.159 1.000 3 -0.123 0.054 1.000 4 0.079 -0.148 -0.098 1.000 5 -0.047 0.035 -0.031 0.019 1.000 6 -0.028 0.015 -0.009 0.077 0.113 7 -0.025 0.024 0.013 -0.012 -0.055 8 0.009 -0.089 0.015 0.002 0.003 9 -0.029 -0.006 0.104 -0.065 0.168 10 0.024 0.011 0.006 0.070 0.485 11 -0.040 0.051 -0.023 -0.028 -0.005 12 0.073 0.022 -0.236 0.106 0.037 13 -0.018 0.052 -0.012 0.048 0.001 14 0.012 -0.027 -0.079 0.027 0.004 15 0.040 0.003 0.019 0.023 -0.170 16 0.067 0.111 0.008 0.031 -0.067 17 0.049 0.100 -0.012 -0.015 0.033 18 0.009 -0.040 0.019 -0.049 -0.007 19 -0.151 0.063 -0.069 0.020 -0.024 20 -0.004 -0.044 -0.290 -0.020 -0.010 21 0.139 -0.022 0.052 -0.017 -0.011 22 0.043 0.000 0.022 0.064 -0.002 23 -0.015 0.010 -0.034 -0.332 -0.034 24 0.012 0.070 0.048 -0.062 0.022 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.457 1.000 8 0.137 0.060 1.000 9 -0.025 -0.084 0.074 1.000 10 0.027 -0.053 -0.040 0.110 1.000 11 0.195 0.229 -0.037 -0.197 -0.039 12 -0.015 -0.076 -0.104 0.050 0.068 13 0.484 0.565 0.004 -0.077 -0.120 14 0.007 -0.012 0.649 0.111 0.051 15 0.056 0.013 -0.002 -0.090 -0.215 16 0.005 -0.066 -0.038 0.204 -0.103 17 -0.061 0.032 -0.046 -0.173 0.065 18 -0.088 -0.091 0.098 0.051 0.021 19 -0.012 0.225 0.090 -0.048 0.065 20 0.049 0.040 -0.145 0.018 0.016 21 -0.002 -0.219 -0.105 0.029 -0.084 22 -0.053 -0.059 -0.066 -0.007 -0.003 23 -0.074 0.000 0.045 0.033 0.004 24 -0.022 -0.038 -0.044 -0.037 -0.022 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 -0.183 1.000 13 -0.053 0.003 1.000 14 -0.116 -0.053 -0.026 1.000 15 0.047 -0.022 0.043 -0.024 1.000 16 -0.029 0.090 -0.020 -0.016 0.236 17 0.003 -0.007 -0.001 -0.021 -0.685 18 -0.027 -0.050 -0.076 0.115 -0.110 19 0.008 -0.010 0.109 0.071 -0.008 20 0.067 -0.010 0.049 -0.135 0.041 21 0.043 0.003 -0.110 -0.081 0.041 22 -0.094 0.005 -0.072 -0.067 -0.002 23 -0.047 -0.077 -0.036 0.066 -0.029 24 0.002 -0.068 -0.056 -0.084 -0.024 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.447 1.000 18 0.065 -0.005 1.000 19 -0.052 0.016 0.055 1.000 20 0.007 -0.026 -0.212 0.079 1.000 21 0.007 -0.009 0.014 -0.870 -0.073 22 0.007 0.030 -0.635 -0.098 0.123 23 0.058 0.037 0.021 0.024 0.222 24 -0.004 0.069 0.124 -0.108 -0.667 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.076 1.000 23 -0.113 0.153 1.000 24 0.184 -0.159 -0.290 1.000
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R = 10 * 10^3; C1 = 10 * 10^-9; C2 = 470 * 10^-9; s = %s; wo = 1 / (R * sqrt(C1 * C2)); to = 1 / wo; m = (3 / 2) * sqrt(C1 / C2); num = 1; dem = 1 + 2 * m * s * to + (s * to)^2; sys = syslin('c', num/dem); t = (0:to/100:20*to)'; y = csim('step', t, sys); tmp = find(y>=0.95); tr5 = t(tmp(1)); figure(1); plot2d(t, y'); figure(2); bode(sys, 10, 10^4); bode_asymp(sys);
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# orig Pythagoras.Y01 +(1+2*x)^2 # flat Pythagoras.Y01 2*x + 1 # merg Pythagoras.Y01 2*x_y_z + 1 # orig Pythagoras.Y01 +(2*x+2*x^2)^2 # flat Pythagoras.Y01 2*x + 2*x^2 # merg Pythagoras.Y01 2*x_y_z + 2*x_y_z^2 # orig Pythagoras.Y01 -(1+2*x+2*x^2)^2 # flat Pythagoras.Y01 2*x + 2*x^2 + 1 # merg Pythagoras.Y01 2*x_y_z + 2*x_y_z^2 + 1 # poly Pythagoras.Y01 0 000012 [3,4,5] Pythagoras.Y01 factor=1 parm= [1] 000030 [5,12,13] Pythagoras.Y01 factor=1 parm= [2] 000056 [7,24,25] Pythagoras.Y01 factor=1 parm= [3] 000090 [9,40,41] Pythagoras.Y01 factor=1 parm= [4] 000132 [11,60,61] Pythagoras.Y01 factor=1 parm= [5] 000182 [13,84,85] Pythagoras.Y01 factor=1 parm= [6] 000240 [15,112,113] Pythagoras.Y01 factor=1 parm= [7] 000306 [17,144,145] Pythagoras.Y01 factor=1 parm= [8] 000380 [19,180,181] Pythagoras.Y01 factor=1 parm= [9] 000462 [21,220,221] Pythagoras.Y01 factor=1 parm= [10] 000552 [23,264,265] Pythagoras.Y01 factor=1 parm= [11] 000650 [25,312,313] Pythagoras.Y01 factor=1 parm= [12] 000756 [27,364,365] Pythagoras.Y01 factor=1 parm= [13] 000870 [29,420,421] Pythagoras.Y01 factor=1 parm= [14] 000992 [31,480,481] Pythagoras.Y01 factor=1 parm= [15]
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clear; clf; avect = 0.5:0.1:2.5; // Vecteurs des différentes valeurs de a (population initiale) h = 0.1; // pas de temps r = 0.4; K = 2; A = 1; // variables globales de la formule de la vitesse d'accroissement function f = logistique(x); // fonction qui calcule la vitesse d'accroissement f = r * x .*((x/A -1).* (1 - x / K)); // opérations vectorielles. x est un vecteur endfunction ndate = 0:h:20; // le vecteur des instants où on calcule la solution for i= 1:21; // Boucle qui dessine les courbes x(1) = avect(i); // Initialisation de la population initiale for n = 1:length(ndate) - 1; // Boucle qui calcul la population pour une valeur de a x(n+1) = x(n) + h * logistique(x(n)); // Calcul de la population end plot2d(ndate, x, style = i); // Tracé de la trajectoire. end
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// Determine structure and lattice parameter of material clc d = 114.6 // diameter of power camera in angstrom lambda = 1.54 // wavelength in angstrom s1 = 86 s2 = 100 s3 = 148 s4 = 180 s5 = 188 s6 = 232 s7 = 272 printf("\n Example 3.8") R = d/2 // Radius if R==57.3 then k = 1/4 // Bragg angle factor end a1 = (sin(s1*k*%pi/180))^2 a2 = (sin(s2*k*%pi/180))^2 a3 = (sin(s3*k*%pi/180))^2 a4 = (sin(s4*k*%pi/180))^2 a5 = (sin(s5*k*%pi/180))^2 a6 = (sin(s6*k*%pi/180))^2 a7 = (sin(s7*k*%pi/180))^2 c = 22 // constant to convert into integral number printf("\n Within experimental error, values are as in integral ratio are as: \n %d:%d:%d:%d:%d:%d:%d",ceil(c*a1),ceil(c*a2),ceil(c*a3),ceil(c*a4),ceil(c*a5),ceil(c*a6),ceil(c*a7)) printf("\n So, this structure is FCC and material is copper with 3.62 angstrom lattice parameter")
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//EXAMPLE 4-57 PG N 265-266 Z1=[200 +%i*4;0 5+%i*10]; Z2=[2+%i*5 %i*4;%i*4 5+%i*10]; I1=det(Z1/Z2); disp('i) Current (I1) is = '+string (I1) +' A '); Z3=[2+%i*5 %i*4;%i*4 5+%i*10]; Z4=[2+%i*5 %i*4;%i*4 5+%i*10]; I2=det(Z3/Z4); disp('ii) Current (I2) is = '+string (I2) +' A ');
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disp('chapter 3 ex3.4') disp('given') disp('signal amplitude Vi=15mV') disp('IBmax=500nA and I2=100*IBmax') Vi=.015 IBmax=500*10^(-9) I2=100*IBmax disp('R3=Vi/I2') R3=Vi/I2 disp('ohms',R3) disp('standard value resistor for R3=270ohms') R3=270 disp('I2=Vi/R3') I2=Vi/R3 disp('amperes',I2) disp('Vo=Av*Vi') Av=66 Vo=Av*Vi disp('volt',Vo) disp('R2=Vo/I2-R3') R2=Vo/I2-R3 disp('ohms',R2) disp('standard value resistor to give Av>66 R2=18kohms') R2=18000 disp('R1=R2||R3') R1=R2*R3/(R2+R3) disp('ohms',R1) disp('standard value resistor R1=270ohms') R1=270 disp('ohms',R1)
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clc //initialisation of variables w=1.0//cfs w1=3.0//cfs w2=45.0//cfs v=3.0//fps h=144//ft D=12*sqrt(4*w/(%pi*w1))//in d1=1.95//cfs D1=12*sqrt(4*d1)/(%pi*v)//in d2=41.6//cfs D2=12*sqrt(4*d2)/(%pi*w1)//ins //CALCULATIONS C=%pi*(D)^2*3/(4*h)//cfs C1=%pi*(1/4)*3//cfs V=(d2*4)/(%pi*4^2)//fps //RESULTS printf('The minimum dry-weather flow =% f cfs',C) printf('The maximum dry-weather flow in excess actual capacity=% f cfs',C1) printf('the storm flow in axcess of maximum dry-weather flow=% f fps',V)
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//variable initialization z=2 //atomic no. of He atom h=1.054*10^-34; //Planck's constant (joule second) R=10967800; //Rydberg constant (m-1) e=1.6*10^-19; //Charge of electron (coulombs) c=3*10^8; //speed of light (m/s) //calculation E=1.5*%pi*h*c*R*z^2; //The energy of the emitted photon (J) IE=2*%pi*h*c*R; //Ionization energy of H atom (J) KE=(E-IE)/e; //Kinetic energy of the photoelectron (eV) printf("\nKinetic energy of photoelectron = %.1f eV",KE);
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//this function minimizes a two vriable boolean expression using kmap function bi =kmap2(k) var=['A''B''' 'A''B' 'AB' 'AB'''] temp =1 for i=1:2 // intially checking for all 1's for j=1:2 if k(i,j)==1 then temp = temp + 1; end end end v=0; bi = ' ' ; if temp == 5 then disp("The minimal expression is : 1'); v=1; else for i= 1 : 2 // considering all 2 1's cases if k(i,1) == 1 & k(i,2) == 1 then if i== 1 then bi = strcat([ bi 'A'''] );v=1; else bi = strcat([ bi 'A']);v=1; end bi = strcat([ bi " + " ]); end if k(1,i) == 1 & k(2,i) == 1 then if i== 1 then bi = strcat([ bi 'B'''] );v=1; else bi = strcat([ bi 'B']);v=1; end end end end; one(1)=k(2,1); f=2;m=2;i=1; for j=1:2 one(f)=k(i,j) f=f+1; end i=2; for j=2:-1:1 one(f)=k(i,j) f=f+1; end one(6)=k(1,1); if v==0 then // for isolated 1's for i =2:5 if one(i)==1 & one(i+1)== 0 & one(i-1) ==0 then if m>0 bi = strcat([bi " + "]); end; bi = strcat([bi var(i-1)]); m=m+1; end end end endfunction // final result will be stored in bi
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// Builder gateway function for PSK modulation function builder_gw_cpp() WITHOUT_AUTO_PUTLHSVAR = %t; tbx_build_gateway("skeleton_cpp", .. ["psk_mod","itpp_psk_mod"], .. ["itpp_psk_mod.cpp"], .. get_absolute_file_path("builder_gateway_cpp.sce"), [], "-litpp"); endfunction builder_gw_cpp(); clear builder_gw_cpp; // remove builder_gw_cpp on stack
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//Variable declaration Vcc=15. //supply voltage(V) Rl=10. //load resistance(ohms) //Calculations //Part a Immax=Vcc/Rl //max peak current(A) Irmsmax=Immax/(sqrt(2)) //max rms current(A) Pomax=Irmsmax**2*Rl //max output power(W) Pi=(2*Vcc*Immax)/%pi //max input power(W) eta=Pomax/Pi //efficiency //Part b Im=(2*Vcc)/(%pi*Rl) //peak current(A) Pdmax=((2*Vcc*Im)/(%pi))-((Im**2*Rl)/2) //max power dissipated(W) eta1=((Im**2)*Rl*%pi)/(2*2*Vcc*Im) //efficiency //Results printf ("a)max signal output power,collector dissipation are %.2f W , %.2f W and efficiency is %.2f %%",Pomax,Pi,eta/1E-2) printf ("b)max dissipation of each transistor and corresponding efficiency is %.2f W and %.1f resp.",Pdmax,eta1)
