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/Metodos/Clase8/scripts/9MetodoRungeKuttaOrden4.sce
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DavidAlex99/Cursos
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9MetodoRungeKuttaOrden4.sce
clc() clear all clf() function result = solucionAnalitica(t) result = (4/1.3)*(exp(0.8*t)-exp(-0.5*t))+2*exp(-0.5*t) endfunction function result= eqdiff(y,t) result = 4*exp(0.8*t)-0.5*y endfunction function [result,points]=metodoRungeKuttaMedio(stepsize,y0, t0, tf, eqf) points = t0:stepsize:tf result = (length(points)) result(1) = y0 for i=2:1:length(points) ya = result(i-1) k1 = eqf(y0,points(i-1)) k2 = eqf(y0+0.5*k1*stepsize,points(i-1)+0.5*stepsize) result(i) = ya+k2*stepsize end endfunction function result=metodoRungeKuttaCuartoOrden(stepsize,y0, t0, tf, eqf) points = t0:stepsize:tf result = (length(points)) result(1) = y0 for i=2:1:length(points) ya = result(i-1) k1 = eqf(y0,points(i-1)) k2 = eqf(y0+0.5*k1*stepsize,points(i-1)+0.5*stepsize) k3 = eqf(y0+0.5*k2*stepsize,points(i-1)+0.5*stepsize) k4 = eqf(y0+k3*stepsize,points(i-1)+stepsize) result(i) = ya+(1/6)*(k1+2*k2+2*k3+k4)*stepsize end endfunction tf = 4 stepsize = 1 [resultsA, pointsA] = metodoRungeKuttaMedio(stepsize,2,0,tf,eqdiff) resultsB = metodoRungeKuttaCuartoOrden(stepsize,2,0,tf,eqdiff) solAnalitica = (length(pointsA)) for i=1:1:length(pointsA) solAnalitica(i) = solucionAnalitica(points(i)) end plot(pointsA,solAnalitica,"color","blue","marker","-") plot(pointsA,resultsA,"color","red","marker","*") plot(pointsA,resultsB,"color","green","marker",".") legend(['Método analitico';'Método de Runge-Kutta a = 1/2';'Método de Runge-Kutta cuarto orden';],[-1]) xgrid()
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clear;lines(0); A=sprand(10,12,0.1); sp=spones(A) B = A~=0 bool2s(B)
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//chapter_no.-3, page_no.-84 //Example_no.3-1-1 clc; //(a)Calculate_the_line_Characteristic_Impedance R=2; L=8*(10^-9); C=.23*(10^-12); f=1*(10^9); G=.5*(10^-3); w=2*%pi*f; Z0=sqrt((R+(%i*w*L))/(G+(%i*w*C))); x=real(Z0); y=imag(Z0); o=atand(y,x); disp(o,'the_phase_of_Z0_is ='); M=abs(Z0);//magintue_of_Z0 disp(M,'the_magnitude_of_Z0_is ='); disp(Z0,'the_line_characteristic_impedance is ='); //(b)Calculate_the_propagation_constant r=sqrt((R+(%i*w*L))*(G+(%i*w*C))); x=real(r); y=imag(r); o=atand(y,x); disp(o,'the_phase_of_r_is ='); M=abs(r);//magintue_of_r disp(M,'the_magnitude_of_r_is ='); disp(r,'the_propagation_constant is =');
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/VALORANT Anti Peek Training.sce
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VALORANT Anti Peek Training.sce
Name=VALORANT Anti Peek Training PlayerCharacters=Dodgey BotCharacters=Quaker Bot Easy.bot IsChallenge=true Timelimit=120.0 PlayerProfile=Dodgey AddedBots=Quaker Bot Easy.bot;Quaker Bot Easy.bot;Quaker Bot Easy.bot;Quaker Bot Easy.bot PlayerMaxLives=0 BotMaxLives=0;0;0;0 PlayerTeam=1 BotTeams=0;0;0;0 MapName=794569841.map MapScale=3.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=true TimeRefilledByKill=0.0 ScoreToWin=1.0 ScorePerDamage=1.0 ScorePerKill=100.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=1.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=true ScoreMultKillEfficiency=false GameTag=VALORANT WeaponHeroTag=Vandal DifficultyTag=2 AuthorsTag=(edited by Tangelo) (edited by T1c Tac), gli, Zaeyron BlockHitMarkers=true BlockHitSounds=true BlockMissSounds=true BlockFCT=true Description=Corrected Bot and Player movement to better simulate VALORANT movement. GameVersion=2.0.1.2 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false 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 Easy DodgeProfileNames=cs peek DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=0.0;0.0;2.0;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=Valorant Peek Bot 1,0 SeeThroughWalls=false NoDodging=false NoAiming=true 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=Dodgey MaxHealth=200.0 WeaponProfileNames=Vandal;;;;;;; MinRespawnDelay=0.5 MaxRespawnDelay=0.5 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=100.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=750.0 MaxCrouchSpeed=500.0 Acceleration=2000.0 AirAcceleration=16000.0 Friction=7.0 BrakingFrictionFactor=0.0 JumpVelocity=600.0 Gravity=3.0 AirControl=0.25 CanCrouch=false CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=true EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=240.0 MainBBRadius=80.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=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 [Character Profile] Name=Valorant Peek Bot 1,0 MaxHealth=150.0 WeaponProfileNames=;Rocket Launcher no Knockback;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=0.0 CrouchHeightModifier=0.6 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=750.0 MaxCrouchSpeed=300.0 Acceleration=2000.0 AirAcceleration=16000.0 Friction=7.0 BrakingFrictionFactor=0.0 JumpVelocity=0.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=220.0 MainBBRadius=30.0 MainBBHasHead=true MainBBHeadRadius=20.0 MainBBHeadOffset=0.0 MainBBHide=true ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 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=Endo 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=cs peek MaxTargetDistance=10000.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.125 MaxLRTimeChange=0.6 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.5 MaxCrouchTime=1.0 MinJumpTime=0.0 MaxJumpTime=0.0 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=1.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.0 BlockedMovementReactionMax=0.125 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=Vandal Type=Hitscan ShotsPerClick=1 DamagePerShot=50.0 KnockbackFactor=0.2 TimeBetweenShots=0.108 Pierces=true Category=FullyAuto BurstShotCount=2 TimeBetweenBursts=0.1 ChargeStartDamage=0.1 ChargeStartVelocity=X=1500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=3000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=3000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=3.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=4.0 MagazineMax=25 AmmoPerShot=1 ReloadTimeFromEmpty=1.5 ReloadTimeFromPartial=1.5 DamageFalloffStartDistance=1000000.0 DamageFalloffStopDistance=1000000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.02 BounceOffWorld=true BounceFactor=0.6 BounceCount=0 HomingProjectileAcceleration=6000.0 ProjectileEnemyHitRadius=0.1 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.1 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-40.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.2 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=390.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=1.0 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=25 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=10.3 ADSFOVScale=Quake/Source 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=Gunshot ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=Bullet ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.1 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=true DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=true DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=5.0 BlockedByWorld=true SpreadSSA=4.0,15.0,-9.0,2.5 SpreadSCA=4.0,15.0,-9.0,2.5 SpreadMSA=4.0,15.0,-9.0,2.5 SpreadMCA=4.0,15.0,-9.0,2.5 SpreadSSH=2.0,27.0,-9.0,1.5 SpreadSCH=2.0,27.0,-9.0,0.0 SpreadMSH=100.0,1000.0,5.0,20.0 SpreadMCH=4.0,15.0,-9.0,1.8 MaxRecoilUp=0.3 MinRecoilUp=0.3 MinRecoilHoriz=-0.3 MaxRecoilHoriz=0.3 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.0001 TimeToRecoilReset=0.075 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.1 AAMaxSpeed=5.0 AADeadZone=0.0 AAFOV=10.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=0.1 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=true PSRLoopStartIndex=5 PSRViewRecoilTracking=0.45 PSRCapUp=90.0 PSRCapRight=90.0 PSRCapLeft=90.0 PSRTimeToPeak=0.16 PSRResetDegreesPerSec=35.0 PSR0=0.5,0.0 PSR1=1.2,0.1 PSR2=2.0,0.1 PSR3=2.0,0.2 PSR4=1.7,1.2 PSR5=1.7,0.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=Rocket Launcher no Knockback Type=Projectile ShotsPerClick=1 DamagePerShot=120.0 KnockbackFactor=0.0 TimeBetweenShots=0.8 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=5090.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=5090.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=100.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=0.0 HeadshotCapable=false HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Rocket VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=2.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 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=Horizontal (16:9) ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Flare ParticleBodyImpact=Flare ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=true Radius=500.0 DamageAtCenter=120.0 DamageAtEdge=0.1 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=true DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=true SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 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//2.17 clc; Vm=230*2^0.5; alph=40; Io=((2*Vm/%pi*cosd(alph))-50)/5; printf("Average value of load current = %.2f A", Io)