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//Chapter 10, Example 10.6, Page 285 clc clear // mass of U235 m = (((4/3)*%pi*125**3*1.60)*235)/(40000*12) printf(" m = %f kg \n",m*10**-3) //Answer may vary due to round off error
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function ledblink_brightness() for x=1:10 //Run for 10 iterations p = cmd_analog_in(1,2); if(p>0 & p<320) then //threshold one cmd_analog_out(1,9,p); elseif p>=320 & p<=900 //threshold two cmd_analog_out(1,10,p); elseif p>900 & p<=1023 //threshold three cmd_analog_out(1,11,p); end end endfunction
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//Example 1.1b //Determine whether the given signal is periodic or not clc; t=0:1/100:5 x=sin(sqrt(2)*%pi*t); plot(x); disp('ploting the signal and showing that itis periodic with period=2pi/sqrt(2)pi');
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<?xml version="1.0" encoding="utf-8"?> <test> <description>StdProject2D Triangle Modified basis P=6 Q=7</description> <executable>StdProject</executable> <parameters>-s triangle -b Modified_A Modified_B -o 6 6 -p 7 7</parameters> <metrics> <metric type="L2" id="1"> <value tolerance="1e-12">2.18252e-14</value> </metric> <metric type="Linf" id="2"> <value tolerance="1e-12">5.15143e-14</value> </metric> </metrics> </test>
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clc //Example 4.3 //Determination of e //------------------------------------------------------------------------------ //Given data //Dimensions of I section ro=0.125 //m ri=0.06 //m bi=0.06 //m bo=0.05 //m t=0.01 //m h=0.065 //m ti=0.015 //m to=0.01 //m res3=mopen(TMPDIR+'3_determination_of_e.txt','wt') mfprintf(res3,'(a)\te=R-rn\n\n') mfprintf(res3,'(b) Calculation of rn:\n') mfprintf(res3,'\trn=(((bi-t)*ti)+((bo-t)*to)+(t*h))/((bi*log((ri+ti)/ri))+(t*log((ro-to)/(ri+ti)))+(bo*log(ro/(ro-to))))\n') rn=(((bi-t)*ti)+((bo-t)*to)+(t*h))/((bi*log((ri+ti)/ri))+(t*log((ro-to)/(ri+ti)))+(bo*log(ro/(ro-to)))) mfprintf(res3,'\trn=%0.4f mm\n\n',rn* 10^3) mfprintf(res3,'(c)Calculation of R:\n') mfprintf(res3,'\tR=ri+ ((0.5* h^2 *t)+(0.5* ti^2 *(bi-t))+((bo-t)*to*(h- 0.5*to)))/(((bi-t)*ti)+((bo-t)*to)+(t*h))\n') R=ri+ ((0.5* h^2 *t)+(0.5* ti^2 *(bi-t))+((bo-t)*to*(h- 0.5*to)))/(((bi-t)*ti)+((bo-t)*to)+(t*h)) mfprintf(res3,'\tR=%0.4f mm\n\n',R* 10^3) e=R-rn mfprintf(res3,'(d)e=R-rn= %0.4f mm',e* 10^3) mclose(res3) editor(TMPDIR+'3_determination_of_e.txt') //------------------------------------------------------------------------------ //-----------------------------End of program-----------------------------------
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clear; clc; // A Textbook on HEAT TRANSFER by S P SUKHATME // Chapter 2 // Heat Conduction in Solids // Example 2.11(a) // Page 65 printf("Example 2.11(a), Page 65 \n\n") D = 0.05 ; // [m] To = 450 ; // [degree C] Tf = 90 ; // [degree C] T = 150 ; // [degree c] h = 115 ; // [W/m^2 K] rho = 8000 ; // [kg/m^3] Cp = 0.42*1000 ; // [J/kg K] k = 46 ; // [W/m K] R = D/2; // (a) // From eqn 2.7.3 for a sphere t1 = rho*Cp*R/(3*h)*log((To-Tf)/(T-Tf)); // [sec] t1_min = t1/60 ; // [min] printf("Time taken by the centre of the ball to reach 150 degree C if internal gradients are neglected is %f seconds i.e. %f minutes \n",t1,t1_min);
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// Example 1.73 clc;clear;close; // Given data format('v',6); StatorLoss=2;//in KW StatorInput=90;//stator input in KW S=4;//in % //calculations S=S/100;//slip StatorOutput=StatorInput-StatorLoss;//in KW Pri=StatorOutput;//rotor input in KW Pcr=S*Pri;//in KW disp(Pcr,"Rotor Copper Loss in KW : "); Pm=Pri-Pcr;//in KW disp(Pm,"Rotor mechanical power developed in KW : ");
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//Example 6.4 //Page 325 //Refer to figure 6.17 on page 300 disp('SNR detector is 3dB higher than Eb/N0, therefore') snr=13.7//SNR=13.7dB disp('Since 4 PSK modulation provides 2bps/Hz, the sampling rate is 5 MHz, which is Nqyuist rate, therefore') a1=10*log10(125000000000000) a2=10*log10(1.3) A0=a1-13.7-7-3-a2 disp('At a carrier frequency of 2GHz, the wavelength is') (3*10^8)/(2*10^9) FM=116+60+20*log10(0.15)-5-20*log10(4*%pi*5*10^4)//Fade Margin can be found by Equation 6.31 //Result //A0 = 116dB //wavelength = 0.15 m //Fade Margin = 38.5 dB
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errcatch(-1,"stop");mode(2);// Example 1.65. turning moment , // given : l=0.03; // in m B=0.09; // in Wb/m^2 I=0.01; // in A N=100; // number of turn T=(N*B*I*l^2); disp(T,"turning moment,T(N-m) = ") exit();
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// sum 3-3 clc; clear; m=25; v=3; E=210*10^3; KE=0.5*m*v^2; d=30; L=2000; A=%pi*d^2/4; U=A*L/(2*E); del=4*10^-5*A; W=A*del; sigi=sqrt(KE*10^3/(W+U)); // printing data in scilab o/p window printf("del is %f N/mm^2 ",sigi);
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clear; clc; //Example 2.15 //Caption : Program To find the Heat to be Removed during Compression //Given values V=600;//[m/s] W_compression=240;//[KJ/Kg] //Solution //Using Eqn(2.32a) Q=(1/2*(V*V)/1000)-W_compression; disp('KJ/kg',-Q,'Thus Heat Removed from each KG of air compressed is') //End
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// FUNDAMENTALS OF ELECTICAL MACHINES // M.A.SALAM // NAROSA PUBLISHING HOUSE // SECOND EDITION // Chapter 3 : TRANSFORMER AND PER UNIT SYSTEM // Example : 3.11 clc;clear; // clears the console and command history // Given data V_1 = 200 // voltage in V f = 50 // frequency in Hz I_0 = 0.6 // single phase current in A P_0 = 80 // power in W // caclulations cos_phi0 = P_0/(V_1*I_0) // power factor sin_phi0 = 0.74 // from above expression I_w = I_0*cos_phi0 // working component of no load current in A I_m = I_0*sin_phi0 // working component of no load current in A R_0 = V_1/I_w // no load circuit resistance in ohm X_0 = V_1/I_m // no load circuit reactance in ohm // display the result disp("Example 3.11 solution"); printf(" \n No-load circuit resistance \n R_0 = %.2f ohm \n", R_0); printf(" \n No-load circuit reactance \n X_0 = %.1f ohm \n", X_0);
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clear // // // //Variable declaration e=1.6*10**-19 //charge(c) mewn=0.21 //electron mobility(m**2/Vs) T=300 //temperature(K) KB=1.38*10**-23 //boltzmann constant //Calculation Dn=mewn*KB*T/e //diffusion coefficient(m**2/sec) //Result
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//Finding resistance //Example 2.5(pg. 23) clc clear R0=80//in ohms t=40// in degree C k0=0.0043 R40=R0*(1+(k0*t)) printf('The value of Resistance at 40 degree C is %3.2f ohms',R40)
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clc clear printf("example 2.22 page number 79\n\n") //to find the emf of cell E0_Ag=0.80; E0_AgNO3=0.80; c_Ag=0.001; c_AgNO3=0.1; E_Ag=E0_Ag+(0.059)*log10(c_Ag); E_AgNO3=E0_AgNO3+(0.059)*log10(c_AgNO3); E=E_AgNO3-E_Ag; printf("emf of cell = %f V" ,E) printf("\n\nsince E is positive, the left hand electrode will be anode and the electron will travel in the external circuit from the left hand to the right hand electrode")
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clc //Initialization of variables d=500 //ft Pi=14 //lb/in^2 Pd=15 //lb/in^2 Sv=0.016 //ft^3 /lb //calculations Wi=144*Pi*Sv Wf=144*Pd*Sv PEi=0 PEf=d Winput=Wf-Wi+PEf-PEi //results printf("Input work = %.1f ft-lb/lbm",Winput)
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function [vel,regionlist,linelist,seedlist,velolist]=velpic(nz,nx,sext) //[vel,regionlist,linelist,seedlist]=velpic(nz,nx) //Macro which interactively defines regions of a matrix. //Closed surfaces inside the frame are not allowed. // nz :Number of columns in the matrix // nx :Number of rows in the matrix // vel :velocity matrix // sext :[smin,smax] gives the velocities min and max // regionlist :list whose elements are matrices of dimension // :(2xN) containing the indices of the different regions // linelist :list whose elements are matrices of dimension (2xM) // :containing the indices of the different lines // seedlist :(2xK) vector containing positions of seeds // velolist :(1xK) vector containing velocities associated to seeds // //! // author: C. Bunks date: 12-NOV-90 [lhs,rhs]=argn(0) //turn off the scilab function 'more' nrnc=lines(); lines(0); // qt='off' // select rhs case 2 then smin=1500;smax=6000; rnd=100 case 3 then smin=sext(1);smax=sext(2) rnd=10**int(-1+log(abs(smax-smin))/log(10)) else error('velpic(nz,nx [,sext])') end //make a suitable frame bnames=list('stop','help','undo','grill','quit'); gopt='off'; [buttons,slides]=makeframe(nz,nx,bnames); slide1=slides(1,:); //seperate matrix into regions defined by lines linelist=makehorizons(nz,nx,bnames,buttons); if qt='on' then return,end //determine indices of matrix in each region write(%io(2),'Searching Regions'), regionlist=list(); indexlist=[ones(1,nz).*.(1:nx);(1:nz).*.ones(1,nx)]; region=0; while size(indexlist)<>[0 0], region=region+1; seed=indexlist(:,1); [inds,indexlist]=id_rgn(indexlist,linelist,seed); regionlist(region)=inds; write(%io(2),' Region Identified: '+string(region)), end, //sow a seed in each region [seedlist]=sow(nz,nx,slide1,bnames,buttons,regionlist,linelist); if qt='on' then return,end [ssl,isl]=sort(seedlist(3,:));//sort seeds and velocities to regions [sr,sc]=size(seedlist); velolist=seedlist(4,isl(sc:-1:1)); rolist=seedlist(3,isl(sc:-1:1)); seedlist=seedlist(1:3,isl(sc:-1:1)); //Load velocity matrix with velocities by region. i2=0; vel=0*ones(1,nz*nx); nor=size(regionlist); nov=maxi(size(velolist)); write(%io(2),'Building velocity matrix'), for k=1:nor, i1=i2+1;i2=i1-1; for j=1:nov, if rolist(j)=k then, i2=i2+1; end, end, rk=regionlist(k); rv=(rk(1,:)-ones(rk(1,:)))*nz+rk(2,:); if i1=i2 then,//constant velocity region vel(rv)=velolist(i1:i2)*ones(rv); else,//linearly varying velocity region vel(rv)=velcalc(rk,seedlist(:,i1:i2),velolist(i1:i2)); end, end, vel=matrix(vel,nz,nx); vel=vel(nz:-1:1,:); //re-establish the line counter lines(nrnc(2)); function []=helpme(msn) //[]=helpme(msn) //macro containing help messages // msn :message number // //! // author: C. Bunks date: 12-NOV-90 hm1=[' '; 'Begin drawing a line by clicking the left'; 'mouse button across a previously drawn line'; 'segment or across a frame line segment. In'; 'the second case the first mouse click must'; 'be in the margin.'; ' '; 'STOP:'; ' Stop drawing lines and start picking velocities'; ' '; 'HELP:'; ' This help message'; ' '; 'UNDO:'; ' Undo a previously drawn line'; ' '; 'GRILL:'; ' Toggle grill on/off'; ' ']; hm2=[' '; 'Terminate drawing a line by clicking the left'; 'mouse button across a previously drawn line'; 'segment or across a frame line segment.'; ' '; 'STOP:'; ' Completely undo the current line and begin'; ' drawing a new line'; ' '; 'HELP:'; ' This help messaage'; ' '; 'UNDO:'; ' Undo a line segment'; ' '; 'GRILL:'; ' Toggle grill on/off'; ' ']; hm3=[' '; 'To sow a seed, choose a velocity by clicking'; 'the left mouse button in the velocity slide.'; ' '; 'The velocity value chosen on the slide'; 'is echoed to the terminal.'; ' '; 'To change the velocity value click the left'; 'mouse button at another location on the slide.'; ' '; 'When a suitable velocity value has been obtained'; 'click the left mouse button somewhere in the frame'; 'to plant the velocity seed'; ' '; 'Multiple seeds in the same region yields linear'; 'velocity gradients. The linear gradients are'; 'established between consecutive seed values'; '(following the order of placement)'; ' '; 'STOP:'; ' Stop planting seeds and return velocity matrix'; ' '; 'HELP:'; ' This help message'; ' '; 'UNDO:'; ' Undo a seed placement'; ' '; 'GRILL:'; ' Toggle grill on/off'; ' ']; hmt=list(hm1,hm2,hm3); x_message(hmt(msn)); function [seedlist]=sow(nz,nx,slide,bnames,buttons,regionlist,linelist); //[seedlist]=sow(nz,nx,slide,bnames,buttons,regionlist,linelist); //Interactively identify the various regions by clicking //the mouse in each region // nz :number of rows of matrix // nx :number of columns of matrix // nol :number of lines (not including the boundary) // slide :slide information // bnames :button names // buttons :button positions // regionlist :list of regions // seedlist :(4xN) matrix where each column contains (from top to // :bottom) the x and y coordinates of the seed, the region // :that the seed is in, and the velocity value associated // :to the seed // //! // author: C. Bunks date: 12-NOV-90 sl1=slide(1);sl2=slide(2);sl3=slide(3); sl4=slide(4);sl5=slide(5);sl6=slide(6); seedlist=[]; //slide bar constants vbar=[0 0 0 0 0;0 0 0 0 0]; if nx<=nz then, sw=sl2-sl1; b1=sl1+.05*sw;b2=sl2-.05*sw; b3=.05*sw;b4=.05*sw; else, sw=sl4-sl3; b1=.05*sw;b2=.05*sw b3=sl3+.05*sw;b4=sl4-.05*sw; end, //get velocity and place seed nol=size(linelist); nor=size(regionlist); sflag='on'; while sflag='on', write(%io(2),'Choose Velocity'), veloflag='on'; vel=-1; while veloflag='on',//loop until desired vel is obtained [i_i,v1,v2]=xclick();v=[v1;v2]; //check for a button [br,bc]=size(buttons); hflag='on'; while hflag='on', hflag='off'; for bi=1:br, if buttons(bi,1)<v1 then, if v1<buttons(bi,2) then, if buttons(bi,3)<v2 then, if v2<buttons(bi,4) then, select bnames(bi) case 'help' then, helpme(3); [i_i,v1,v2]=xclick();v=[v1;v2]; hflag='on'; case 'stop' then,//stop sowing (all regions >= one seed) [sr,sc]=size(seedlist); rflag='off'; for rk=1:nol, srflag='off'; for sk=1:sc, if seedlist(3,sk)=rk then, srflag='on'; end, end, if srflag='off' then, rflag='on'; end, end, if rflag='on' then, write(%io(2),'Not every region has a seed'), write(%io(2),'Choose Velocity'), [i,v1,v2]=xclick();v=[v1;v2]; hflag='on'; else, sflag='off'; veloflag='off'; end, case 'grill' then, if gopt='on' then, gopt='off'; else, gopt='on'; end, makegrill(nx,nz,gopt); [i,v1,v2]=xclick();v=[v1;v2]; hflag='on'; case 'undo' then,//undo line segment [sr,sc]=size(seedlist); toff=.05*maxi([nx,nz])/3; if sc>0 then, s1=seedlist(1,sc); s2=seedlist(2,sc); text=string(seedlist(4,sc)); dess(36)=15; xset("alufunction",6); plot2d(s1',s2',[-3,0],"000"); xstring(s1+toff,s2+toff,text,0,0); xset("alufunction",3); seedlist=seedlist(:,1:sc-1); else, write(%io(2),'Nothing to undo'), write(%io(2),'Choose Velocity'), end, [i,v1,v2]=xclick();v=[v1;v2]; hflag='on'; case 'quit' then, qt=resume('on'); end, end,end, end,end, end, end, if sflag='on' then,//stop hasn't been signalled //get velocity if sl1<=v1 then, if v1<=sl2 then, if sl3<=v2 then, if v2<=sl4 then, //calculate velocity rounded to nearest rnd //plot bar indicator and give velocity value xset("alufunction",6); plot2d(vbar(1,:)',vbar(2,:)',[1],"000"); xset("alufunction",3); if nx<=nz then, vel=rnd*round((sl5+(sl6-sl5)*(v2-sl3)/(sl4-sl3))/rnd); vbar=[b1 b2 b2 b1 b1;v2-b3 v2-b3 v2+b4 v2+b4 v2-b3]; plot2d(vbar(1,:)',vbar(2,:)',[1],"000"), else, vel=rnd*round((sl5+(sl6-sl5)*(v1-sl1)/(sl2-sl1))/rnd); vbar=[v1-b1 v1+b2 v1+b2 v1-b1 v1-b1;b3 b3 b4 b4 b3]; plot2d(vbar(1,:)',vbar(2,:)',[1],"000"), end, write(%io(2),vel,'(f10)'), end,end, end,end, if vel<>-1 then,//check that a velocity was chosen //plant seed if 1<=v1 then, if v1<=nx then, if 1<=v2 then, if v2<=nz then, //find the region that v is in rflag='on'; nr=0; while rflag='on',//look for a region that contains seed nr=nr+1; rk=regionlist(nr); rflag='off'; for nl=1:nol,//for this region check all lines [testflag,bav]=testpt(v,rk(:,1),linelist(nl)); if testflag='on' then, rflag='on'; end, end, if rflag='off' then,//this region if no intersections sregion=nr; end, end, //plot seed and add to seedlist mrgn=.05*maxi([nx,nz])/3; plot2d(v1',v2',[-3,0],"000"); xstring(v1+mrgn,v2+mrgn,string(vel),0,0); seedlist=[seedlist,[v;sregion;vel]]; veloflag='off'; end,end, end,end, end, end, end, end, function [linelist]=makehorizons(nz,nx,bnames,buttons) //[linelist]=makehorizons(nz,nx,bnames,buttons) //macro which creates a frame with control buttons and //interactively draws lines (i.e., horizons) // nz :Number of rows in frame // nx :Number of columns in frame // bnames :Button names // buttons :Button locations // linelist :list whose elements are (2xN) matrices of line indices // //! // author: C. Bunks date: 12-NOV-90 //define outer perimeter as a line prt=.001; linelist=list([1-prt 1-prt nx+prt nx+prt 1-prt;... 1-prt nz+prt nz+prt 1-prt 1-prt]); nol=size(linelist); //start line drawing layer='true'; yec=[]; while layer='true', nol=nol+1; //Define layer by drawing a line write(%io(2),'Draw a Line'), [line,linelist,yec]=drawline(nz,nx,linelist,yec,bnames,buttons); if size(line)=[0,0] then,//if returned line is empty then stop layer='false'; else if line=0 then, nol=nol-1; else, nol=size(linelist); nol=nol+1; linelist(nol)=line; end, end, end, function [buttons,slides]=makeframe(nz,nx,btextlist); //[buttons,slides]=makeframe(nz,nx,btextlist); //macro which makes a frame and buttons // nz :Number of rows in frame // nx :Number of columns in frame // btextlist :text for buttons // buttons :button information // slides :slide information // //! // author: C. Bunks date: 12-NOV-90 //setup of frame //draw work box. //note that the work box is placed in [1,nx] x [1,nz] //and that the remaining elements are for centering properly //the box (i.e., mrgn and the 1). maxx=maxi([nz,nx]); mrgn=.05*(maxx-1); xmin=1-mrgn-maxx+nx;xmax=maxx+4*mrgn; ymin=1-mrgn-maxx+nz;ymax=maxx+4*mrgn; if nx>nz+4*mrgn then, xmin=1-mrgn-maxx+nx;xmax=maxx+mrgn; ymin=1-mrgn-maxx+nz;ymax=maxx+mrgn; end, if nx<nz-4*mrgn xmin=1-mrgn-maxx+nx;xmax=maxx+4*mrgn; ymin=1-mrgn-maxx+nz;ymax=maxx+mrgn; end, rect=[xmin,ymin,xmax,ymax]; plot2d(0,0,[1],"012",' ',rect); plot2d([1;1;nx;nx;1],[nz;1;1;nz;nz],[1],"000"), //make buttons and slides dess4=10 dess6=10 dx=(xmax-xmin)/dess4 dy=(ymax-ymin)/dess6 //make button bank bs=size(btextlist);//number of buttons bsi=1/(2*bs); buttons=[]; if nz=>nx then,//in the right side margin bc=int(bs/(4+bsi))+1;//number of columns br=int(bs/(bc+bsi))+1;//number of rows bm=2*mrgn/(bc+1); bentry=0; for bj=1:bc,for bi=1:br, xbmin=nx+2*(bj-1)*bm+bm;xbmax=xbmin+2*bm; ybmax=nz-2*(bi-1)*bm;ybmin=ybmax-2*bm; bentry=bentry+1; if bentry<=bs then, text=btextlist(bentry); else, text=' '; end, makebutton(xbmin,xbmax,ybmin,ybmax,dx,dy,text); buttons=[buttons;xbmin,xbmax,ybmin,ybmax]; end,end, else,//in the top margin br=int(bs/(4+bsi))+1;//number of rows bc=int(bs/(br+bsi))+1;//number of columns bm=2*mrgn/(br+1); bentry=0; for bi=1:br,for bj=1:bc, xbmin=1+2*(bj-1)*bm;xbmax=xbmin+2*bm; ybmin=nz+2*(bi-1)*bm+bm;ybmax=ybmin+2*bm; bentry=bentry+1; if bentry<=bs then, text=btextlist(bentry); else, text=' '; end, makebutton(xbmin,xbmax,ybmin,ybmax,dx,dy,text); buttons=[buttons;xbmin,xbmax,ybmin,ybmax]; end,end, end, //velocity slide if nz=>nx then, xbmin=nx+mrgn;xbmax=xbmin+2*mrgn; ybmin=1;ybmax=(1+nz)/2; else, xbmin=(1+nx)/2;xbmax=nx; ybmin=nz+mrgn;ybmax=ybmin+2*mrgn; end, text='VEL'; dx=(xmax-xmin)/dess4; dy=(ymax-ymin)/dess6; makeslide(xbmin,xbmax,ybmin,ybmax,dx,dy,text,smin,smax); slides=[xbmin,xbmax,ybmin,ybmax,smin,smax]; function []=makebutton(xbmin,xbmax,ybmin,ybmax,dx,dy,text) //[]=makebutton(xbmin,xbmax,ybmin,ybmax,dx,dy,text) //make to make a button // xbmin :min x coordinate of button // xbmax :max x coordinate of button // ybmin :min y coordinate of button // ybmax :max y coordinate of button // dx :ratio of plot length to frame length: (xmax-xmin)/dess(4) // dy :ratio of plot height to frame height: (ymin-ymax)/dess(6) // text :text in button // //! // author: C. Bunks date: 12-NOV-90 //make button box xstringb(xbmin,ybmin,text,xbmax-xbmin,ybmax-ybmin); xrect(xbmin,ybmax,xbmax-xbmin,ybmax-ybmin); function []=makeslide(xbmin,xbmax,ybmin,ybmax,dx,dy,text,smin,smax) //[]=makeslide(xbmin,xbmax,ybmin,ybmax,dx,dy,text) //make to make a button // xbmin :min x coordinate of button // xbmax :max x coordinate of button // ybmin :min y coordinate of button // ybmax :max y coordinate of button // dx :ratio of plot length to frame length: (xmax-xmin)/dess(4) // dy :ratio of plot height to frame height: (ymin-ymax)/dess(6) // text :text in button // smin :min value of slide // smax :max value of slide // //! // author: C. Bunks date: 12-NOV-90 //NOTE: The constant wcf is a 'wierd correction factor necessary //for the correct positioning of the text in the button. I don't //understand why it is needed... wcf=1.3; //make slide box xvec=[xbmin xbmin xbmax xbmax xbmin];//x button frame vector yvec=[ybmax ybmin ybmin ybmax ybmax];//y button frame vector delx=xbmax-xbmin;dely=ybmax-ybmin; //label slide dess(27)=1;//soft caracters sl=length(text); if delx<dely then, cw=(xbmax-xbmin)/(dx*sl);//char.width=.9*(box width)/(text length) else, cw=(ybmax-ybmin)/(dx*sl); end, ch=cw/.82; // setcsize(cw,ch); textx=(xbmin+xbmax-dx*sl*cw/wcf)/2;//text x position texty=(ybmin+ybmax-dy*ch/wcf)/2;//text y position dess(51)=2;//turn labelling on dess(50)=textx;dess(52)=texty;//positions of text plot2d(xvec',yvec',[1],"000"); xstring(textx,texty,text,0,0), //label min value of slide text=string(smin); sl=length(text); if delx<dely then, cw=(xbmax-xbmin)/(dx*sl); ch=cw/.82; textx=(xbmin+xbmax-dx*sl*cw/wcf)/2;//text x position texty=ybmin+dy*ch/wcf/2;//text y position else, cw=(ybmax-ybmin)/(dx*sl); ch=cw/.82; textx=xbmin+dx*cw/wcf;//text x position texty=(ybmin+ybmax-dy*cw/wcf)/2;//text y position end, // setcsize(cw,ch); dess(51)=2;//turn labelling on dess(50)=textx;dess(52)=texty;//positions of text xstring(textx,texty,text,0,0), //label max value of slide text=string(smax); sl=length(text); if delx<dely then, cw=(xbmax-xbmin)/(dx*sl); ch=cw/.82; textx=(xbmin+xbmax-dx*sl*cw/wcf)/2;//text x position texty=ybmax-3*dy*ch/wcf/2;//text y position else, cw=(ybmax-ybmin)/(dx*sl); ch=cw/.82; textx=xbmax-dx*(1+sl)*cw/wcf;//text x position texty=(ybmin+ybmax-dy*cw/wcf)/2;//text y position end, // setcsize(cw,ch); dess(51)=2;//turn labelling on dess(50)=textx;dess(52)=texty;//positions of text xstring(textx,texty,text,0,0), function [line,linelist,yec]=drawline(nz,nx,linelist,yec,bnames,buttons) //[line,linelist,yec]=drawline(nz,nx,linelist,yec,bnames,buttons) //interactively draw a line // nz :number of columns of matrix // nx :number of rows of matrix // linelist :list containing the matrices of indices for // :each line // yec :extension list // bnames :Names of buttons // buttons :Button locations // line :new line // //! // author: C. Bunks date: 12-NOV-90 //to begin new line the first two clicks of the mouse must //intersect an old line or the frame line=[]; [i,x1,x2]=xclick(); testflag='off'; flag='on'; //check for a button [br,bc]=size(buttons); hflag='on'; while hflag='on',//while the mouse has been clicked in a button hflag='off'; for bi=1:br,//check all the buttons if buttons(bi,1)<x1 then, if x1<buttons(bi,2) then, if buttons(bi,3)<x2 then, if x2<buttons(bi,4) then, select bnames(bi) case 'help' then, helpme(1); [i_i,x1,x2]=xclick(); hflag='on'; case 'stop' then, testflag='on'; flag='off'; yecl=0; case 'grill' then, if gopt='on' then, gopt='off'; else, gopt='on'; end, makegrill(nx,nz,gopt); [i_i,x1,x2]=xclick(); hflag='on'; case 'undo' then,//undo last line ls=size(linelist); if ls>1 then,//remove a line [yer,yecc]=size(yec); yf=yec(1,yecc); yl=yec(2,yecc); lk=linelist(ls); [lkr,lkc]=size(lk); xset("alufunction",6); plot2d(lk(1,yf+1:lkc-yl)',lk(2,yf+1:lkc-yl)',[1],"000"), xset("alufunction",3); ltemp=list(); for k=1:ls-1, ltemp(k)=linelist(k); end, linelist=ltemp; yec=yec(:,1:yecc-1); else, write(%io(2),'Nothing to undo'), end, [i_i,x1,x2]=xclick(); hflag='on'; case 'quit' then, qt=resume('on') end, end,end, end,end, end, end, //start drawing line yext=[]; while testflag='off', plot2d(x1',x2',[-3,-1],"000");//make a start circle [i_i,y1,y2]=xclick(); //check for a button [br,bc]=size(buttons); hflag='on'; while hflag='on' hflag='off'; for bi=1:br, if buttons(bi,1)<y1 then, if y1<buttons(bi,2) then, if buttons(bi,3)<y2 then, if y2<buttons(bi,4) then, select bnames(bi) case 'help' then, helpme(1); [i_i,y1,y2]=xclick(); hflag='on'; case 'stop' then, write(%io(2),'Nothing to stop'), [i_i,y1,y2]=xclick(); hflag='on'; case 'grill' then, if gopt='on' then, gopt='off'; else, gopt='on'; end, makegrill(nx,nz,gopt); [i_i,y1,y2]=xclick(); hflag='on'; case 'undo' then, write(%io(2),'Nothing to undo'), [i_i,y1,y2]=xclick(); hflag='on'; case 'quit' then, qt=resume('on'); end, end,end, end,end, end, end, //if line segment defined by first two points intersects a //previously defined line and y is in the frame then start a new line inflag='off'; if 1<=y1 then, if y1<=nx then,//y in the frame if 1<=y2 then, if y2<=nz then, inflag='on'; xsec=[];//list of intersections nol=size(linelist); for ln=1:nol,//test against all the lines for intersections [testflag,bav]=testpt([x1;x2],[y1;y2],linelist(ln)); [br,bc]=size(bav); xsec=[xsec,[bav;ln*ones(1,bc)]]; end, //choose longest intersection which yields shortest segment //and add on the necessary extensions [xr,xc]=size(xsec); if xc>0 then, testflag='on'; btemp=xsec(1:2,:)-[x1;x2]*ones(1,xc); [val,in]=maxi([1 1]*(btemp.*btemp));//longest intersection xset("alufunction",6); plot2d(x1',x2',[-3,-1],"000");//undo start circle xset("alufunction",3); x=xsec(1:2,in);//new x x1=x(1);x2=x(2); ln=xsec(4,in);li=xsec(3,in); shortline=linelist(ln);//extension line [sr,sc]=size(shortline); if sc-li>li then, yext=shortline(:,1:li); [yer,yecf]=size(yext);//yec is useful for undoing else, yext=shortline(:,sc:-1:li+1); [yer,yecf]=size(yext); end, end, end,end, end,end, if inflag='off' then,//case where y is not in the frame xset("alufunction",6); plot2d(x1',x2',[-3,-1],"000");//undo start circle xset("alufunction",3); x1=y1;x2=y2; plot2d(x1',x2',[-3,-1],"000");//undo start circle end, if testflag='off' then,//case where x-y does not cross a line xset("alufunction",6); plot2d(x1',x2',[-3,-1],"000");//undo start circle xset("alufunction",3); x1=y1;x2=y2; plot2d(x1',x2',[-3,-1],"000");//undo start circle end, end, if flag='on' then, plot2d([x1;y1],[x2;y2],[1,-1],"000"), line=[yext,[x1;x2],[y1;y2]]; x1=y1;x2=y2; end, //continue line while flag='on', flag='off'; [i_i,y1,y2]=xclick(); //check for a button [br,bc]=size(buttons); hflag='on'; while hflag='on' hflag='off'; for bi=1:br, if buttons(bi,1)<y1 then, if y1<buttons(bi,2) then, if buttons(bi,3)<y2 then, if y2<buttons(bi,4) then, select bnames(bi) case 'help' then,//get help helpme(2); [i_i,y1,y2]=xclick(); hflag='on'; case 'stop' then,//totally undo current line [lr,lc]=size(line); xset("alufunction",6); plot2d(line(1,yecf+1:lc)',line(2,yecf+1:lc)',[1,-1],"000"), xset("alufunction",3); flag='off'; yecl=0; line=0; case 'grill' then,//toggle grill if gopt='on' then, gopt='off'; else, gopt='on'; end, makegrill(nx,nz,gopt); [i_i,y1,y2]=xclick(); hflag='on'; case 'undo' then,//undo line segment [lr,lc]=size(line); xset("alufunction",6); plot2d(line(1,lc-1:lc)',line(2,lc-1:lc)',[1,-1],"000"), xset("alufunction",3); flag='off'; if lc>yecf+2 then, hflag='on'; line=line(:,1:lc-1); x=line(:,lc-1); x1=x(1);x2=x(2); [i_i,y1,y2]=xclick(); flag='on'; end, if flag='off' then, yecl=0; line=0; end, case 'quit' then qt=resume('on') end, end,end, end,end, end, end, if line<>0 then,//line drawing has not been stopped //test if line intersects itself [lr,lc]=size(line); if lc-1>yecf+1 then, [testflag,bav]=testpt([x1;x2],[y1;y2],line(:,yecf+1:lc-1)); else, testflag='off'; end, if testflag='on' then, write(%io(2),' '), write(%io(2),'*********ERROR*********') write(%io(2),' Lines are not allowed'), write(%io(2),'to intersect themselves'), write(%io(2),' '), write(%io(2),' Choose another point'), flag='on'; else, //test if point intersects a previously drawn line yext=[]; flag='on'; xsec=[]; nol=size(linelist); for ln=1:nol, [testflag,bav]=testpt([x1;x2],[y1;y2],linelist(ln)); [br,bc]=size(bav); xsec=[xsec,[bav;ln*ones(1,bc)]]; end, //check all the intersections and choose the shortest [br,bc]=size(xsec); if bc>0 then, flag='off'; btemp=xsec(1:2,:)-[x1;x2]*ones(1,bc); [val,in]=mini([1 1]*(btemp.*btemp)); y1=xsec(1,in);y2=xsec(2,in); //find the extension of the intersected line by the //shortest segment of the intersecting line ln=xsec(4,in);li=xsec(3,in); shortline=linelist(ln); [sr,sc]=size(shortline); if sc-li>li then, yext=shortline(:,li:-1:1); [yer,yecl]=size(yext); else, yext=shortline(:,li+1:sc); [yer,yecl]=size(yext); end, end, //plot line segment plot2d([x1;y1],[x2;y2],[1,-1],"000"), line=[line,[y1;y2],yext]; x1=y1;x2=y2; end, end, end, if yecl<>0 then, yec=[yec,[yecf;yecl]]; end, write(%io(2),'Done With Current Line'), function [flag,bav]=testpt(p1,p2,line) //[flag,bav]=testpt(p1,p2,line) //macro which tests whether the line segment defined by the //two points p1 and p2 intersects any of the line segments //in line. // p1 :2x1 matrix giving the indices of point number one // p2 :2x1 matrix giving the indices of point number two // line :2xN matrix giving the indices of a line // flag :flag='on' indicates an intersection, flag='off' // :indicates no intersection // bav :3xM matrix giving all the intersections found (if any) // :and the position in the line of the intersection // //! // author: C. Bunks date: 12-NOV-90 //set up arguments of fortran subprogram m45.f noi=0; nc=maxi(size(line)); bav=0*ones(3,nc); flag=0; [flag,bav,noi]=fort('testpt',... p1,1,'r',... p2,2,'r',... nc,3,'i',... line,4,'r',... flag,5,'i',... noi,6,'i',... bav,7,'r',... 