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//page 271 //Example 8.1 clc; clear; close; n = round(rand() * 10 + 2); a = round(rand(1,n) * 10) b = round(rand(1,n) * 10) disp(n,'n = '); disp(a,'a = '); disp(b,'b = '); disp(a*b','Then, (a|b) = '); //end
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clc T1=673; //K T2=473; //K T0=303; //K T1a=T2; //dSa/dS=T1/T1a // W=(T1-T0)*dS; Work done by the power cycle when there was no temperature difference between the vapour condensing and vapour evaporating // Wa=(T1-T0)*dSa; Work done by the power cycle when the vapour condenses at 400°C and vapour evaporates at 200°C //Fraction of energy that becomes unavailable is given by (W-Wa)/W UAE=T0*(T1-T1a)/T1a/(T1-T0); disp("the fraction of energy that becomes unavailable =") disp(UAE)
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//ques6 clc disp('definite integral'); syms x a n=input('Enter n :'); g=exp(a*x)*(sin(x))^n; f=integ(g,x); disp(f);
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[1,2] * [1,2,-5] = [1,4,-1,-10] initial: [1,4,-1,-10] / [1,2], rem1=[1,4,-1,-10], div2=[1,2], lenq=3, len1=4, len2=2 step end: quot=[0,0,0]/qden=1, rem1=[1,4,-1,-10]/rden=1, div2=[1,2], bquot=-5, lenq=3, len1=4, len2=2 while end: quot=[0,0,-5]/1, rem1=[1,4,4]/1 step end: quot=[0,0,-5]/qden=1, rem1=[1,4,4]/rden=1, div2=[1,2], bquot=2, lenq=3, len1=3, len2=2 while end: quot=[0,2,-5]/1, rem1=[1,2]/1 step end: quot=[0,2,-5]/qden=1, rem1=[1,2]/rden=1, div2=[1,2], bquot=1, lenq=3, len1=2, len2=2 while end: quot=[1,2,-5]/1, rem1=[0]/1 / vect1 = [1,2,-5] initial: [1,4,-1,-10] / [1,2,-5], rem1=[1,4,-1,-10], div2=[1,2,-5], lenq=2, len1=4, len2=3 step end: quot=[0,0]/qden=1, rem1=[1,4,-1,-10]/rden=1, div2=[1,2,-5], bquot=2, lenq=2, len1=4, len2=3 while end: quot=[0,2]/1, rem1=[1,2,-5]/1 step end: quot=[0,2]/qden=1, rem1=[1,2,-5]/rden=1, div2=[1,2,-5], bquot=1, lenq=2, len1=3, len2=3 while end: quot=[1,2]/1, rem1=[0]/1 / vect2 = [1,2]
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// Scilab Code Ex6.7: Page-372 (2011) clc;clear; phi = %pi/2; // Scattering angle, degrees m0 = 9.1e-031;....// Rest mass of an electron, kg h = 6.62e-034;....// Planck's constant, J-s c = 3e+008;....// Speed of light in vacuum, m/s E = 8.16e-014;....// Energy of gamma radiation, J lambda = h*c/(E*1e-010); // Wavelength of incident photon, angstrom lambda_prime = lambda+h*(1-cos(phi))/(m0*c*1e-010); // Wavelength of scattered photon, angstrom printf("\nThe wavelength of radiation at 90 degrees = %6.4f angstrom", lambda_prime); // Result // The wavelength of radiation at 90 degrees = 0.0486 angstrom
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load isZero.hdl, output-file isZero.out, compare-to isZero.cmp, output-list in%B1.8.1 zero%B3.1.3; set in %B00000000, eval, output; set in %B00000001, eval, output; set in %B00000010, eval, output; set in %B00000100, eval, output; set in %B00001000, eval, output; set in %B00010000, eval, output; set in %B00100000, eval, output; set in %B01000000, eval, output; set in %B10000000, eval, output; set in %B11111111, eval, output;
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//Example 5.6// x=0.75*10^-3;//m //meter //given t=3.6*10^4;//s //seconds //time a=0.95;//given D=(x^2)/((a^2)*(t)) mprintf("D = %e m^2/s",D) b=20*10^-6;//m^2/s //preexponential constant c=142000;//J/mol //activation energy for defect motion d=8.314;//J/(mol.K)//universal gas constant e=c/d //mprintf("\ne = %e",e) y=(-log(D/b)) T1=inv(y/e) mprintf("\nT1 = %i K = 952 degree C",T1)
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//Chapter-6, Illustration 1, Page 308 //Title: Refrigeration cycles //============================================================================= clc clear //INPUT DATA COP=8.5;//Co-efficient of performance T1=300;//Room temperature in K T2=267;//Refrigeration temperature in K //CALCULATIONS COPmax=T2/(T1-T2);//Maximum COP possible //OUTPUT mprintf('Maximum COP possible is %3.2f \n Since the COP claimed by the inventor is more than the maximum possible COP his claim is not correct',COPmax) //==============================END OF PROGRAM=================================
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// FUNDAMENTALS OF ELECTICAL MACHINES // M.A.SALAM // NAROSA PUBLISHING HOUSE // SECOND EDITION // Chapter 7 : THREE-PHASE INDUCTION MOTOR // Example : 7.7 clc;clear; // clears the console and command history // Given data V = 440 // supply voltage in V P = 6 // number of poles f = 50 // frequency in Hz P_a = 45000 // i/p power N_l = 900 // speed in rpm P_tloss = 2000 // total power loss in W // caclulations N_s = 120*f/P // synchronous speed in rpm s = (N_s-N_l)/N_s // slip P_ag = (P_a-P_tloss) // air gap power in W P_rcu = s*P_ag // rotor copper loss in W P_mech = P_ag-P_rcu // mechanical power in W P_0 = P_mech-3000 // o/p power in W n = (P_0/P_ag)*100 // efficiency since n = P_o/P_in // display the result disp("Example 7.7 solution"); printf(" \n Slip \n s = %.1f \n", s ); printf(" \n Rotor copper loss \n P_rcu = %.f W \n", P_rcu ); printf(" \n Out put power \n P_0 = %.f W \n", P_0 ); printf(" \n Efficiency \n n = %.f percent \n", n );
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// código modelo de hidrolise enzimática de amido brandam et al (2003) anexado a otimização por enxame de partículas clear clc tic() format(10) // valores dos parâmetros // gelatinização, T < Tg k_g1 = 5.7*10^31 // s^-1 E_g1 = 220.6 // kJ/mol // gelatinização, T > Tg k_g2 = 3.1*10^14 // s^-1 E_g2 = 108.3 // kJ/mol K = 273.15 // converter para°C T_g = 60 + K // ºC // constante dos açúcares k_gl = 0.023 // kg/U s k_mlt = 0.117 // kg/U s k_dex = 0.317 // kg/U s k_alfa_mal = 0.389 // kg/U s k_beta_mal = 0.137 // kg/U s k_gl_ = 2.9*10^-8 // kg/U s k_mlt_ = 1.5*10^-8 // kg/U s k_alfa_mal_ = 1.2*10^-7 // kg/U s k_beta_mal_ = 8.4*10^-8 // kg/U s // constante dos Gases R = 8.314/1000 // J/mol K T_i = 62.562772 //PSO Foco em Gasto e Rendimento II tempo_zero = (4.2)*(T_i-25)*30*60 // massas molares MM_gli = 180.156 // g/mol MM_mal = 342.3 // g/mol MM_mlt = 504.437 // g/mol MM_dex = 504.4 // g/mol // condições iniciais x1_0 = 98.51 //Concentração Amido Sólido Inicial em g/L x2_0 = 0.0 //Concentração Amido Gelatinizado Inicial em g/L x3_0 = 0.0 //Concentração Dextrinas Inicial em g/L x4_0 = 0.0 //Concentração Glicose Inicial em g/L x5_0 = 0.0 //Concentração Maltose Inicial em g/L x6_0 = 0 //Concentração Maltotriose Inicial em g/L function Taxa_Gelatinizacao = Sist_1(x1) if (T < T_g) then r_g = x1*k_g1*exp(-(E_g1/(R*T))) else r_g = x1*k_g2*exp(-(E_g2/(R*T))) end Taxa_Gelatinizacao = r_g endfunction function Atividade = Sist_2_3(T) if T < (63+273.15) then a_a = -0.001270154057*T^3 + 1.235930164837*T^2 - 400.438346*T + 43203.7983384673 a_b = 0.049*T -13.9 end if T >= (63+273.15) then a_a = 0.005646191991*T^3 - 5.814417*T^2 + 1995.013302*T - 228070.0234 a_b = -0.374*T + 128.3 end if a_a < 0 then a_a = 0 end if a_b < 0 then a_b = 0 end if T <313 then a_a = 1 a_b = 1 end a_Tref = 220.28986 b_Tref = 486.95652 Atividade = [a_a*a_Tref,a_b*b_Tref] endfunction function Amido = Sist_4(x2,T) a_ = Sist_2_3(T) a_a = a_(1) a_b = a_(2) r_gl = k_gl*a_a*x2 r_mal = k_alfa_mal*a_a*x2+k_beta_mal*a_b*x2 r_mlt = k_mlt*a_a*x2 r_dex = k_dex*a_a*x2 Amido = [r_gl,r_mal,r_mlt,r_dex] endfunction function Dextrinas = Sist_5(x3,T) a_ = Sist_2_3(T) a_a = a_(1) a_b = a_(2) r_gl_ = k_gl_*a_a*x3 r_mal_ = k_alfa_mal_*a_a*x3 + k_beta_mal_*a_b*x3 r_mlt_ = k_mlt_*a_a*x3 Dextrinas = [r_gl_,r_mal_,r_mlt_] endfunction function out = f(in) for k=1:length(in) if in(k)<0 in(k)=0 end end x1 = in(1) x2 = in(2) x3 = in(3) r_g = Sist_1(x1) r_amido = Sist_4(x2,T) r_dextrinas = Sist_5(x3,T) r_gl = r_amido(1) r_mal = r_amido(2) r_mlt = r_amido(3) r_dex = r_amido(4) r_gl_ = r_dextrinas(1) r_mal_ = r_dextrinas(2) r_mlt_ = r_dextrinas(3) dx1 = -r_g //dSs_dt dx2 = r_g - r_gl - r_mal - r_mlt - r_dex //dSg_dt dx3 = r_dex - r_gl_ - r_mal_ - r_mlt_ //dD_dt dx4 = r_gl + r_gl_ //dgl_dt dx5 = r_mal + r_mal_; //dmal_dt dx6 = r_mlt + r_mlt_; //dmlt_dt out=[dx1,dx2,dx3,dx4,dx5,dx6] endfunction dt = 0.25 // passo de integração tf = 60*60 // tempo final em s limit_time = tf/60 function Cp = calor_especifico(T) Cp = (-4*10^(-11)*(T-K)^5 + 1*10^(-8)*(T-K)^4 - 1*10^(-6)*(T-K)^3 + 1*10^(-4)*(T-K)^2 - 0.0033*(T-K) + 4.2198) //kJ/kg K endfunction // PSO function fitness = simulador(plottar,T0, c_ang,tempos) gasto = 0 kant = 0 b = T0 T = T0 + 273.15 t_min = 1e30 gasto_min = 1e30 tempos = [0,tempos,(tf-sum(tempos))] kk = length(tempos) tempos_original = tempos for k = 2:kk tempos(k)=sum(tempos_original(1:k)) end in=[x1_0,x2_0,x3_0,x4_0,x5_0,x6_0] for t=dt:dt:tf-dt for k = 1:length(tempos)-1 if t > tempos(k) && t <= (tempos(k+1)) if k~=kant T0 = T - K b = T0 - c_ang(k)*t end T = c_ang(k)*t + b kant = k end end if T > T_max then T = T_max end if T < T_min then T = T_min end T=T+K k1 = f(in) k2 = f(in + 0.5*dt*k1) k3 = f(in + 0.5*dt*k2) k4 = f(in + dt*k3) for i=1:length(in) in(i) = in(i) + (dt/6)*(k1(i) + 2*k2(i) + 2*k2(i) + 2*k3(i) + k4(i)) end tt(t/dt) = t/60 TT(t/dt) = T-K d_x1(t/dt) = in(1) // Amido d_x2(t/dt) = in(2) // Amido Gelatinizado d_x3(t/dt) = in(3) // Dextrinas d_x4(t/dt) = in(4) // Glicose d_x5(t/dt) = in(5) // Maltose d_x6(t/dt) = in(6) // Maltotriose //gasto = gasto+(T*dt) gasto = gasto+((T+K)*dt)*(calor_especifico(T)) evolucao_ami = (d_x1(t/dt)) produzido_gli = (d_x4(t/dt)-x4_0) produzido_mal = (d_x5(t/dt)-x5_0) produzido = (d_x4(t/dt)+d_x5(t/dt))-(x4_0+x5_0) //concentrações finais das espécies em mol/L //desejados mols_gli = d_x4(t/dt)/MM_gli mols_mal = d_x5(t/dt)/MM_mal //indesejados mols_dex = d_x3(t/dt)/MM_dex mols_mlt = d_x6(t/dt)/MM_mlt //seletividade selet = (mols_gli+mols_mal)/(mols_mlt+mols_dex) end if plottar==1 disp("Gastando = "+ string((tempo_zero+gasto)/((limit_time+30)*60))+" kJ.s/kg") disp("Gastando = "+ string(gasto)+" kJ.s/kg") disp("Rendimento em glicose = "+ string(produzido_gli)+" g/L") disp("Rendimento em maltose = "+ string(produzido_mal)+" g/L") disp("Evolução do Amido Sólido = "+ string(evolucao_ami)+" g/L") disp("Seletividade de "+ string(selet)) scf() plot(tt,d_x1,'g.') plot(tt,d_x3,'c.') //plot(tt,d_x4,'r.') //plot(tt,d_x5,'b.') //plot(tt,d_x6,'y.',"markerSize",2) xlabel("Time (min)") ylabel("Concentration (g/L)") g=gca() g.data_bounds = [0,0;limit_time,100] xtitle('Concentração ao longo do tempo',['Time (min)'],['Concentration (g/L)']) //h=legend(["Amido Sólido", "Dextrinas", "Glicose", "Maltose", "Maltotriose"], pos=-2) g1 = newaxes() set(g1, "filled", "off") plot(tt,TT,'k.',"markerSize",2) //xlabel("Tempo (min)") ylabel("Temperature (ºC)") g1=gca() g1.data_bounds = [0,25;limit_time,80] g1.axes_visible(1) = "off" g1.y_location = "right" end //if produzido < 78 then // produzido = 0 //end fitness = [produzido,gasto] endfunction tpop = 200 vezesmax = 60 c1 = 1 c2 = 2 T_min = 25 T_max = 350-K T_gel = 63 T_a_max = 335-K gasto_min =0 //gasto_max = (tempera_max*tf) fim = 0 // partícula = [Tinicial. 5 c_angulares, 4 intervalos de tempo] N_interv = 5 size_particula = 10 limiteinf = [T_min,-0.1,-0.1,-0.1,-0.1,-0.1,1,1,1,1] limitesup = [T_max,0.1,0.1,0.1,0.1,0.1,tf,tf,tf,tf] amp = limitesup - limiteinf vezes = 1 inercia = 2 iner=ones(tpop,size_particula)*inercia for i = 1:tpop for j = 1:size_particula velocidades(i,j) = rand()*amp(j)/10 posicao(i,j)= rand()*amp(j) + limiteinf(j) if j > (N_interv + 2) tempousado = sum(posicao(i,7:(j-1))) tempolivre = tf - tempousado posicao(i,j) = rand()*tempolivre end end pbest(i,:) = [0,1e30] melhorposicao(i,:) = posicao(i,:) end gbest = [0,1e30] posicao(1,:) = [64.668384 -0.0486105 0.0000459 -0.0011856 0.0385702 0.0190725 48.140101 3511.4108 8.5148174 0.2732467] //chute inicial disp("entrou no loop principal") while fim==0 for i=1:tpop fitness(i,:) = simulador(0,posicao(i,1),posicao(i,2:6),posicao(i,7:10)) if (fitness(i,1)> pbest(i,1)) melhorposicao(i,:) = posicao(i,:) pbest(i,:) = fitness(i,:) end if (pbest(i,1) > gbest(1)) gbest = pbest(i,:) melhorvez = vezes melhorpartic = i melhorposicaodetodos = posicao end printf('\n i=%d vez=%d, particula= %.02f %.02f %.02f %.02f %.02f %.02f %.02f %.02f %.02f %.02f \n sumtempo = %.01f, produzido = %.02f, gastando = %.02f \n Gbest = %.02f %.02f \n\n', i,vezes, posicao(i,1), posicao(i,2), posicao(i,3), posicao(i,4), posicao(i,5), posicao(i,6), posicao(i,7), posicao(i,8), posicao(i,9), posicao(i,10), sum(posicao(i,7:10)), fitness(i,1), fitness(i,2), gbest(1),gbest(2)) end inercia=(inercia-inercia/2) if inercia<0.05 then inercia=2 end for i=1:tpop for k=1:size_particula iner(i,k) = inercia velocidades(i,k)=inercia*velocidades(i,k)+ (c1* rand()*(melhorposicao(i,k)-posicao(i,k))) + (c2*rand()*melhorposicaodetodos(melhorpartic,k)-posicao(i,k)) posicao(i,k)=posicao(i,k)+velocidades(i,k) if posicao(i,k)>limitesup(k) || posicao(i,k)<limiteinf(k) posicao(i,k)=rand()*amp(k)*0.3 + limiteinf(k) end end for k=1:size_particula if k>(N_interv+2) && sum(posicao(i,7:(k)))>=tf //disp(posicao(i,:)) tempousado=sum(posicao(i,7:(k-1))) tempolivre=tf-tempousado if tempolivre<0 disp(k) disp(tempousado) disp(tempolivre) disp(posicao(i,:)) pause end posicao(i,k)= rand()*tempolivre //disp(k) //disp(tempousado) //disp(tempolivre) //disp(posicao(i,:)) //pause end end end vetorgbest(vezes,:)=gbest vezes=vezes+1 if vezes>=vezesmax then fim=1 //end end if ((vezes/20)-int(vezes/20))<0.01 then for i = 1:tpop if i<>melhorpartic then for j = 1:size_particula velocidades(i,j) = rand()*amp(j)/10 posicao(i,j)= rand()*amp(j) + limiteinf(j) if j > (N_interv + 2) tempousado = sum(posicao(i,7:(j-1))) tempolivre = tf - tempousado posicao(i,j) = rand()*tempolivre end end end //pbest(i,:) = [0,1e30] //melhorposicao(i,:) = posicao(i,:) end end if (fim==1) then fitness(i,:) = simulador(1,melhorposicaodetodos(melhorpartic,1),melhorposicaodetodos(melhorpartic,2:6),melhorposicaodetodos(melhorpartic,7:10)) end end disp("Otimização concluída :)") disp("") disp("Tempo de execução: " + string(int(toc())) + "s")
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//Find x in R^6 such that: //Check for the size of constraints conMatrix= [-1,1,0,3,1; -1,0,-3,-4,5; 2,5,3,0,1 0,1,0,1,2; -1,0,2,1,1]; conLB=[1;2;3;-%inf;-%inf]; conUB = [1;2;3;-1;2.5]; lb=[-1000;-10000; 0; -1000; -1000; -1000]; ub=[10000; 100; 1.5; 100; 100; 1000]; //and minimize 0.5*x'*Q*x + p'*x with p=[1; 2; 3; 4; 5; 6]; Q=eye(6,6); nbVar = 6; nbCon = 5; x0 = repmat(0,nbVar,1); param = list("MaxIter", 300, "CpuTime", 100); [xopt,fopt,exitflag,output,lambda]=qpipopt(nbVar,nbCon,Q,p,lb,ub,conMatrix,conLB,conUB,x0,param) //Error //qpipopt: The size of constraints is not equal to the number of variables //at line 175 of function qpipopt called by : //[xopt,fopt,exitflag,output,lambda]=qpipopt(nbVar,nbCon,Q,p,lb,ub,conMatrix,conLB,conUB,x0,param)
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function c=str2code(str) // str2code - return scilab integer codes associated with a character string //! if prod(size(str))<>1 then error('Not implemented for vector of strings') end alpha=['0','1','2','3','4','5','6','7','8','9',.. 'a','b','c','d','e','f','g','h','i','j',.. 'k','l','m','n','o','p','q','r','s','t',.. 'u','v','w','x','y','z','_','#','!','0',.. ' ','(',')',';',':','+','-','*','/','\',.. '=','.',',','''','[',']','%','|','&','<','>','~',.. '^'] alphb=['0','1','2','3','4','5','6','7','8','9',.. 'A','B','C','D','E','F','G','H','I','J',.. 'K','L','M','N','O','P','Q','R','S','T',.. 'U','V','W','X','Y','Z','0','0','?','0',.. '0','0','0','0','0','0','0','0','0','$',.. '0','0','0','""','{','}','0','0','0','`','0','@',.. '0'] c=[] for k=1:length(str) l=find(alpha==part(str,k)) if l<>[] then c=[c,l(1)-1] else l=find(alphb==part(str,k)) c=[c,-l(1)+1] end end
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Ex7_07.sce
// Scilab Code Ex7.7: Page-255 (2014) clc; clear; e = 1.602e-019; // Charge on an electron, C h = 6.62e-034; // Planck's constant, Js h_bar = h/(2*%pi); // Reduced Planck's constant, Js m = 9.11e-031; // Electron mass, kg B = 2.00; // External magnetic field, T m_l1 = 0; // Lower orbial magnetic quantum number m_l2 = 1; // Upper orbial magnetic quantum number delta_m_l = m_l2 - m_l1; // Change in m_l mu_B = e*h_bar/(2*m); // Bohr's magneton, J/T delta_E = mu_B*B*delta_m_l/e; // Energy difference between components of p states of atomic hydrogen placed in the external field, eV printf("\nThe value of Bohr magneton = %4.2e J/T", mu_B); printf("\nThe energy difference between components of p states of atomic hydrogen placed in the external field = %4.2e eV", delta_E); // Result // The value of Bohr magneton = 9.26e-024 J/T // The energy difference between components of p states of atomic hydrogen placed in the external field = 1.16e-004 eV