'sort',... [1,1],5,'i',... [3,nc],7,'r',... [1,1],6,'i'); bav=bav(:,1:noi); if flag=1 then, flag='on'; else, flag='off'; end, function []=redraw(linelist,seedlist,velolist) //[]=redraw(linelist[,seedlist[,velolist]]) //Macro which redraws the lines drawn by velpic //and gives the locations and velocities chosen // linelist :list containing the lines to be drawn // seedlist :list containing the seed positions // velolist :list containing the velocity values // //! // author: C. Bunks date: 12-NOV-90 [lhs,rhs]=argn(0); //determine the number of lines nol=size(linelist); l1=linelist(1); nr=maxi(l1(1,:)); nc=maxi(l1(2,:)); //draw frame plot2d(0,0,[1],"012",' ',[1,1,nr,nc]); //draw the lines (the first line from velpic is the //exterior line) for k=1:nol, lk=linelist(k); plot2d(lk(1,:)',lk(2,:)',[1],"000"), end, if rhs=2 then, plot2d(seedlist(1,:)',seedlist(2,:)',[-3,0],"000"), end, if rhs=3 then, [vr,vc]=size(velolist); toff=.05*maxi([nr,nc])/3; for k=1:vc, text=string(velolist(k)); s1=seedlist(1,k);s2=seedlist(2,k); dess(50)=s1+toff;dess(52)=s2+toff;//positions of text plot2d(s1',s2',[-3,0],"000"); xstring(s1+toff,s2+toff,text,0,0); end, end, function [ind,indexlist]=id_rgn(indexlist,linelist,seed); //[ind,indexlist]=id_region(indexlist,linelist,seed); //Macro which determines all the indices of the matrix of dimension //(nz X nx) which are in the region defined by the seed and the //linelist. The elements which are in the same region as the seed //are those which are on the same side of all the lines in the //linelist. // indexlist :(2xN) vector containing all the indices to be searched // linelist :list of lines // seed :pair of indices of the matrix identifying the region // ind :all indices of the matrix associated to the region // :defined by seed // //! // author: C. Bunks date: 12-NOV-90 nlist=0*indexlist; ic=maxi(size(indexlist)); nol=size(linelist); llist=[];noe=[1]; for k=1:nol, noe=[noe,noe(k)+maxi(size(linelist(k)))]; llist=[llist,linelist(k)]; end, nolt=maxi(size(llist)); noi=0;non=0;bav=0*ones(3,nolt); lln=0*ones(2,nolt); ind=0*indexlist; [ind,nlist,noi,non]=fort('id_rgn',... indexlist,1,'i',... llist,2,'r',... seed,3,'r',... ind,4,'i',... nol,5,'i',... nolt,6,'i',... ic,7,'i',... noi,8,'i',... noe,9,'i',... nlist,10,'i',... bav,11,'r',... lln,12,'r',... non,13,'i',... 'sort',... [2,ic],4,'i',... [2,ic],10,'i',... [1,1],8,'i',... [1,1],13,'i'); ind=ind(:,1:noi); indexlist=nlist(:,1:non); function []=makegrill(nx,nz,gopt) //Plot a grill in the region [1 nx] x [1 nz] // nx :Number of x positions // nz :Number of z positions // gopt :Plotting flag where 'on' means plot // :and 'off means unplot // //! // author: C. Bunks date: 12-NOV-90 // Change JPC 2 mars 1992 // dess; if gopt <>'on' then,xset("alufunction",6);end for k=2:nx-1, plot2d([k;k],[1;nz],[2],"000"), end, for k=2:nz-1, plot2d([1;nx],[k;k],[2],"000"), end xset("alufunction",3); function [vi]=velcalc(indexlist,seedlist,velolist) //Create velocity field for a region defined by indexlist //where velocity varies linearly between control points //defined by the seedlist sl and its associated velocities //in vl. // indexlist :list of indices of region // seedlist :indices of velocity seed locations // velolist :velocity control points // vi :velocities for region // //! // author: C. Bunks date: 12-NOV-90 [vr,vc]=size(velolist); [ir,ic]=size(indexlist); vi=velolist(1)*ones(1,ic); for k=1:vc-1, s1=seedlist(1:2,k);s2=seedlist(1:2,k+1); v1=velolist(k);v2=velolist(k+1); x=indexlist(1,:);y=indexlist(2,:); x1=s1(1);y1=s1(2); x2=s2(1);y2=s2(2); dx=x2-x1;dy=y2-y1;dv=v2-v1; r2=dx*dx+dy*dy; xv=x-x1*ones(x); yv=y-y1*ones(y); gr=(xv*dx+yv*dy)/r2; vi=vi+mini(maxi(gr,0*gr),ones(gr))*dv; end,
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//Exa 4.17 clc; clear; close; format('v',7); //Given Data : m=1;//Kg p1=1;//bar T1=290;//K p2=30;//bar T2=290;//K n=1.3;//constant R=300;//Nm/KgK Cv=0.72;//KJ/KgK disp("part (a) Isothermally") V1=R*T1/p1/10^5;//m^3/Kg V2=p1*V1/p2;//m^3/Kg w=p1*10^5*V1*log(V2/V1)/1000;//KJ/Kg disp(w,"Workdone in KJ/Kg : "); deltaU=m*Cv*(T2-T1);//KJ(as T1=T2) disp(deltaU,"Change in internal energy in KJ : "); q=w+deltaU;//KJ/Kg disp(q,"Heat transfer in KJ/Kg : "); S2subS1=m*R/1000*log(V2/V1)+m*Cv*log(T2/T1);//KJ/KgK disp(S2subS1,"Change in entropy in KJ/KgK : "); disp("part (b) Polytropically") T2=T1*(p2/p1)^((n-1)/n);//K disp(T2,"Temperature T2 in K : "); V1=R*T1/p1/10^5;//m^3/Kg V2=(p1/p2)^(1/n)*V1;//m^3/Kg w= m*R/1000*(T1-T2)/(n-1);;//KJ/Kg disp(w,"Workdone in KJ/Kg : "); deltaU=m*Cv*(T2-T1);//KJ(as T1=T2) q=w+deltaU;//KJ/Kg disp(q,"Heat transfer in KJ/Kg : "); S2subS1=m*R/1000*log(V2/V1)+m*Cv*log(T2/T1);//KJ/KgK disp(S2subS1,"Change in entropy in KJ/KgK : ");
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-- SPPRT13SP.TST -- -- Grant of Unlimited Rights -- -- Under contracts F33600-87-D-0337, F33600-84-D-0280, MDA903-79-C-0687, -- F08630-91-C-0015, and DCA100-97-D-0025, the U.S. Government obtained -- unlimited rights in the software and documentation contained herein. -- Unlimited rights are defined in DFAR 252.227-7013(a)(19). By making -- this public release, the Government intends to confer upon all -- recipients unlimited rights equal to those held by the Government. -- These rights include rights to use, duplicate, release or disclose the -- released technical data and computer software in whole or in part, in -- any manner and for any purpose whatsoever, and to have or permit others -- to do so. -- -- DISCLAIMER -- -- ALL MATERIALS OR INFORMATION HEREIN RELEASED, MADE AVAILABLE OR -- DISCLOSED ARE AS IS. THE GOVERNMENT MAKES NO EXPRESS OR IMPLIED -- WARRANTY AS TO ANY MATTER WHATSOEVER, INCLUDING THE CONDITIONS OF THE -- SOFTWARE, DOCUMENTATION OR OTHER INFORMATION RELEASED, MADE AVAILABLE -- OR DISCLOSED, OR THE OWNERSHIP, MERCHANTABILITY, OR FITNESS FOR A -- PARTICULAR PURPOSE OF SAID MATERIAL. --* -- -- SPECIFICATION FOR PACKAGE SPPRT13 -- PURPOSE: -- THIS PACKAGE CONTAINS CONSTANTS OF TYPE SYSTEM.ADDRESS. -- THESE CONSTANTS ARE USED BY SELECTED CHAPTER 13 TESTS, -- BY PARTS OF THE AVAT SYSTEM, AND BY ISOLATED TESTS FOR -- OTHER CHAPTERS. -- MACRO SUBSTITUTIONS: -- $VARIABLE_ADDRESS, $VARIABLE_ADDRESS1, AND $VARIABLE_ADDRESS2 ARE -- EXPRESSIONS YIELDING LEGAL ADDRESSES FOR VARIABLES FOR THIS -- IMPLEMENTATION. -- $ENTRY_ADDRESS, $ENTRY_ADDRESS1, AND $ENTRY_ADDRESS2 ARE -- EXPRESSIONS YIELDING LEGAL ADDRESSES FOR TASK ENTRIES -- (I.E., FOR INTERRUPTS) FOR THIS IMPLEMENTATION. -- IF NO EXPRESSIONS CAN BE GIVEN THAT ARE SATISFACTORY FOR THE -- VALUES OF THESE CONSTANTS, THEN DECLARE SUITABLE FUNCTIONS -- IN THE SPECIFICATION OF PACKAGE FCNDECL, CREATE A PACKAGE BODY -- CONTAINING BODIES FOR THE FUNCTIONS, AND REPLACE THE MACROS WITH -- APPROPRIATE FUNCTION CALLS. WITH FCNDECL; USE FCNDECL; WITH SYSTEM; PACKAGE SPPRT13 IS VARIABLE_ADDRESS : CONSTANT SYSTEM.ADDRESS := $VARIABLE_ADDRESS; VARIABLE_ADDRESS1 : CONSTANT SYSTEM.ADDRESS := $VARIABLE_ADDRESS1; VARIABLE_ADDRESS2 : CONSTANT SYSTEM.ADDRESS := $VARIABLE_ADDRESS2; ENTRY_ADDRESS : CONSTANT SYSTEM.ADDRESS := $ENTRY_ADDRESS; ENTRY_ADDRESS1 : CONSTANT SYSTEM.ADDRESS := $ENTRY_ADDRESS1; ENTRY_ADDRESS2 : CONSTANT SYSTEM.ADDRESS := $ENTRY_ADDRESS2; END SPPRT13;
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function [newImg] = sousEchant(img,n) s = size(img); newLenX = s(1)/n; newLenY = s(2)/n; newImg = zeros(newLenX,newLenY); for raw=1:newLenY for col=1:newLenX for c=1:s(3) newImg(col,raw,c) = img(col*n,raw*n,c); end; end; end; endfunction; function [newImg] = surEchant(img,n) s = size(img); lenX = s(1); lenY = s(2); newImg = zeros(lenX * n,lenY * n, 3); for raw=1:lenY for col=1:lenX for c=1:s(3) for i=0:(n-1) for j=0:(n-1) x = ((col*n)-1) + i; y = ((raw*n)-1) + j; newImg(x, y, c) end; end; end; end; end; endfunction; function [quant] = quantification(img, m) maxVal = max(img); minVal = min(img); quant = ((maxVal - minVal) / m) / (maxVal - minVal); endfunction; function [newImg] = quantificationImage(img, composante, nbBit) m = 2^nbBit; pas = quantification(im, m); im2double(im); for i=1:m end; endfunction function [periode] = calcPeriode(img, vmin, vmax) moy = vmax - vmin / 2; i = find(img(:, 1, 1) == moy); periode = size(img(:, 1, 1)) / size(i); endfunction;
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clc //initialisation of variables m= 1.008 //gms m1= 36.98 //gms N= 6*10^23 //molecules r= 1.275*10^-8 //cm //CALCULATIONS u= m*m1/(N*(m+m1)) I= u*r^2 //RESULTS printf (' reduced mass = %.2e g',u) printf (' \n moment of inertia = %.2e g cm^2',I)
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//Ex 2.9.9 clc;clear;close; format('v',8); //Given : Vs=5;//Volt Eta=1;//constant VT=26/1000;//V //I=I0 so exp(V1/Eta/VT)-1=1 V1=log(1+1)*Eta*VT;//Volt V2=Vs-V1;//volt disp(V1,"Voltage across diode D1 in V : "); disp(V2,"Voltage across diode D2 in V : ");
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//pagenumber 114 example 19 clear na=10*22;//atoms per cubic metre nd=1.2*10^21;//donor per cubic metre voltag=1.38*10^-23*(273+298)/(1.6*10^-19);//correction in the book voltag=0.026; ni=1.5*10^16; ni=ni^2; v1=voltag*log((na*nd)/(ni)); disp("thermal voltage = "+string((voltag))+"volt"); disp("barrier voltage = "+string(abs(v1))+"volt");//correction in the book
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clc; //Example 21.16 //page no 291 printf("Example 21.16 page no 291\n\n"); //water flows in a concrete pipe v_p=0.02// flow velocity,m/s D_p=1.5//diameter of pipe L_p=20//length of pipe,m rho_p=1000//density of water,kg/m^3 meu_p=0.001//viscosity of water,kg/m.s K_p=0.003//roughnes factor,m //this prototype is to be modeled in a lab using a 1/3o th scale pipe D_m=D_p/30//D_m is diameter of modeled pipe L_m=L_p*(D_m/D_p)//length of modeled pipe K_m=K_p*(D_m/D_p)//roughness factor for modeled pipe //the fluid in the model is caster oil rho_m=961.3//densiy of oil, kg/m^3 meu_m=0.0721//viscosity of oil,kg/m.s //since R_e = (rho_m*v_m*D_m)/meu_m = (rho_p*v_p*D_p)/meu_p v_m = (rho_p*v_p*D_p*meu_m)/(rho_m*D_m*meu_p)// flow velcity in molded pipe printf("\n flow velocity v_m=%f m/s",v_m); //pressure drop in prototype P_drop_m=1e+5//pressure drop in model P_drop_p=(P_drop_m*rho_p*(v_p)^2)/(rho_m*(v_m)^2)//pressure drop in prototype printf("\n pressure drop in prototype P_drop_p=%f Pa",P_drop_p);
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clc A=0.12; //m^2 T=800; //K a=5.67*10^(-8); disp("(i) The total rate of energy emission =") Eb=a*A*T^4; disp(Eb) disp("W") disp("(ii) The intensity of normal radiation =") Ibn=a*T^4/%pi; disp(Ibn) disp("W/m^2.sr") disp("(iii) The wavelength of maximum monochromatic emissive power =") wavelength=2898/T; disp(wavelength) disp("μm")
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//chapter 18 //example 18.1 //page 559 clear all; clc ; //given Rl=15;//load resistance ep=30;//peak ip voltage Rg=1;//gate resistance kohm //forward blocking voltage VfXm>30 for SCR to remain in off until triggered VAK=1; Ip=(ep-VAK)/Rl; //rms value of Il Irms=0.5*Ip; printf("\nIrms=%.2f A and ep=%d V",Irms,ep); printf("\nC6F is suiatable SCR with VFXM=50 V,current range allowable is 1.6 A"); //from chart Vg=0.5;//Trigger voltage Ig=0.025//mA Irg=Vg/Rg; It=Ig+Irg;//trigger current printf("\nTrigger voltage=%.1f V and trigger current=%.3f mA",Vg,It); Ih=1; Il=Ih; ei=VAK+1000*Il*Rl; ei=1; printf("\nei=%d V\nSCR will switch off when ei falls below 1 V",ei);
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//2D plots x=[-1:.1:1]; y=x.^2; figure; plot(x,y,'-*'); xlabel('domain');ylabel('range'); title('Square function(plot)') xs2pdf(0,'plotfunction.pdf') figure; plot2d(x,y); xlabel('domain');ylabel('range'); title('Square function(plot2d)') xs2pdf(1,'plot2dfunction.pdf') figure; plot2d3(x,y);xlabel('domain');ylabel('range'); title('Square function(plot2d3)') xs2pdf(2,'plot2d3function.pdf')
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//Chapter-5,Example 5_2,Page 5-23 clc() //Given Values: m=1 //mass of given particle in kg h=6.63*10^-34 //Planck's constant v=1*10^3 //velocity of particle //Calculations: lam=h/(m*v) //de Broglie wavelength printf('de Broglie wavelength associated with particle is =%.40f m \n \n',lam) printf(' This wavelength is too small for any practical significance.')
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clear; clc; // Illustration 8.4 // Page: 484 printf('Illustration 8.4 - Page: 484\n\n'); // Solution // a - water vapor b - air //*****Data***** T_G1 = 356; // [K] P_total = 101.325; // [kPa] Y_1 = .03; // [kg water/kg dry air] //*****// C_pa = 1.884; // [kJ/kg.K] C_pb = 1.005; // [kJ/kg.K] C_s1 = C_pb + Y_1*C_pa;// [kJ/kg.K] T_1 = 373.15; // [K] T_c = 647.1; // [K] M_a = 18.02; // [gram/mole] M_b = 28.97; // [gram/mole] lambda_1 = 2256; // [Latent Heat of Vaporizarion at T_1, kJ/kg] // Using equation 8.10 // T_as = T_G1- (Y_as - Y_l)*lambda_as/C_s1 // where lambda_2 = lambda_1*((1-T_as/T_c)/(1-T_1/T_c))^.38 // Y_as = P_a/(P_total-P_a)*M_a/M_b // and P_a = exp(16.3872-(3885.7/(T_as-42.98))) - Antoine equation for component 'a' deff('[y] = f12(T_as)',' y = T_as - T_G1 + ((exp(16.3872 - (3885.7/(T_as - 42.98)))/(P_total - (exp(16.3872 - (3885.7/(T_as - 42.98))))))*(M_a/M_b) - Y_1)*(lambda_1*((1-T_as/T_c)/(1-T_1/T_c))^.38/C_s1)'); T_as = fsolve(310,f12); // [K] printf("Adiabatic Saturation Temperature is %f K\n",T_as); // Now using equation 8.2 P_a = exp(16.3872-(3885.7/(T_as-42.98))); // [kPa] Y_as = P_a/(P_total-P_a)*M_a/M_b; // [kg water/kg dry air] printf("Absolute humidity is %f kg water/kg dry air\n",Y_as);
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//Ex2_7 Pg-88 clc disp("Relaxation time in terms of mobility is given by") disp(" t=m*u/e") printf("\n\n Taking effective mass of electron an holes in consideration,\n relaxation time is given by \n") disp(" t=m_star*u/e") disp("(a) foe electrons,m_star = 0.259*m_0") m0=9.1*10^(-31) ue=0.135 //mobility of electrons e=1.6*10^(-19) //electron charge t_e=(0.259*m0*ue)/e printf("\n Average relaxation time of eletrons = %.2f*1e-13 secs\n ",t_e*1e13) uh=0.048 //mobility of holes disp("(b) For holes in the valance band,m=0.537*m_0") t_h=(0.537*m0*uh)/e printf("\n Average relaxation time of eletrons = %.2f*1e-13 secs\n ",t_h*1e13)
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// Electric Machinery and Transformers // Irving L kosow // Prentice Hall of India // 2nd editiom // Chapter 1: Electromechanical Fundamentals // Example 1-10 clear; clc; close; // Clear the work space and console. // Given data no_of_coils = 40; N = 20; // no of turns in each coil omega = 200; // angular velocity of armature in rad/s phi = 5 * 10 ^ -3; // flux per pole a = 4; // No. of parallel paths P = 4; // No. of poles // Calculations Z = no_of_coils * 2 * N; // No. of conductors E_g = ( phi * Z * omega * P ) / ( 2 * %pi * a ); // Voltage generated by the // armature between brushes // Display the results disp("Example 1-10 Solution : "); printf("\n Z = % d conductors ", Z); printf("\n Eg = % .2f V between the brushes ", E_g);
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clc; clear; mprintf('MACHINE DESIGN \n Timothy H. Wentzell, P.E. \n EXAMPLE-3.6 Page No.55\n'); L=60; //[in] Length of column Sy=36000; //[lb/in^2] Yield strength SF=2; //[]Safty factor E=30*10^6; //[lb/in^2] Modulus of elasticity A=2.26; //[in^2] Area of cross section (Appendix 5.4) I=0.764; //[in^4] Moment of inertia (Appendix 5.4) r=sqrt(I/A); //[in] Radius of gyration K=0.65; //[] End support condition factor from Figure 3.8 Le=K*L; //[in] Effective length mprintf('\n The effective length is %f in.',Le); SR=Le/r; //[] Slenderness ratio mprintf('\n The slenderness ratio is %f.',SR); Cc=sqrt(2*%pi^2*E/Sy); //[] Column constant mprintf('\n The column constant is %f.',Cc); if Cc>SR then mprintf('\n The column constant is greater than slenderness ratio, so use the Johnson formula.'); end F=(A*Sy/SF)*(1-Sy*SR^2/(4*%pi^2*E)); mprintf('\n The acceptable load for a safty factor of 2 is %f lb.',F);
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//Ex4_17 // Image Smoothing with a Butterworth LowPass Filter // Version : Scilab 5.4.1 // Operating System : Window-xp, Window-7 //Toolbox: Image Processing Design 8.3.1-1 //Toolbox: SIVP 0.5.3.1-2 //Reference book name : Digital Image Processing //book author: Rafael C. Gonzalez and Richard E. Woods clc; close; clear; xdel(winsid())//to close all currently open figure(s). function[H]=lowpassfilter(type1,M,N,D0,n)//lowpassfilter is used to filter an image . u=0:(M-1); v=0:(N-1); idx=find(u>M/2); u(idx)=u(idx)-M; idy=find(v>N/2); v(idy)=v(idy)-N; [U,V]=meshgrid(v,u); D=sqrt(U.^2+V.^2); select type1 case'butterworth'then if argn(2)==4 then n=1; end H = ones(M,N)./(1+(D./D0).^(2*n)); else disp('Unknownfiltertype.') end endfunction /////////////////////////////////// Main Programm //////////////////////////////// a=imread("Ex4_17.tif"); //gray=rgb2gray(a); gray=im2double(a); figure,ShowImage(gray,'Gray Image'); title('Original Image','color','blue','fontsize',4); [M,N]=size(gray); h=fft2(gray);//fft2() is used to find 2-Dimensional Fast Fourier Transform of an matrix i=log(1+abs(h)); in=fftshift(i);//fftshift() is used to rearrange the fft output, moving the zero frequency to the center of the spectrum. inm=mat2gray(in) figure,ShowImage(inm,'Frequency Spectrum'); title('Frequency Spectrum','color','blue','fontsize',4); /////////////////////////// Filtering With Cut-off Frequency 10 /////////////////////// filt=lowpassfilter('butterworth',M,N,10); // Function which generate Filter Mask Corresponding to Low Frequency //filt_shift=fftshift(filt); //figure,ShowImage(filt_shift,'Filter Mask'); //title('Filter Mask to Specific Cut-Off Frequency'); n=filt.*h;//Multiply the Original Spectrum with the Filter Mask. Image_filter=real(ifft(n)); Image_filter=mat2gray(Image_filter) figure,ShowImage(Image_filter,'Filtered Image'); title('Filtered Image with Cut-Off Frequency 10','color','blue','fontsize',4); /////////////////////////// Filtering With Cut-off Frequency 30 /////////////////////// filt=lowpassfilter('butterworth',M,N,30); // Function which generate Filter Mask Corresponding to Low Frequency //filt_shift=fftshift(filt); //figure,ShowImage(filt_shift,'Filter Mask'); //title('Filter Mask to Specific Cut-Off Frequency'); n=filt.