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// Exa 7.5 clc; clear; // Given data // A wide-band pass filter fL=400; // Lower cutoff frequency(Hz) fH=2000; // Higher cutoff frequency(Hz) A0=4; // passband gain // Solution printf('Since, the pass band gain is 4. so each of LPF and HPF section may be designed to give gain of 2,\n that is Ao=1+ (Rf/Ri) = 2.\n So, Rf and Ri should be equal. \n Let Rf=Ri=10 kΩ for each of LPF and HPF sections.'); disp(""); disp(""); disp("For HPF, fL=400 Hz."); printf(' Assume C2=0.01 μF. '); C2=0.01*10^-6; // Farads // Since fL= 1/(2*%pi*R2*C2); // Therefore R2= 1/(2*%pi*C2*fL); printf(' \n The calculated value of R = %.1f kΩ.',int(R2)/1000); disp(""); disp(""); disp("For LPF, fH=2000 Hz."); printf(' Assume C1=0.01 μF.'); C1=0.01*10^-6; // Farads // Since fH= 1/(2*%pi*R1*C1); // Therefore R1= 1/(2*%pi*C1*fH); printf(' \n The calculated value of R = %.2f kΩ.',R1/1000); disp(""); disp(""); fo=sqrt(fL*fH); Q=fo/(fH-fL); printf(' The value of cutoff frequency = %.1f Hz.\n ',fo); printf('\n The quality factor = %.2f (<10) since wide passband filter.',Q);
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s=poly(0,'s'); F=syslin('c',[80000/((2+s)*s*(s+50)*(s+200))]) //without k fmin=0.1; //Min freq in Hz fmax=20; //Max freq in Hz scf(1);clf; bode(F,fmin,fmax); //Plots frequency response of open-loop system in Bode diagram [GainMargin,freqGM]=g_margin(F) //Calculates gain margin [dB] and corresponding frequency [Hz] disp(GainMargin,"GM=") [PhaseMargin,freqPM]=p_margin(F) //Calculates phase [deg] and corresponding freq [Hz] of phase margin disp(PhaseMargin,"PM=") show_margins(F) //display gain and phase margin and associated crossover frequencies
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gauspuls.sci
function [y]=gauspuls(t,fc,bw) // Generates Gaussian-modulated sinusoidal pulses // Calling Sequence // [y]=gauspuls(t,fc,bw) // [y]=gauspuls(t,fc) // [y]=gauspuls(t) // Parameters // t: Real or complex valued vector or matrix // fc: Real non negative number or complex number // bw: Real positive number or complex number // Description // This is an Octave function // This function returns a Gaussian RF pulse of unity amplitude at the times indicated in array t. // Examples // 1. gauspuls(1,2,3) // ans= 1.427D-56 // 2. gauspuls([1 2 3],1,1) // ans= 0.0281016 0.0000006 1.093D-14 funcprot(0); rhs=argn(2); if ( rhs<1 ) then error ("Wrong number of input arguments.") elseif (rhs==1) y= callOctave("gauspuls",t) elseif (rhs==2) y= callOctave("gauspuls",t,fc) else y= callOctave("gauspuls",t,fc,bw) end endfunction
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Chapter16_example1.sce
clc clear //Input data s=0.005//Delay in sec d=30//Bore in cm N=600//Speed in r.p.m dx=[10,15,20]//Bore diameters in cm //Calculations t=(s/d)*dx//Time of delay in sec. In textbook, t(2) is given wrong as 0.00025 sec instead of 0.0025 sec //Output printf('The delay time for %i cm diameter bore is %3.5f sec \n The delay time for %i cm diameter bore is %3.5f sec \n The delay time for %i cm diameter bore is %3.5f sec',dx(1),t(1),dx(2),t(2),dx(3),t(3))
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// Example 34_1 clc;funcprot(0); //Given data P=120000;// The cost of the water softner plant in rupees S=(8/100)*P;// The salvage value of the plant in rupees r=8/100;//Interest on sinking fund n=12;//The life of the plant in years RMLc=8000;//Repair,maintainence and labour costs Cc=5000;// Chemical cost //Calculation A=(P-S)*(r/(((1+r)^n)-1));// Annual sinking fund payment for the plant in rupees Ac=A+RMLc+Cc;// Annual cost of the plant in rupees printf('\nAnnual cost of the plant=Rs.%0.0f',Ac); // The answer vary due to round off error
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ex3_31.sce
//Exam:3.31 clc; clear; close; //Miller indices of plane n=1; h=1; k=1; l=1; angle=30;//in degree wavelength=2;//in angstrom d=n*wavelength/(2*sind(angle));//interplanar spacing a=d*(h^2+k^2+l^2)^(1/2);//interatomic spacing disp(a,'interatomic spacing(in angstrom)=');
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Ex7_2.sce
//Ex 7.2 clc;clear;close; format('v',5); Zs=240;//no. of conductors in stator winding Zr=48;//no. of conductors in rotor winding Rr=0.013;//ohm/phase(resstance rotor windig) XL=0.048;//ohm/phase(leakega reactance) Vs=400;//V //(a) Eo=Vs*Zr/Zs;//V(rotor emf) disp(Eo,"(a) Rotor emf(V)"); //(b) S=4/100;//slip Eo=Eo*S;//V(rotor emf for 4% slip) disp(Eo,"(b) Rotor emf at 4% slip(V)"); Z=sqrt(Rr^2+(S*XL)^2);//ohm/phase(rotor impedence at 4% slip) Ir=Eo/Z;//A(Rotor curren at 4% slip) disp(Ir,"(b) Rotor curren at 4% slip(A)"); //(c) fi_r=atand(S*XL/Rr);//degree disp(fi_r,"(c) Phase difference at 4% slip(degree)"); S=100/100;//100% slip fi_r=atand(S*XL/Rr);//degree disp(fi_r,"(c) Phase difference at 100% slip(degree)");
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ex7_7.sce
// Exa 7.7 format('v',6);clc;clear;close; // Given data Cin = 35;// in pF // (R1+Rin)/Rin = 10; RinBYR1= 1/9; //while balance equation with compensating capacitor // R1*C1 = Rin*(C2+Cin); C1= Cin*RinBYR1;//compansating capacitor in pF disp(C1,"The compansating capacitor in pF is");
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10_04.sce
//Problem 10.04: An ammeter has a f.s.d. of 100 mA and a resistance of 50 ohms. The ammeter is used to measure the current in a load of resistance 500 ohms when the supply voltage is 10 V. Calculate (a) the ammeter reading expected (neglecting its resistance), (b) the actual current in the circuit, (c) the power dissipaed in the ammeter, and (d) the power dissipated in the load. //initializing the variables: V = 10; // in volts fsd = 0.1; // in Amperes ra = 50; // in ohms R = 500; // in ohms //calculation: Ie = V/R Ia = V/(R + ra) Pa = Ia*Ia*ra PR = Ia*Ia*R printf("\n\n Result \n\n") printf("\n (a)expected ammeter reading = %.2E A\", Ie) printf("\n (b)Actual ammeter reading = %.2E A",Ia) printf("\n (c)Power dissipated in the ammeter = %.2E W", Pa) printf("\n (d)Power dissipated in the load resistor = %.2E W",PR)
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2_03.sce
//Problem 2.03: The current flowing through a resistor is 0.8 A when a p.d. of 20 V is applied. Determine the value of the resistance. //initializing the variables: I = 0.8; // in Ampere V = 20; // in Volts //calculation: R = V/I printf("\n\nResult\n\n") printf("\nResistance(R): %.0f Ohms\n",R)
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Ex14_1.sce
clear; clc; disp(' Example 14.1'); // aim : To determine // (a) the free air delivered // (b) the volumetric efficiency // (c) the air delivery temperature // (d) the cycle power // (e) the isothermal efficiency // given values d = 200*10^-3;// bore, [m] L = 300*10^-3;// stroke, [m] N = 500;// speed, [rev/min] n = 1.3;// polytropic index P1 = 97;// intake pressure, [kN/m^2] T1 = 273+20;// intake temperature, [K] P3 = 550;// compression pressure, [kN/m^2] // solution // (a) P4 = P1; P2 = P3; Pf = 101.325;// free air pressure, [kN/m^2] Tf = 273+15;// free air temperature, [K] SV = %pi/4*d^2*L;// swept volume, [m^3] V3 = .05*SV;// [m^3] V1 = SV+V3;// [m^3] V4 = V3*(P3/P4)^(1/n);// [m^3] ESV = (V1-V4)*N;// effective swept volume/min, [m^3] // using PV/T=constant Vf = P1*ESV*Tf/(Pf*T1);// free air delivered, [m^3/min] mprintf('\n (a) The free air delivered is = %f m^3/min\n',Vf); // (b) VE = Vf/(N*(V1-V3));// volumetric efficiency mprintf('\n (b) The volumetric efficiency is = %f percent\n',VE*100); // (c) T2 = T1*(P2/P1)^((n-1)/n);// free air temperature, [K] mprintf('\n (c) The air delivery temperature is = %f C\n',T2-273); // (d) CP = n/(n-1)*P1*(V1-V4)*((P2/P1)^((n-1)/n)-1)*N/60;// cycle power, [kW] mprintf('\n (d) The cycle power is = %f kW\n',CP); // (e) // neglecting clearence W = n/(n-1)*P1*V1*((P2/P1)^((n-1)/n)-1) Wi = P1*V1*log(P2/P1);// isothermal efficiency IE = Wi/W;// isothermal efficiency mprintf('\n (e) The isothermal efficiency neglecting clearence is = %f percent\n',IE*100); // End
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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 0.254973D+00 2 -0.341532D-02 0.194612D-02 3 -0.878505D-01 0.580712D-03 0.439514D+00 4 0.625273D-04 -0.694377D-03 -0.569146D-02 0.372769D-02 5 -0.327907D-03 -0.179969D-04 -0.249702D-03 -0.314408D-04 0.262716D-02 6 -0.214174D-03 0.153181D-04 -0.127064D-03 -0.764085D-04 0.319585D-03 7 0.173440D-03 -0.770122D-04 0.412983D-03 -0.165946D-04 0.456395D-03 8 -0.266649D-03 -0.346814D-04 -0.455140D-03 0.477699D-04 0.114116D-03 9 -0.231979D+00 -0.171528D-04 0.142381D+00 0.169804D-01 0.379816D-01 10 -0.219967D+00 -0.560449D-02 0.761405D-01 -0.623712D-02 0.123981D+00 11 -0.927010D-01 0.119550D-01 0.224547D+00 -0.233379D-01 0.145487D-02 12 -0.188963D+00 0.434084D-03 0.672079D+00 0.228633D-01 0.618533D-01 13 -0.909036D-01 -0.151309D-01 -0.679329D-01 -0.287047D-02 0.192105D-01 14 -0.254584D+00 0.587942D-02 0.974765D-01 -0.960546D-03 -0.188937D-01 15 -0.149795D+01 0.190964D-01 -0.194252D+00 0.105341D-01 -0.111231D+00 16 -0.110080D-01 -0.757799D-02 0.192423D-01 -0.108065D-02 -0.151228D-03 17 -0.583902D-03 -0.378362D-03 -0.182940D-02 0.794921D-04 -0.185541D-03 18 -0.360680D+00 0.410837D-01 -0.125127D+00 -0.111851D-01 -0.228893D-01 19 0.100125D+00 -0.393836D-02 0.129646D-01 -0.324684D-02 -0.649102D-02 20 -0.801249D-01 -0.548362D-02 0.177785D+01 0.170399D-01 -0.190615D-01 21 -0.790954D-01 0.309091D-02 -0.266685D-01 0.476373D-02 0.561330D-02 22 0.110597D-02 -0.800001D-04 0.134742D-02 0.129582D-03 -0.424446D-04 23 -0.898159D-02 -0.238862D-03 -0.139826D-01 0.120342D-01 0.750162D-04 24 0.232563D-02 0.813415D-04 0.250248D-02 -0.364822D-03 -0.525405D-04 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.583376D-03 7 0.776903D-03 0.415626D-02 8 0.224158D-05 0.554270D-03 0.319903D-02 9 0.601233D-02 0.677304D-02 0.656255D-02 0.354374D+02 10 0.203883D-01 0.225568D-01 0.597479D-02 0.100481D+01 0.140398D+02 11 0.193303D-01 0.533043D-01 0.494367D-01 -0.240614D+01 0.119364D+01 12 -0.117806D-01 0.466433D-01 0.721238D-01 0.100380D+02 0.175996D+01 13 0.487323D-01 0.123993D+00 -0.206154D-02 0.179763D+01 0.118373D+01 14 -0.710718D-02 0.679913D-01 0.411019D+00 0.338560D+01 0.195757D+01 15 -0.240171D-01 -0.563847D-01 0.142314D-01 -0.277158D+01 -0.891032D+01 16 0.705586D-04 0.673515D-03 0.820627D-03 0.473239D+00 0.398564D-01 17 0.516625D-04 0.186269D-03 -0.195003D-04 -0.782623D-01 0.619074D-02 18 -0.386677D-01 -0.938657D-01 -0.242785D-01 0.600513D+00 -0.374538D+00 19 -0.654295D-02 0.154780D-01 -0.659985D-02 0.279619D+00 -0.697533D+00 20 -0.263188D-01 -0.462980D-01 -0.359550D+00 0.209837D+01 -0.353214D+01 21 0.682915D-02 -0.133067D-01 0.791645D-02 -0.606574D+00 0.715364D+00 22 -0.736924D-04 -0.196832D-03 0.151537D-03 -0.913579D-02 -0.164972D-02 23 -0.165132D-02 -0.300553D-02 -0.960734D-03 -0.490903D-01 -0.161911D+00 24 0.379400D-03 0.272615D-03 0.228033D-03 -0.164152D-01 0.181436D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.431489D+02 12 -0.653439D+01 0.167489D+03 13 -0.118140D+01 0.692122D-01 0.142915D+02 14 0.571678D+01 0.786920D+01 -0.240464D+01 0.116326D+03 15 -0.325702D+01 0.599078D+01 -0.195963D+01 0.139761D+01 0.168911D+03 16 -0.146113D+00 0.179984D+00 0.107769D+00 0.194313D+00 0.296823D+00 17 0.392491D-01 -0.680627D-01 0.186390D-01 0.149486D-01 -0.738949D+00 18 0.358010D+01 0.189019D+02 -0.641709D+01 -0.112970D+01 -0.258029D+02 19 -0.127790D+01 -0.285493D+00 -0.269298D+00 -0.434555D+00 0.236851D+00 20 -0.468669D-01 -0.200926D+02 -0.161403D+01 -0.755827D+02 0.114919D+02 21 0.154258D+01 0.149004D+00 0.319219D+00 0.397937D+00 -0.121820D+01 22 -0.902473D-01 -0.359585D-01 -0.100159D-01 0.412053D-01 0.132109D+00 23 0.355796D-01 0.130129D+01 -0.274979D+00 -0.386559D+00 0.130463D-01 24 -0.219933D-01 -0.176144D+00 0.348070D-01 -0.773638D-02 -0.352316D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.308438D+00 17 -0.130520D-01 0.956614D-02 18 -0.552440D+00 0.159937D+00 0.171046D+03 19 0.122678D+00 -0.608765D-02 -0.169943D+01 0.488033D+01 20 -0.331917D+00 -0.473398D-02 -0.600141D+02 -0.148950D+01 0.557624D+03 21 -0.136036D+00 0.873710D-02 0.389497D+01 -0.461721D+01 0.190401D+00 22 0.988752D-03 -0.740645D-03 -0.757298D+00 0.139705D-01 0.241633D+00 23 -0.199394D-02 0.457449D-02 -0.591920D+00 -0.197314D+00 0.593570D+01 24 0.409215D-02 -0.204872D-03 0.246208D+00 0.292279D-01 -0.245778D+01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.542754D+01 22 -0.513677D-01 0.812197D-02 23 -0.107048D+00 0.130241D-01 0.892801D+00 24 -0.566265D-02 -0.354377D-02 -0.818052D-01 0.260369D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.153 1.000 3 -0.262 0.020 1.000 4 0.002 -0.258 -0.141 1.000 5 -0.013 -0.008 -0.007 -0.010 1.000 6 -0.018 0.014 -0.008 -0.052 0.258 7 0.005 -0.027 0.010 -0.004 0.138 8 -0.009 -0.014 -0.012 0.014 0.039 9 -0.077 0.000 0.036 0.047 0.124 10 -0.116 -0.034 0.031 -0.027 0.646 11 -0.028 0.041 0.052 -0.058 0.004 12 -0.029 0.001 0.078 0.029 0.093 13 -0.048 -0.091 -0.027 -0.012 0.099 14 -0.047 0.012 0.014 -0.001 -0.034 15 -0.228 0.033 -0.023 0.013 -0.167 16 -0.039 -0.309 0.052 -0.032 -0.005 17 -0.012 -0.088 -0.028 0.013 -0.037 18 -0.055 0.071 -0.014 -0.014 -0.034 19 0.090 -0.040 0.009 -0.024 -0.057 20 -0.007 -0.005 0.114 0.012 -0.016 21 -0.067 0.030 -0.017 0.033 0.047 22 0.024 -0.020 0.023 0.024 -0.009 23 -0.019 -0.006 -0.022 0.209 0.002 24 0.029 0.011 0.023 -0.037 -0.006 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.499 1.000 8 0.002 0.152 1.000 9 0.042 0.018 0.019 1.000 10 0.225 0.093 0.028 0.045 1.000 11 0.122 0.126 0.133 -0.062 0.048 12 -0.038 0.056 0.099 0.130 0.036 13 0.534 0.509 -0.010 0.080 0.084 14 -0.027 0.098 0.674 0.053 0.048 15 -0.077 -0.067 0.019 -0.036 -0.183 16 0.005 0.019 0.026 0.143 0.019 17 0.022 0.030 -0.004 -0.134 0.017 18 -0.122 -0.111 -0.033 0.008 -0.008 19 -0.123 0.109 -0.053 0.021 -0.084 20 -0.046 -0.030 -0.269 0.015 -0.040 21 0.121 -0.089 0.060 -0.044 0.082 22 -0.034 -0.034 0.030 -0.017 -0.005 23 -0.072 -0.049 -0.018 -0.009 -0.046 24 0.097 0.026 0.025 -0.017 0.030 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 -0.077 1.000 13 -0.048 0.001 1.000 14 0.081 0.056 -0.059 1.000 15 -0.038 0.036 -0.040 0.010 1.000 16 -0.040 0.025 0.051 0.032 0.041 17 0.061 -0.054 0.050 0.014 -0.581 18 0.042 0.112 -0.130 -0.008 -0.152 19 -0.088 -0.010 -0.032 -0.018 0.008 20 0.000 -0.066 -0.018 -0.297 0.037 21 0.101 0.005 0.036 0.016 -0.040 22 -0.152 -0.031 -0.029 0.042 0.113 23 0.006 0.106 -0.077 -0.038 0.001 24 -0.021 -0.084 0.057 -0.004 -0.017 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.240 1.000 18 -0.076 0.125 1.000 19 0.100 -0.028 -0.059 1.000 20 -0.025 -0.002 -0.194 -0.029 1.000 21 -0.105 0.038 0.128 -0.897 0.003 22 0.020 -0.084 -0.643 0.070 0.114 23 -0.004 0.049 -0.048 -0.095 0.266 24 0.046 -0.013 0.117 0.082 -0.645 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.245 1.000 23 -0.049 0.153 1.000 24 -0.015 -0.244 -0.537 1.000
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//Chapter 9 //Example 9.6 //page 352 //To calculate short circuit solution using algorithm for short circuit studies clear;clc; Y11=1/(0.15*%i)+1/(0.15*%i)+1/(0.1*%i)+1/(0.2*%i); Y12=-1/(0.2*%i); Y21=Y12; Y13=-1/(0.15*%i); Y31=Y13; Y14=-1/(0.1*%i); Y41=Y14; Y22=1/(0.15*%i)+1/(0.15*%i)+1/(0.1*%i)+1/(0.2*%i); Y23=-1/(0.1*%i); Y32=Y23; Y24=-1/(0.15*%i); Y42=Y24; Y33=1/(0.15*%i)+1/(0.1*%i); Y34=0; Y43=Y34; Y44=1/(0.15*%i)+1/(0.1*%i); //Ybus matrix can be written as Ybus=[Y11 Y12 Y13 Y14;Y21 Y22 Y23 Y24;Y31 Y32 Y33 Y34;Y41 Y42 Y43 Y44]; Zbus=inv(Ybus); //preault voltages V10=1;V20=1;V30=1;V40=1; //post fault voltages V1f=V10-(Zbus(1,4)/Zbus(4,4))*V40; V2f=V20-(Zbus(2,4)/Zbus(4,4))*V40; V3f=V30-(Zbus(3,4)/Zbus(4,4))*V40; V4f=V40-(Zbus(4,4)/Zbus(4,4))*V40; //to calculate fault current through Zf=0 If=V40/(Zbus(4,4)+0); //short circuit current in lines 1-3,1-2,1-4,2-4 and 2-3 I13f=(V1f-V3f)/(0.15*%i); I12f=(V1f-V2f)/(0.2*%i); I14f=(V1f-V4f)/(0.1*%i); I24f=(V2f-V4f)/(0.15*%i); I23f=(V2f-V3f)/(0.1*%i); //If at all fault occurs on bus1 or bus2 If12=1/Zbus(1,1); //displaying the results printf('\n Ybus='); disp(Ybus); printf('\n Zbus='); disp(Zbus); printf('\nV1f= %0.4f pu',V1f); printf('\nV2f= %0.4f pu',V2f); printf('\nV3f= %0.4f pu',V3f); printf('\nV4f= %0.1f pu\n',V4f); printf('\nFault current=-j%0.5f pu\n',abs(If)); printf('\nI13f=j%0.3f pu',abs(I13f)); printf('\nI12f=j%0.3f pu',abs(I12f)); printf('\nI14f=-j%0.3f pu',abs(I14f)); printf('\nI24f=-j%0.3f pu',abs(I24f)); printf('\nI23f=-j%0.3f pu\n',abs(I23f)); printf('\n Fault current for a fault on bus 1 (or bus 2)\n If=-j%0.6f pu\n\n',abs(If12));
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clear clc //Example 8.2 disp('Example 8.2') //Eqn 8-6 //Pump characteristics q=0:0.1:240; Phe=30*(q/200).^2; plot2d(q,Phe,rect=[0,0,240,40]); xgrid() xtitle("Fig 8.13 Pump characteristics","q,gal/min","P,psi") scf(); q=200;//Flow rate in gal/min Phe=30*(q/200).^2; Pv=40-Phe; //Eqn 8-8 //(a) l=0.5;Pv=10; Cv=q/l/sqrt(Pv); mprintf("(a) The value of coefficient Cv is %f",Cv) //plotting valve characteristic curve l=[0:0.01:0.8]'; n=length(l); Cv=125; function y=valve_1(q) Pv=40-30*(q/200).^2; y=Cv*l.*sqrt(Pv)-q; endfunction [q_valve1,f1]=fsolve(200*ones(n,1),valve_1); //200*ones(n,1) is the initial guess for q plot2d(l,q_valve1); //(b) q=200*110/100; //110% flow rate Phe=30*(q/200).^2; Pv=40-Phe; //Eqn 8-8 l=1; Cv=q/sqrt(Pv)/l; mprintf("\n(b) The value of coefficient Cv is %f",Cv) //We use Cv=115; Cv=115; l=[0.2:0.01:0.9]'; n=length(l); R=50; function y=valve_2(q) Pv=40-30*(q/200).^2; y=[R^(l-1)]*Cv.*sqrt(Pv)-q; endfunction [q_valve2,f2]=fsolve(150*ones(n,1),valve_2); plot2d(l,q_valve2,style=2) //(c) Cv=1.2*115; mprintf("\n(c) The value of coefficient Cv is %f",Cv) l=[0.2:0.01:0.9]'; n=length(l); R=50; function y=valve_3(q) Pv=40-30*(q/200).^2; y=[R^(l-1)]*Cv.*sqrt(Pv)-q; endfunction [q_valve3,f3]=fsolve(linspace(60,200,n)',valve_3); //Initial guess has to be smart for each valve, //since we want near linear profile we can give a linear initial guess plot2d(l,q_valve3,style=3) //(d) Cv=0.8*115; mprintf("\n(c) The value of coefficient Cv is %f",Cv) l=[0.2:0.01:0.9]'; n=length(l); R=50; function y=valve_4(q) Pv=40-30*(q/200).^2; y=[R^(l-1)]*Cv.*sqrt(Pv)-q; endfunction [q_valve4,f4]=fsolve(linspace(60,200,n)',valve_4); //Initial guess has to be smart for each valve, //since we want near linear profile we can give a linear initial guess plot2d(l,q_valve4,style=4,rect=[0,0,1,240]) xtitle('Ex-8.2 Installed valve characteristics','$l$','q gal/min'); a=legend("Valve 1, linear Cv=125","Valve 2, Equal% Cv=115","Valve 3, Equal% Cv=138","Valve 4, Equal% Cv=92",position=4); a.font_size=2; a=get("current_axes");b=a.title;b.font_size=3;c=a.x_label;c.font_size=5; c=a.y_label;c.font_size=5;