*h;//Multiply the Original Spectrum with the Filter Mask. Image_filter=real(ifft(n)); Image_filter=mat2gray(Image_filter) figure,ShowImage(Image_filter,'Filtered Image'); title('Filtered Image with Cut-Off Frequency 30','color','blue','fontsize',4); /////////////////////////// Filtering With Cut-off Frequency 60 /////////////////////// filt=lowpassfilter('butterworth',M,N,60); // Function which generate Filter Mask Corresponding to Low Frequency //filt_shift=fftshift(filt); //figure,ShowImage(filt_shift,'Filter Mask'); //title('Filter Mask to Specific Cut-Off Frequency'); n=filt.*h;//Multiply the Original Spectrum with the Filter Mask. Image_filter=real(ifft(n)); Image_filter=mat2gray(Image_filter) figure,ShowImage(Image_filter,'Filtered Image'); title('Filtered Image with Cut-Off Frequency 60','color','blue','fontsize',4); /////////////////////////// Filtering With Cut-off Frequency 160 /////////////////////// filt=lowpassfilter('butterworth',M,N,160); // Function which generate Filter Mask Corresponding to Low Frequency //filt_shift=fftshift(filt); //figure,ShowImage(filt_shift,'Filter Mask'); //title('Filter Mask to Specific Cut-Off Frequency'); n=filt.*h;//Multiply the Original Spectrum with the Filter Mask. Image_filter=real(ifft(n)); Image_filter=mat2gray(Image_filter) figure,ShowImage(Image_filter,'Filtered Image'); title('Filtered Image with Cut-Off Frequency 160','color','blue','fontsize',4); /////////////////////////// Filtering With Cut-off Frequency 460 /////////////////////// filt=lowpassfilter('butterworth',M,N,460); // Function which generate Filter Mask Corresponding to Low Frequency //filt_shift=fftshift(filt); //figure,ShowImage(filt_shift,'Filter Mask'); //title('Filter Mask to Specific Cut-Off Frequency'); n=filt.*h;//Multiply the Original Spectrum with the Filter Mask. Image_filter=real(ifft(n)); Image_filter=mat2gray(Image_filter) figure,ShowImage(Image_filter,'Filtered Image'); title('Filtered Image with Cut-Off Frequency 460','color','blue','fontsize',4);
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clc; clear; h=6.63*10^-34 //Plancks constant in J-s K_b=1.38*10^-23 //Boltzmanns constant in m^2 kg s^-2 K^-1 T=300 //Temperature in K m=1.00878*1.66*10^-27 //mass of neutron in kg //calculation lambda=(h/sqrt(3*m*K_b*T)) mprintf("The de-Broglie wavelength is = %1.2e m or 0.145 nm",lambda)
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clc; x=[-1,2,-1,5,6]; y=[3,1,4,2,3]; px=1; //////////////////// xy=0; tx=0; ty=0; x2=0; n=length(x); for(i=1:n) xy =xy+(x(i)*y(i)); tx=tx+(x(i)); ty=ty+(y(i)); x2=x2+(x(i)^2); // printf("%.5f",x(i)); end a=((n*xy)-(tx*ty))/((n*x2)-(tx*tx)); b=((ty*x2)-(tx*xy))/((n*x2)-(tx*tx)); printf("%.5f\n",a); printf("%.5f\n",b); f=(a*px)+b printf("%.5f\n",f); /* printf("%.5f\n",xy); printf("%.5f\n",tx); printf("%.5f\n",ty); printf("%.5f\n",x2); printf("%.5f\n",n); */
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//Calculation of orifice diameter clc,clear //Given: bp=15 //Brake power per cylinder in kW N=2000 //Engine speed in rpm bsfc=0.272 //Brake specific fuel consumption in kg/kWh API=32 //American Petroleum Institute specific gravity in degreeAPI theta_i=30 //Period of injection in degrees P_i=120 //Fuel injection pressure in bar P_c=30 //Combustion chamber pressure in bar Cd=0.9 //Coefficient of discharge for the injector function rho=specificgravity(API),rho=141.5/(131.5+API),endfunction //Specific gravity(rho) as a function of API //Solution: s=specificgravity(API) //Specific gravity of fuel m_f=bsfc*bp*2/(N*60) //Fuel consumption in kg t=theta_i/360*60/N //Time for injection in s m_f=m_f/t //Fuel consumption per cycle in kg/s A_f=m_f/(Cd*sqrt(2*s*1000*(P_i-P_c)*10^5)) //Orifice area of fuel injector in m^2 A_f=A_f*10^6 //Orifice area of fuel injector in mm^2 d_f=sqrt(4*A_f/%pi) //Diameter of fuel orifice in mm //Results: printf("\n The diameter of the fuel orifice, d = %.2f mm\n\n",d_f)
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// Aim:To find the discharge flow and pressure // Given: // high inlet flow-rate: Q_high_inlet=20; //gpm // low inlet pressure: p_low_inlet=500; //psi // Ratio of piston area to rod area: Ratio=5/1;
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function M1=%hm_s(M1) // Copyright INRIA // hypermatrix sign change M1('entries')=-M1('entries')
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clc //solution //given P=45000//N//load applied A1=45*20//mm^2//area of cross section at link A-A //stress in section A-A f1=P/A1//(N/mm^2) printf("the stress in section A-A is ,%f N/mm^2\n",f1) //stress in section B-B A2=20*(75-40)//mm^2//area of cross section at link B-B f2=P/A2//(N/mm^2) printf("the stress in B-B section ,%f N/mm^2",f2)
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function []=bb_bode(sl,fmin,fmax,pas,comments) //! // Copyright INRIA // Modified by Roberto Bucher to obtain frequencies in rad/s [lhs,rhs]=argn(0); dom='c'; //xset('default'); //--------------------- nyq_frq=[];l10=log(10); pas_def='auto' // default ilf=0 typ=type(sl) //-compat next line added for list/tlist compatibility if typ==15 then typ=16,end select typ case 16 then // sl,fmin,fmax [,pas] [,comments] typ=sl(1);typ=typ(1); if typ<>'lss'&typ<>'r' then error(97,1) end if typ=='lss' then if sl(7)==[] then error('Undefined time domain (sl(7))');end end if typ=='r' then if sl(4)==[] then error('Undefined time domain (sl(4))');end end dom=sl('dt') if dom==[]|dom==0 then error(96,1),end if dom=='d' then dom=1;end select rhs case 1 then //sl comments=' ' fmin_default=1.d-3; fmax_default=1.d3; if dom=='c' then fmax_default=1.d3; else fmax_default=1/(2*dom),end [frq,repf]=repfreq(sl,fmin_default,fmax_default); [d,phi]=dbphi(repf); sl=[] case 2 then // sl,frq comments=' ' if min(fmin)<=0 then error('bode: requires strictly positive frequency vector') end [frq,repf]=repfreq(sl,fmin); [d,phi]=dbphi(repf); fmin=[];sl=[] case 3 , //sl,frq,comments ou sl,fmin,fmax if type(fmax)==1 then comments=' ' if fmin<=0 then error('bode: requires strictly positive frequency range') end [frq,repf]=repfreq(sl,fmin,fmax,pas_def),sl=[] [d,phi]=dbphi(repf); else comments=fmax if min(fmin)<=0 then error('bode: requires strictly positive frequency vector') end if type(dom)==1 then nyq_frq=1/2/dom;end if find(fmin>nyq_frq)~=[] then warning('There are frequencies beyond Nyquist f!'); end [frq,repf]=repfreq(sl,fmin);fmin=[];sl=[] [d,phi]=dbphi(repf); end case 4 , if type(pas)==1 then comments=' ', else comments=pas;pas=pas_def; end, if min(fmin)<=0 then error('bode: requires strictly positive frequency vector') end [frq,repf]=repfreq(sl,fmin,fmax,pas) [d,phi]=dbphi(repf); case 5 then, if min(fmin)<=0 then error('bode: requires strictly positive frequency vector') end [frq,repf]=repfreq(sl,fmin,fmax,pas) [d,phi]=dbphi(repf); else error('Invalid call: sys,fmin,fmax [,pas] [,com]') end; case 1 then //frq,db,phi [,comments] ou frq, repf [,comments] select rhs case 2 , //frq,repf comments=' ' [phi,d]=phasemag(fmin);fmin=[] case 3 then if type(fmax)==1 then comments=' '//frq db phi d=fmin,fmin=[] phi=fmax,fmax=[] else [phi,d]=phasemag(fmin);fmin=[] comments=fmax end; case 4 then comments=pas;d=fmin;fmin=[];phi=fmax;fmax=[] else error('Invalid call: frq,db,phi,[com] or frq,repf,[com]') end; frq=sl;sl=[];[mn,n]=size(frq); if min(frq)<=0 then error('bode: requires strictly positive frequencies') end if mn<>1 then ilf=1;//un vecteur de frequences par reponse else ilf=0;//un seul vecteur de frequence end; else error('Bode: invalid call') end; [mn,n]=size(phi) // //Captions if comments==' ' then comments(mn)=' '; mnc=0 hx=0.48 else mnc=mn hx=0.43 end; [wrect,frect]=xgetech(); //magnitude xsetech(wrect=[wrect(1)+0,wrect(2)+0,wrect(3)*1.0,wrect(4)*hx*0.95]); frq=2*%pi*frq; rect=[mini(frq),mini(d),maxi(frq),maxi(d)] // just to fix the scales for xgrid plot2d1("oln",mini(frq),mini(d),0,"051"," ",rect); // xgrid first xgrid(4); // now the curves plot2d1("oln",frq',d',[1:mn],"000"," ",rect); if type(dom)==1 then [xx1,xx2]=xgetech(); val= xx2([2;4])'; plot2d1("oln",max(frq)*[1;1],val,5,"000"," ",rect); end xtitle('Magnitude ',' rad/s','db'); //phase xsetech(wrect=[wrect(1)+0,wrect(2)+wrect(4)*hx,wrect(3)*1.0,wrect(4)*hx*0.95]); rect=[mini(frq),mini(phi),maxi(frq),maxi(phi)] // just to fix the scales for xgrid plot2d1("oln",mini(frq),mini(phi),0,"051"," ",rect); xgrid(4); // now the curves plot2d1("oln",frq',phi',[1:mn],"000"); if type(dom)==1 then [xx1,xx2]=xgetech(); val= xx2([2;4])'; plot2d1("oln",max(frq)*[1;1],val,5,"000"); end xtitle('Phase ',' rad/s','degrees'); if mnc>0 then xsetech([wrect(1)+0,wrect(2)+wrect(4)*2*hx,wrect(3)*1.0,wrect(4)*0.1],[0 0 1 1]); dash=xget('dashes') y0=0.7;dy=-1/2 x0=0;dx=1/2 count=0 for k=1:mnc xset('dashes',k) xsegs([x0;x0+0.08],[y0;y0]) rect=xstringl(x0+0.1,y0,comments(k)) xset('dashes',dash(1)); xstring(x0+0.1,y0-rect(4)/3,comments(k)) count=count+1 y0=y0+dy if count==3 then x0=x0+dx;y0=0.7,end end xset('dashes',dash(1)) end xsetech(wrect,frect); endfunction
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clear clf() for J = 1:3 for I = 1:3 perdants = [] gagnants = [] M1σ = 2950+I*250 M2σ = 2950+J*250 exec('C:\Users\Julien Guégan\Documents\Cours\MAM4\STAGE\2 cohorts\Tfini\PIP - Tfini.sce',-1) subplot(3,3,(I-1)*3+J) //Mσ = 3000:3800 //plot(Mσ,Mσ,'k') plot(perdants,gagnants,'r.') plot(gagnants,perdants,'b.') // contour(Mσ,Mσ,s,[0.99,0.999,1,1.001,1.01]) end end
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//Page Number: //Example 2.10 clc; //Given, c=3D+8; //m/s a=3; //cm a1=a/100; //m b=2; //cm b1=b/100; //m f=7.5D+9; //HZ p=5D+3; //W mu=%pi*4D-7; w=2*%pi*f; bet=sqrt(((w/c)^2)-((%pi/a1)^2)); //Charecteristic impedance z0=w*mu*2*b/(bet*a); disp('ohm',z0,'Charecteristic impedance:'); //Peak electric field e0=4*w*mu*p/(bet*a*b); disp('V/m',e0,'Peak electric field:'); //Maximum voltage v0=e0*b1; disp('kV',v0/1000,'Maximum voltage:'); //Answer for v0 is given as 3.172 kV it should be 33.71 kV