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angulo = input("Entre com um valor de ângulo em graus de 0° a 90°:"); seno = sind(angulo); disp(seno);
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//Given that deltaP = 9.3*10^3 //in N/m^2 density_water = 998 //in kg/m^3 g = 9.8 //in m/s^2 //Sample Problem 15-2 printf("**Sample Problem 15-2**\n") //deltaP = density_water*g*L //therefore L = deltaP/(density_water*g) printf("The diver started at a depth of %fm", L)
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// * * * * * * * * * * * * * * * * * * * * // // -- Auswertung Winkelregelung -- // // * * * * * * * * * * * * * * * * * * * * // // Boris: cd "/Users/borishenckell/Documents/eclipse workspace/PR_Regelungsrtechnik_-_Versuch_2a/PR Regelungsrechnik - Versuch 2a" // Dirk: cd "/media/daten/workspace/PR_Regelungsrechnik_-_Versuch_2a/PR Regelungsrechnik - Versuch 2a/Scilab/" daten1 = fscanfMat("../Messwerte/win_12"); daten1=daten1; //t=daten1(:,1); Zeit //z=daten1(:,2); Position //phi=daten1(:,3); Winkel //w=daten1(:,4); Winkelgeschwindigkeit //v=daten1(:,5); Geschwindigkeit //s=daten1(:,6); Startsignal //phi_soll=daten1(:,7) ; Referenz-Winkel t1=daten1(:,1); z1=daten1(:,2); phi1=daten1(:,3); w1=daten1(:,4); v1=daten1(:,5); s1=daten1(:,6); phi_soll1=daten1(:,7); // Interessanten bereich ausschneiden [val min_ind] = min(s1)//max(s1(1:length(s1)-1) - s1(2:length(s1))); stoe_anfang = min_ind; [val max_ind] = max(abs(z1)) stoe_ende = max_ind//-195; // Anfang auf null setzen T_1 = t1 - t1(stoe_anfang); // in Sekunden wandeln T1 = T_1; // interessantes Stück ausschneiden T1 = T1(stoe_anfang:stoe_ende); scf(5); clf(5); Z1 = z1(stoe_anfang:stoe_ende); plot2d(T1,Z1,2) xtitle("Position des Wagens","Zeit [s]","Position [m]"); //legend("mit anti-Windup","ohne anti-Windup",1); //xs2pdf(gcf(),'../Bilder/win_pos.pdf'); scf(6); clf(6); Phi1 = phi1(stoe_anfang:stoe_ende); plot2d(T1,Phi1,2) xtitle("Winkel des pendels","Zeit [s]","Winkel [rad]"); //legend("mit anti-Windup","ohne anti-Windup",1); //xs2pdf(gcf(),'../Bilder/win_win.pdf'); scf(7); clf(7); V1 = v1(stoe_anfang:stoe_ende); plot2d(T1,V1,2) xtitle("Geschwindigkeit des Wagens","Zeit [s]","Geschwindigkeit [m/s]"); //legend("mit anti-Windup","ohne anti-Windup",1); //xs2pdf(gcf(),'../Bilder/win_gesch.pdf'); scf(8); clf(8); Phi_soll1 = phi_soll1(stoe_anfang:stoe_ende); plot2d(T1,Phi_soll1,2) xtitle("Referenzwinkel","Zeit [s]","Winkel [rad]"); //legend("mit anti-Windup","ohne anti-Windup",1); //xs2pdf(gcf(),'../Bilder/win_ref.pdf'); scf(4); clf(4); plot2d(T1,Phi1,2)//,rect=[5,-0.55,30,-0]) plot2d(T1,Phi_soll1,5)//,rect=[5,-0.55,30,-0]) xtitle('Winkel','Zeit [s]','Winkel [rad]'); legend('Winkel des Pendels','Referenzwinkel',4); //xs2pdf(gcf(),'../Bilder/win_win_ref.pdf'); // --- pdf abspeichern --- // //xs2pdf(5,'../Bilder/win_pos.pdf'); //xs2pdf(6,'../Bilder/win_win.pdf'); //xs2pdf(7,'../Bilder/win_gesch.pdf'); //xs2pdf(8,'../Bilder/win_ref.pdf'); //xs2pdf(4,'../Bilder/win_win_ref.pdf');
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//Chapter2 //Page.No-46, Figure.No-2.10 //Example_2_2_a //Output voltage for inverting amplifier //Given: clear;clc; vin=20*10^-3; // Input voltage in volts A=200000; // Voltage gain vo=-(A*vin); // Output voltage in volts printf("\n Output voltage is vo = %.f V \n",vo) // Result
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clear all clc f=input('Enter frequency in Hz:') t=0:0.0001:1 x1=cos(2*%pi*f*t); x2=cos(2*%pi*(2*f)*t) message=[]; carrier1=[]; carrier2=[]; I=input('Enter binary data:') for i=1:length(I) if(I(i))==1 m_s=ones(1,length(t)); else m_s=zeros(1,length(t)); end message=[message,m_s]; carrier1=[carrier1,x1] carrier2=[carrier2,x2] end fsk=[]; for n=1:length(I) if(I(n)==1) fsk=[fsk,x2]; else fsk=[fsk,x1] end end subplot(4,1,1); plot(message); xtitle('Message Signal'); xlabel('Time---->'); ylabel('Amplitude--->'); subplot(4,1,2); plot(carrier1); xtitle('Carrier Signal'); xlabel('Time---->'); ylabel('Amplitude--->'); subplot(4,1,3); plot(fsk); xtitle('Modulated Signal'); xlabel('Time---->'); ylabel('Amplitude--->'); //demodulation xdemod1=[]; xdemod2=[]; demod=[]; xdemod1=fsk.*carrier1; xdemod2=fsk.*carrier2; xdemod=xdemod2-xdemod1; for i=1:length(I) if i==1 s=sum(xdemod(1:length(t))) else s=sum(xdemod((i-1)*length(t):i*length(t))) end if(s>0) demod=[demod,zeros(1,length(t))] else demod=[demod,ones(1,length(t))] end end subplot(4,1,4); plot(demod); xtitle('DeModulated Signal'); xlabel('Time---->'); ylabel('Amplitude--->');
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<?xml version="1.0" encoding="utf-8"?> <test> <description>Double Bifurcation, P=5</description> <executable>PulseWaveSolver</executable> <parameters>TwoBifurcations.xml</parameters> <files> <file description="Session File">TwoBifurcations.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="A" tolerance="1e-12">96.2931</value> <value variable="u" tolerance="1e-12">11.9121</value> </metric> <metric type="Linf" id="2"> <value variable="A" tolerance="1e-12">6.31075</value> <value variable="u" tolerance="1e-12">6.15717</value> </metric> </metrics> </test>
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function dayDateTime() today = datenum(); [dayNumber,dayString] = weekday(today,'long'); mprintf("\nToday is %s, the %dth day of the week.\n", dayString, dayNumber); mprintf("The date is: %s\n", date()); t = clock(); mprintf("The time is: %d:%d:%d\n",t(4), t(5), t(6)); endfunction dayDateTime()
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//example 4.12. clc disp("From the given information we can write,") disp(" A = -16*10^6/j*omega and beta = 10^3/[2*10^3+j*omega]^2") disp("To verify the Barkhausen condition means to verify whether |A*beta| = 1 at a frequency for which A*beta = 0 degree. Let us express, A*beta in its rectangluar form.") disp(" A*beta = -16*10^6*10^3 / j*omega*[2*10^3+j*omega]^2 = -16*10^9 / j*omega*[4*10^6+4*10^3*j*omega+(j*omega)^2]") disp(" = -16*10^9 / j*omega*[4*10^6+4*10^3*j*omega-omega^2] as j*2 = -1") disp(" = -16*10^9 / 4*10^6*j*omega+4*10^3*j^2*omega^2-j*omega^3]") disp(" = -16*10^9 / j*omega*[4*10^6-omega^2]-[omega^2*4*10^3]") disp("Rationalising the denominator function we get,") disp(" A*beta = -16*10^9[-omega^2*4*10^3 - j*omega*[4*10^6-omega^2]] / [-[omega^2*4*10^3]-j*omega*[4*10^6-omega^2]]*[-omega^2*4*10^3 - j*omega*[4*10^6-omega^2]]") disp("Using (a-b)(a+b) = a^2 - b^2 in the denominator,") disp(" A*beta = 16*10^9[omega^2*4*10^3+j*omega*[4*10^6-omega^2]] / [-omega^2*4*10^3]^2 - [j*omega*[4*10^6-omega^2]^2") disp(" A*beta = 16*10^9[omega^2*4*10^3+j*omega*[4*10^6-omega^2]] / 16*10^6*omega^4 + omega^2(4*10^6-omega^2)^2") disp("Now to have A*beta = 0 degree, the imaginary part of A*beta must be zero. This is possible when,") disp("Therefore, omega*(4*10^6 - omega^2) = 0") disp("Therefore, omega = 0 or 4*10^6 - omega^2 = 0") disp("Therefore, omega^2 = 4*10^6 Neglecting zero value of frequency") disp("Therefore, omega = 2*10^3 rad/sec") disp("At this frequency |A*beta| can be obtained as,") disp(" |A*beta| = 16*10^9[4*10^3*omega^2] / 16*10^6*omega^4+omega^2[4*10^6-omega^2]^2 at omega = 2*10^3") ab=(2.56*10^20)/(2.56*10^20) disp(ab," |A*beta| =") disp("Therefore, At omega = 2*10^3 rad/sec, A*beta = 0 degree as imaginary part is zero while |A*beta| = 1. Thus Barkhausen Criterion is satisfied.") disp("The frequency at which circuit will oscillate is the value of omega for which |A*beta| = 1 and A*beta = 0 degree at the same time") disp("i.e. omega = 2*10^3 rad/sec") disp("But omega = 2*pi*f") f=(2*10^3)/(2*%pi) // in Hz format(9) disp(f,"Therefore, f(in Hz) = omega / 2pi =")
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nc = 0.87; nt = 0.9; T1 = 311; rp = 8; // P2/P1 P1 = 1; P2 = 8; P3 = 0.95*P2; P4 = 1; g = 1.4; cv = 0.718; cp = 1.005; R = 0.287; // With no cooling T2s = T1*((P2/P1)^((g-1)/g)); T2 = T1 + (T2s-T1)/0.87; T4s = T3*(P4/P3)^((g-1)/g); n = (((T3-T4s)*nt)-((T2s-T1)/nc))/(T3-T2); // With cooling n_cycle = n-0.05; x = 0.13; r = 0.13/1.13; disp("%",r*100,"Percentage of air that may be taken from the compressor is")
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function [Q, T]=Questao3(A) //extrai dimensoes [l,c] = size(A) //tira o mínimo e armazena em p p=min(l,c) //inicia a matriz Q como identidade Q=eye(l,l) // e = eye(l,l) for k=1:p-1 //pega o vetor coluna de A x=A(k:l,k) //calcula v a partir da expressão abaixo v = x+(sign(x(1)))*norm(x)*e(1:l-k+1,1) //normaliza v v = v/norm(v) //P é a matriz de householder P = eye(l-k+1, l-k+1) - 2*(v*v')/(v'*v) //Qk é a matriz Q na iteração K Qk= [eye(k-1,k-1),zeros(k-1,l-k+1);zeros(l-k+1,k-1),P] //iterações A=Qk*A Q=Qk*Q end Q=Q' T=A endfunction
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Undefined index: service Неизвестный индекс под названием 'service' в массиве
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//chapter 4 //broadside array printf("\n"); n=4; lamda=0.1 d=0.5 i=0.25 Rrad=73; //part a Prad=n*(i^2*Rrad); printf("the radiated power is %gW",Prad); //part b L=n*d; printf("\nthe length is %dm",L); BWFN=2*lamda/L; HPBW=BWFN/2; printf("\nthe Beam width first null is %g radians",BWFN); printf("\nthe half power beam width is %g radians",HPBW);
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clc(); clear; // To determine e/m ratio //e/m=(deltalambda*4*pi*c)/(B*(lambda)^2) deltalambda=0.01*10^-9; //Zeeman shift c=3*(10^8); //speed of light in vacuum in m/s B=0.78; //magnetic field lambda=550*(10^-9); //wavelength in nm Y=(deltalambda*4*(%pi)*3*(10^8))/(B*(lambda)^2) //e/m ratio printf("e/m =%e",Y);
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*************************************************** * Run the following command to create the queues * * runmqsc <queue manager name> <TESTNODE_qmgr_default.tst * *************************************************** DEFINE QL('BACKEND1')
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clear //T < +∞ exec('C:\Users\Julien Guégan\Documents\Cours\MAM4\STAGE\2 cohorts\Tfini\Fonctions 2 cohorts - T fini.sci',-1) T = 40 t = 0:T // CI M01 = 400 M02 = 400 n1 = 100 n2 = 1 n = n1+n2 Mee = fsolve(0,eqnM) τee = fsolve(0,list(lambda,Mee)) disp(" M** = "+string(Mee)+" , τ** = "+string(τee)) gagnants = [] //on stock les Mσ gagnants perdants = [] //les perdants egalité = [] //on stock quand il y a egalité tic() stepM = 10 Mσ = 1700:stepM:2100 load("C:\Users\Julien Guégan\Documents\Cours\MAM4\STAGE\2 cohorts\Tfini\Trade-Off\tradeoff_save",'tradeoff_τ','tradeoff_M','Metoileμγ','τetoileμγ') scf() x = tradeoff_M plot(x, tradeoff_τ,'b-','thickness',3) plot(Metoileμγ,τetoileμγ,'k.') ylabel('$τ*$','fontsize',4) xlabel('$M*$','fontsize',4) title('$Compromis\ Evolutif$','fontsize',3) hm = stepM for Mx = 1:length(Mσ) disp('M1σ = '+string(Mσ(Mx))) for My = 1:length(Mσ) n1 = 100 n2 = 1 M1σ = Mσ(Mx) index = find(x == M1σ) τ1σ = tradeoff_τ(index) M2σ = Mσ(My) index = find(x == M2σ) τ2σ = tradeoff_τ(index) M = ode("stiff",[M01;M02;800;800],0,t, syst_dyn) J1 = M(3,length(t)) J2 = M(4,length(t)) n11 = (n1*J1*n)/(n1*J1+n2*J2) n21 = (n2*J2*n)/(n1*J1+n2*J2) s(Mx,My) = n21/n2 if ((100-n11) > 0) then gagnants = [gagnants M2σ] perdants = [perdants M1σ] else //sinon M1 augmente donc on le garde gagnants = [gagnants M1σ] perdants = [perdants M2σ] end end end disp("TIME = "+string(toc()/60)+" min") scf() plot(perdants,gagnants,'r.') plot(gagnants,perdants,'b.') contour(Mσ,Mσ,s,20) plot(Mee,Mee,'k.')
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sce
builder_gateway_plsi.sce
gateway_path = get_absolute_file_path("builder_gateway_plsi.sce"); cur_path = pwd(); chdir(gateway_path); libname = 'openpr_plsi'; names = ['plsiread','int_readdata'; 'plsitrain','int_plsitrain']; files = (listfiles(['*.cpp']))' if ~MSDOS then hfiles = (listfiles('*.h'))'; files = [hfiles, files]; end tbx_build_gateway(libname, names, files, gateway_path); chdir(cur_path); clear libname names gateway_path files tbx_build_gateway cur_path;
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/2321/CH10/EX10.10.2/EX10_10_2.sce
0401fd99df6f6a18009c06f58e81ad8ec769780f
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
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Scilab
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1,024
sce
EX10_10_2.sce
//Example No. 10.10.2 clc; clear; close; format('v',7); tau=0.895;//scale factor sigma=0.166;//(spacing factor) fU=30;//MHz(Upper frequency) fL=10;//MHz(Lower frequency) c=3*10^8;//m/s(Speed of light) lambdaU=c/(fU*10^6);//m(Upper wavelength) lambdaL=c/(fL*10^6);//m(Lower wavelength) l1=lambdaU/2;//m(Length of shortest element) disp(l1,"Length of shortest element, l1 in meter is : "); l2=l1/tau;l3=l2/tau;l4=l3/tau;l4=l3/tau;l5=l4/tau;l6=l5/tau;l7=l6/tau;l8=l7/tau;l9=l8/tau;l10=l9/tau;l11=l10/tau;//m(Length of element) disp(l11,l10,l9,l8,l7,l6,l5,l4,l3,l2,"Other elements length(m) l2, l3, l4, l5, l6, l7, l8, l9, l10, l11 are : "); alfa=17.97;//degree(angle) R1=(l1/2)/tand(alfa/2);//m(Spacing between elements) R2=R1/tau;R3=R2/tau;R4=R3/tau;R4=R3/tau;R5=R4/tau;R6=R5/tau;R7=R6/tau;R8=R7/tau;R9=R8/tau;R10=R9/tau;R11=R10/tau;//m disp(R11,R10,R9,R8,R7,R6,R5,R4,R3,R2,R1,"Spacing between elements in meter R1, R2, R3, R4, R5, R6, R7, R8,R9, R10, R11 are : "); //Answer is not accurate in the book.
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449d555969bfd7befe906877abab098c6e63a0e8
/2471/CH3/EX3.6/Ex3_6.sce
dfd29dc9460bb307a381822d4346931f5b425cff
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
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sce
Ex3_6.sce
clear ; clc; // Example 3.6 printf('Example 3.6\n\n'); printf('Page No. 67\n\n'); // given P = 9000;// Capital Cost in Pound n = 5;// Project lifetime Less_dep = 8000;// Less Depreciation //For Project A d1 = [4500 3750 3000 1500 750 ]// Saving in every year (before depreciation) dT1 = sum (d1) Net_S1 = dT1- Less_dep;// Total Net Saving Avg1 = Net_S1/n;// Average net annual saving R_R1 = (Avg1/P)*100; //For Project d2 = [750 2250 4500 4500 1500 ]// Saving in every year (before depreciation) dT2 = sum (d2) Net_S2 = dT2- Less_dep;// Total Net Saving Avg2 = Net_S2/n;// Average net annual saving R_R2 = (Avg2/P)*100; printf('The percentage of Rate of Return on original investment for Project A is %3.1f \n',R_R1) printf('The percentage of Rate of Return on original investment for Project B is %3.1f \n',R_R2)
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/98/CH10/EX10.4/example10_4.sce
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FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
3
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null
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example10_4.sce
//Chapter 10 //Example 10_4 //Page 236 clear;clc; load_kw=15000; pf=0.8; r=1; vr=132; loss=0.05; i=load_kw*1000/sqrt(3)/vr/1000/pf; l_loss=loss*load_kw; r=l_loss*1000/3/i^2; l=r; printf("Line current = %.0f A \n\n", i); printf("Line losses = %.0f kW \n\n", l_loss); printf("R = %.2f ohm \n\n", r); printf("Length of the line = %.2f km \n\n", l);
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/1172/CH1/EX1.33/Example1_33.sce
39e8e534ab612fe1a961ebb33fb78358b3f1842f
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no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
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sce
Example1_33.sce
clc // Given That rotation=13.2// in degree conc=0.1// gram per cubic cm l=2// length of tube in dm //Sample Problem 33 Page No. 60 printf("\n # Problem 33 # \n ") printf(" \n Standard formula used \n delta=pi*d*del_mu/lambda \n") s= (rotation*(%pi/180))/ (l*conc) specific_rotation=s*180/%pi printf("Specific rotation of sample is %d degree. \n",specific_rotation)
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/779/CH18/EX18.2/18_2.sce
f635e7a25264baabcaf930c298f664e53b10b77a
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
3
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null
null
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665
sce
18_2.sce
P1 = 101.3e03; P4 = P1; // in Pa P2 = 8*P1; P3 = P2; T1 = 288; Vs = 2000; V3 = 100; Vc = V3; V1 = Vs + Vc ; n = 1.25; R = 287; V4 = ((P3/P4)^(1/n))*V3; W = ((n*P1*(V1-V4)*1e-06)/(n-1))*(((P2/P1)^((n-1)/n))-1); P = (W*800*0.001)/60 ; disp("kW",P,"Indicated poer is") disp("%",100*(V1-V4)/Vs,"Volumetric efficiency is") m = (P1*(V1-V4)*1e-06)/(R*T1); m_dot = m*800; disp("kg/min",m_dot,"Mass flow rate is") FAD = (V1-V4)*1e-06*800; disp("m3/min",FAD,"Free air delivery is") Wt = P1*(V1-V4)*1e-06*log(P2/P1); n_isothermal = (Wt*800*0.001)/(P*60); disp("%",100*n_isothermal,"Isothermal efficiency is") Pi = P/0.85; disp("kW",Pi,"Input power is")
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449d555969bfd7befe906877abab098c6e63a0e8
/3131/CH6/EX6.2/6_2.sce
eb970b62220bf0fad96923a42ca55b95cd6a9452
[]
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FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