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// Exa 10.4 clc; clear; close; // Given data V_H = 10;// in V V_L = -10;// in V I_max = 100;// in µA I_max = I_max * 10^-6;// in A V_HV = 0.1;// in V V_sat = 10;// in V R2 = 1;// in k ohm R1 = 199;// in k ohm R = (R1*R2)/(R1+R2);// in k ohm disp(R*10^3,"The resistance in Ω is"); // Note: The unit of the answer in the book is wrong
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// Exa 2.13 clc; clear; close; // Given data AR= 100;// true value of resistance in ohm AI= 2;// true value of current in amp R= 0.2;// uncertainties in resistance in ohm I= 0.01;// uncertainties in current in amp PLR= R/AR*100;// percentage limiting error to resistance PLC= I/AI*100;// percentage limiting error to current P=AI^2*AR;// in watt LE_P= 2*PLC+PLR;// limiting error in the power dissipation disp("Power dissipation") disp(string(P-P*LE_P/100)+" to "+string(P+P*LE_P/100))
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//Example 1.14<i> //Find whether the following signal is periodic or not clc; n=-10:10; x=cos(2*%pi*n); subplot(321) plot2d(n,x); f=(2*%pi)/(2*%pi);//where f is the no of cycles/sample. N=1/f;//where N is the no of samples per cycle. disp('samples',N,'(a)The given signal is periodic'); //Example 1.14<ii> //Find whether the following signal is periodic or not. clc; n=-20:20; x=exp(%i*6*%pi*n); subplot(322) plot2d3(n,x); f=(6*%pi)/(2*%pi);//where f is the no of cycles per sample. N=1/f;//where N is the no of samples per cycle. disp('samples',N,'(b)the given signal is periodic'); //example 1.14<1v> //Find whether the given signal is periodic or not clc; n=-30:30; x=exp(%i*(2*%pi/3)*n)+exp(%i*(3*%pi/4)*n); subplot(323) plot2d3(n,x); disp('(c)The given signal is periodic'); //Example 1.14<v> //Find whether the given signal is periodic or not; clc; n=-20:20; x=exp(%i*(3*%pi/5)*(n+1/2)); subplot(324) plot(n,x); f=(3*%pi/5)/(2*%pi);//where f is the no of cycles per sample. N=1/f;//where n is the no of samples per cycle. disp('samples',N,'(d)the given signal is periodic'); //Example1.14<vi> //whether the given signal is periodic or not clc; n=-40:40; x=12*cos(20*n); subplot(325) plot(n,x); f=20/(2*%pi);//where f is the no of cycles per sample N=1/f;//where n is the no of sample per cycle disp('samples',N,'(e)the given signal is not peridic'); disp('In the figure we have the plots of part (a) - (d) in clockwise order strating from the top left');
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//Example 1.15d //Check whether the given signal is periodic or not clc; t=-10:0.01:10; y=(cos(t))^2; plot(t,y); disp('Plot shows that the given signal is periodic with period %pi');
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//Author: Varun Bhatt // //This function generates head phantom image that can be used to test numerical accuracy of //2D reconstruction algorithms. P generally contains one large ellipse and several smaller //ellipses of different intensities. // //Input parameters: //def - Specifies the default phantom ("shepp-logan" or "modified shepp-logan") to be used. //n - A number specifying rows and columns of the image (256x256 by default) //E - Custom ellipses that should be used to generate phantom. // It should have 6 columns corresponding to intensity, semi major and semi minor axis, // x, y offset and rotation angle. // //Output: //p - The generated phantom image //ellipse - Ellipses used to generate the phantom. // //Examples: //Modified shepp logan of size 256: // // P=phantom(); // imshow(P); // //Shepp logan of size 400: // // P=phantom("shepp-logan",400); // imshow(P); // //Custom ellipse: // // e=[1 0.8 0.6 0 0 0]; // P=phantom(e,256); // imshow(P); // //References: //1) Shepp, Larry; B. F. Logan (1974). "The Fourier Reconstruction of a Head Section". IEEE Transactions on Nuclear Science. NS-21 (3): 21–43. //2) P. A. Toft, "The Radon Transform, Theory and Implementation", p. 201 function [p,ellipse]=phantom(varargin) narg=argn(2); if(narg>2) then error("Invalid input. At most 2 parameters required."); end //Default phantoms (taken from references): // A a b x0 y0 phi // --------------------------------- shepp_logan=[ 1 .69 .92 0 0 0 ; -.98 .6624 .8740 0 -.0184 0 ; -.02 .1100 .3100 .22 0 -18 ; -.02 .1600 .4100 -.22 0 18 ; .01 .2100 .2500 0 .35 0 ; .01 .0460 .0460 0 .1 0 ; .01 .0460 .0460 0 -.1 0 ; .01 .0460 .0230 -.08 -.605 0 ; .01 .0230 .0230 0 -.606 0 ; .01 .0230 .0460 .06 -.605 0 ]; // A a b x0 y0 phi // --------------------------------- modified_shepp_logan = [ 1 .69 .92 0 0 0 ; -.8 .6624 .8740 0 -.0184 0 ; -.2 .1100 .3100 .22 0 -18 ; -.2 .1600 .4100 -.22 0 18 ; .1 .2100 .2500 0 .35 0 ; .1 .0460 .0460 0 .1 0 ; .1 .0460 .0460 0 -.1 0 ; .1 .0460 .0230 -.08 -.605 0 ; .1 .0230 .0230 0 -.606 0 ; .1 .0230 .0460 .06 -.605 0 ]; ellipse=modified_shepp_logan; //Default phantom if(narg==1) then arg1=varargin(1); if(type(arg1)==10) then //if arg1 is a string convstr(arg1,"l"); if(arg1=="shepp-logan") then ellipse=shepp_logan; elseif(arg1=="modified shepp-logan") then ellipse=modified_shepp_logan; else error("Wrong type of phantom. It should be Shepp-Logan or Modified Shepp-Logan"); end elseif(size(size(arg1),"*")==2) then //if arg1 is 2D matrix if(size(arg1,2)==6) then ellipse=arg1; else error("6 columns should be present in the phantom"); end else error("Invalid first input argument"); end end n=256 //Default n if(narg==2) then arg2=varargin(2); if(isscalar(arg2)) n=arg2; else error("Second parameter should be a scalar.") end end p=zeros(n,n); x_sym=((0:n-1)-(n-1)/2)/((n-1)/2); x_rel=repmat(x_sym,n,1); y_sym=(x_sym').*(-1); y_rel=repmat(y_sym,1,n); for i=1:size(ellipse,1) A=ellipse(i,1); //Intensity addition //a,b of ellipse a=ellipse(i,2); b=ellipse(i,3); //Offset x0=ellipse(i,4); y0=ellipse(i,5); phi=ellipse(i,6)*3.14/180; //Rotation angle x=x_rel-x0; y=y_rel-y0; e=((x.*cos(phi)+y.*sin(phi)).^2)./(a^2) + ((y.*cos(phi)-x.*sin(phi)).^2)./(b^2); //Ellipse equation ind=find(e<=1); p(ind)=p(ind)+A; //Adding intensity to the ellipse end p=p'; endfunction
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disp('chapter 10 ex10.1') disp('given') disp('design a triangular rectanglar signal generator to have 5volt triangular output') disp('frequency ranging from 200Hz to 2kHz and a duty cycle adjustable from 20% to 80%') disp('using bipolar op-amps with a supply of +or-15volt') Vcc=15 Vo=5 f1=200 f2=2000 disp('Schmitt circuit design') disp('I3>IBmax') disp('let I3=50*10^(-6)A and Vf=0.7volt') IBmax=500*10^(-9) I3=50*10^(-6) Vf=0.7 disp('R2=Vosat/I3') R2=(Vcc-1)/I3 disp('ohms',R2) disp('use 270kohm standard value and recalculate I3') R2=270000 disp('I3=Vosat/R2') I3=(Vcc-1)/R2 disp('amperes',I3) disp('R3=UTP/I3') R3=Vo/2/I3 disp('ohms',R3) //use 47kohm and 1kohm disp('integrator circuit') disp('let C1 charging current I1min=50*10^(-6)A') I1min=50*10^(-6) disp('lowest frequency f1,PWmax=80%of Tmax') PWmax=0.80*1/f1 disp('watts',PWmax) disp('C1=I1min*t/v') C1=I1min*PWmax/Vo disp('farads',C1) //standard value disp('R4+R5+R6=(+Vosat-Vf)/I1min') disp('R9=R4+R5+R6') R9=(Vcc-1-Vf)/I1min disp('ohms',R9) disp('If2=I1min*f2/f1') If2=I1min*f2/f1 disp('amperes',If2) disp('R5+R6=(+Vosat-Vf)/If2') disp('R8=R5+R6') R8=(Vcc-1-Vf)/If2 disp('ohms',R8) disp('R4=(R4+R5+R6)-(R5+R6)') R4=R9-R8 disp('ohms',R4) //use 250kohm standard value potentiometer disp('PWmin=20% of Tmax') PWmin=.20*1/f1 disp('watts',PWmin) disp('R6=(R5+R6)*PWmin/PWmax') R6=R8*PWmin/PWmax disp('ohms',R6) disp('use 6.8kohm standard value') R6=6800 disp('R5=(R5+R6)-R6') R5=R8-R6 disp('ohms',R5) //standard value of potentiometer disp('R7=R6=6.8kohm')
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//Fuels and Combustion// //Example 8.15// CR=7.8;//compression ratio for first case// E1=1-(1/CR)^0.258;//Energy efficiency corresponding to CR value 7.8// printf('Efficiency of the engine in the first case=E1=%f',E1); CR=9.5;//compreesion ratio for second case// E2=1-(1/CR)^0.258;//Energy efficiency corresponding to CR value 9.5// printf('\nEfficiency of the engine in the second case=E2=%f',E2); IE=E2-E1;//Increase in efficiency// printf('\nIncrease in efficiency=IE=%f',IE); PIE=IE*100/E2;//percentage of increase in efficiency// printf('\nPercentage of increase in efficiency=PIE=%f',PIE);
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Ex6_2.sce
//Chapter 6,Example 6.2 Page 199 clc clear Cs = 106 // micro F C2 = 0.35 // micro F R2 = 318 // ohms R1 = 130 // ohms w = 314 Cp = Cs*(R2/R1) Rp = R1/(w^2*C2*Cs*10^-12*R2^2) tang = 1/(w*Rp*Cp*10^-6) printf (" Rp = %f ohm \n ",Rp) printf (" Cp = %f μF \n ",Cp) printf (" tan δ = %f \n ",tang) //Answers may vary due to round off error
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Ch05Ex14.sce
// Scilab Code Ex5.14: Page:303 (2011) clc;clear; lambda = 5.9e-007;....// Wavelength of the reflected light, m n = 10;....// Order of the ring D10 = 0.005;....// Diameter of the 10th ring,in m R = (D10^2)/(4*n*lambda); // Radius of curvature of the lens, m printf("\nThe radius of curvature of the lens = %6.4f m", R); t = (D10^2)/(8*R); // Thickness of the corresponding air film, m printf("\nThe thickness of the corresponding air film = %4.2e m",t); // Result // The radius of curvature of the lens = 1.0593 m // The thickness of the corresponding air film = 2.95e-006 m
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clc(); clear; // To calculate the critical current Hc=2*10^3; //critical magnetic field in amp/m R=0.02; //radius in m p=3.14; Ic=2*p*R*Hc; printf("the critical current is %f amp",Ic);