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sce
6_2.sce
clear all; clc; disp("Ex 6_2") //Calculations // At joint C: //Applying summation of forces along all axes and equating them to zero //We get two equations and we solve for each component //Solving by matrix method to obtain solution disp("At joint C:") a1=30 a=a1*%pi/180 b1=45 b=b1*%pi/180 A=[-cos(a),sin(b);sin(a),-cos(b)] B=[0;-1.5] C=inv(A) D=C*B F_CD=D(1) F_CB=D(2) //Result printf('\n The values are ') printf('\n F_CD=%0.2f \n F_CB=%0.2f \n All values are in kN',F_CD, F_CB) disp("At joint D:") F_DA=4.10 printf('\n F_DA = %0.2f kN (T)', F_DA) F_DB=4.10 printf('\n F_DB = %0.2f kN (T)', F_DB)
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/Ford/ES-XW7T-1A278-AC 2003/14.0 Immunity from Transient Disturbances CI 220 0.tst
46628b5a4d25e6606e74f1eaf2155f18979dc2e7
[]
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CZPFOX/Standards
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af34157e6e447d1a2b39136b9f3734feb663d9bb
refs/heads/master
2020-06-18T12:58:06.033918
2019-07-11T02:55:42
2019-07-11T02:55:42
196,309,147
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tst
14.0 Immunity from Transient Disturbances CI 220 0.tst
<?xml version="1.0" encoding="UTF-8" standalone="yes"?> <AutoTestC version="2.0.0"> <Pulse>CUSTOM WAVE</Pulse> <Title>Pulse A1 Mode 1</Title> <Organization>Ford</Organization> <Standard>ES-XW7T-1A278-AC 2003</Standard> <Item>14.0 Immunity from Transient Disturbances CI 220</Item> <voltage>13</voltage> <count>1</count> <wave id="0"> <type>4</type> <dspin id="0">5</dspin> <dspin id="1">0</dspin> <dspin id="2">0.2</dspin> <spin id="0">10</spin> <spin id="1">0</spin> <comboindex id="0">0</comboindex> <time>120</time> <timeUnit>0</timeUnit> </wave> </AutoTestC>
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/TABELLE/src/results/stratPG-C.magic/.svn/text-base/result2s0.tst.svn-base
a1f134c9fdc0bd209488d9ecb20fdc269da1d8a1
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deepak0431/granada
fc9acf52590a1315805702af41d87760ef089545
077460440ded909242697d5f0fd1de8526c53ac6
refs/heads/master
2021-01-10T11:58:32.017549
2011-12-15T01:51:29
2011-12-15T01:51:29
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result2s0.tst.svn-base
@relation magic @attribute a1 real [4.2835, 334.177] @attribute a2 real [0.0, 256.382] @attribute a3 real [1.9413, 5.3233] @attribute a4 real [0.0131, 0.893] @attribute a5 real [3.0E-4, 0.6752] @attribute a6 real [-457.9161, 575.2407] @attribute a7 real [-331.78, 238.321] @attribute a8 real [-205.8947, 179.851] @attribute a9 real [0.0, 90.0] @attribute a10 real [1.2826, 495.561] @attribute a11 {g, h} @data g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g h g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g h g g g g g g g h g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g h g g g h g h g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g h g h g h g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g h g g g h g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g h g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g h g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g h g g g g g g g g g g g g g h g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g h g h g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g g h g g g g g g g g g g g g g g g g g g g g h h h g h h h h h h h h h h h h h g h h h h h g h h h g h g h h h g h h h h h h h h h h h h h h h h h h h h h h h g h h h h h h h h h g h g h g h g h h h g h h h g h g h h h g h h h h h g h g h h h g h h h g h h h h h h h h h h h g h g h h h g h h h g h g h g h h h g h h h g h g h g h g h g h h h h h g h h h g h h h g h h h h h h h g h g h h h g h g h h h g h h h g h h h h h h h h h h h g h g h h h h h g h g h h h g h h h h h g h h h h h h h g h g h g h g h h h g h h h h h g h g h h h h h h h g h h h h h h h g h h h h h h h g h h h g h h h g h h h g h g h h h g h h h h h h h h h g h g h h h h h h h h h h h h h h h g h h h g h g h g h h h h h h h h h h h h h h h h h h h h h h h h h h h h h h h g h g h g h g h g h h h h h g h g h h h g h g h g h h h h h h h h h h h h h h h h h g h h h g h g h g h h h h h h h h h h h h h g h g h h h g h g h g h h h g h g h h h g h h h h h h h g h g h h h h h g h h h h h h h h h g h h h h h h h h h g h g h g h g h h h g h g h h h g h h h h h g h g h h h g h g h h h h h h h h h h h h h h h g h h h h h h h g h h h h h g h g h h h g h g h g h g h h h g h h h g h h h h h g h h h g h h h g h h h h h h h g h h h g h h h h h h h g h h h h h g h g h h h h h g h g h h h h h g h g h h h g h g h h h g h g h g h h h h h h h h h h h h h g h h h g h h h h h g h h h h h h h h h g h h h h h h h h h g h g h h h h h g h h h g h h h h h h h h h g h h h h h g h h h g h g h g h h h h h g h g h h h h h h h h h g h g h h h h h h h h h g h g h g h g h h h h h h h h h h h h h h h h h g h g h h h h h h h h h h h h h g h g h h h g h g h g h g h g h h h h h h h h h h h g h g h g h h h h h g h g h h h h h h h g h g h h h g h 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clear;close();getd(".");getd("./kNN");getd("./RLG");getd("./RLG/Geometry");getd("./Pruning_strategy") //stance = [-2.3750e-1,-4.3146e-1,+1.9095e-2;-2.3750e-1,+4.3146e-1,+1.9097e-2;+2.3750e-1,-4.3146e-1,+1.9097e-2;+2.3750e-1,+4.3146e-1,+1.9095e-2]; stance = [-2.3750e-1,0,-4.3146e-1;-2.3750e-1,0,+4.3146e-1;+2.3750e-1,0,-4.3146e-1;+2.3750e-1,0,+4.3146e-1]; [a,b,c] = plane_ACP(stance); orig = floor(rand(1,3)*10); orig=c; //orig = [1,1,1]; //n = floor(rand(1,3)*10); n = a; [x,y,z] = rect3D(orig,n); //xtoproj = floor(rand(1,3)*10); xtoproj = [1 0 0]; xproj = projectionPlan(xtoproj,orig,n); //disp(cross(n,xproj-xtoproj)) //scatter3(xtoproj(1)*ones(1,2),xtoproj(2)*ones(1,2),xtoproj(3)*ones(1,2),50,'red'); //scatter3(xproj(1)*ones(1,2),xproj(2)*ones(1,2),xproj(3)*ones(1,2),50,'green'); alp=linspace(0,2*%pi,2*20); tet=linspace(0,%pi/2,20); rHS = 0.55+0.17; dirHS = [0 1 0]; ctLift = floor(rand(1,3)*50); [xHS,yHS,zHS]=halfSph(stance(1,:),rHS,alp,tet,dirHS); [xHS1,yHS1,zHS1]=halfSph(stance(2,:),rHS,alp,tet,dirHS)//+rand(1,3)); [xHS2,yHS2,zHS2]=halfSph(stance(3,:),rHS,alp,tet,dirHS)//+rand(1,3)); [xHS3,yHS3,zHS3]=halfSph(stance(4,:),rHS,alp,tet,dirHS)//+rand(1,3)); figure; scatter3(xHS,yHS,zHS,"markerEdgeColor", "black","markerFaceColor", [0 .8 .8]); scatter3(xHS1,yHS1,zHS1,"markerEdgeColor", "black","markerFaceColor", [.8 0 .8]); scatter3(xHS2,yHS2,zHS2,"markerEdgeColor", "black","markerFaceColor", [.8 0 0]); scatter3(xHS3,yHS3,zHS3,"markerEdgeColor", "black","markerFaceColor", [0 .8 0]); for i = 1:length(xHS) v = projectionPlan([xHS(i),yHS(i),zHS(i)],orig,n); xHS(i) = v(1);yHS(i) = v(2);zHS(i) = v(3); v = projectionPlan([xHS1(i),yHS1(i),zHS1(i)],orig,n); xHS1(i) = v(1);yHS1(i) = v(2);zHS1(i) = v(3); v = projectionPlan([xHS2(i),yHS2(i),zHS2(i)],orig,n); xHS2(i) = v(1);yHS2(i) = v(2);zHS2(i) = v(3); v = projectionPlan([xHS3(i),yHS3(i),zHS3(i)],orig,n); xHS3(i) = v(1);yHS3(i) = v(2);zHS3(i) = v(3); end xp = projectionPlan([1 0 0],orig,n); n = n/norm(n); //xp = xp/norm(xp); xp = (xp-orig); xp = xp/norm(xp); yp = cross(n,xp); R = [xp;yp;n]; for i = 1:length(xHS) v = R*([xHS(i);yHS(i);zHS(i)]-orig'); xHSp(i) = v(1);yHSp(i) = v(2);zHSp(i) = v(3); v = R*([xHS1(i);yHS1(i);zHS1(i)]-orig'); xHSp1(i) = v(1);yHSp1(i) = v(2);zHSp1(i) = v(3); v = R*([xHS2(i);yHS2(i);zHS2(i)]-orig'); xHSp2(i) = v(1);yHSp2(i) = v(2);zHSp2(i) = v(3); v = R*([xHS3(i);yHS3(i);zHS3(i)]-orig'); xHSp3(i) = v(1);yHSp3(i) = v(2);zHSp3(i) = v(3); end WSmiProj(:,:,1) = [xHSp';yHSp']'; WSmiProj(:,:,2) = [xHSp1';yHSp1']'; WSmiProj(:,:,3) = [xHSp2';yHSp2']'; WSmiProj(:,:,4) = [xHSp3';yHSp3']'; Cxy = computeCxy(WSmiProj,[1 0;0 1]); oo = R'*[Cxy.origin, 0]'+orig'; [xRect,yRect,zRect] = rect3D(oo',n,xp,yp,Cxy.length,Cxy.width); //plot3d(x,y,z); figure; plot3d(xRect,yRect,zRect); scatter3(xHS,yHS,zHS,"markerEdgeColor", "black","markerFaceColor", [0 .8 .8]); scatter3(xHS1,yHS1,zHS1,"markerEdgeColor", "black","markerFaceColor", [.8 0 .8]); scatter3(xHS2,yHS2,zHS2,"markerEdgeColor", "black","markerFaceColor", [.8 0 0]); scatter3(xHS3,yHS3,zHS3,"markerEdgeColor", "black","markerFaceColor", [0 .8 0]);
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//Chapter-3, Example 3.5, Page 111 //============================================================================= clc clear //INPUT DATA L1=0.25;//self inductance of coil in henry(H) N1=500;//no of turns of coil 1 N2=10500;//no of turns of coil 2 phi2=0.6*L1;//60 % of flux of first coil(m1) is linked with second coil(m2) z=100;//rate of change of current(dii/dt) in A/sec //CALCULATIONS x=L1/N1;//flux/ampere in first coil(phi1/I1) y=0.6*(x);//flux linking the second coil(phi2/I1) M=N2*(y);//mutual inductance between the two coils in H E=M*(z);//induced emf in V //OUTPUT mprintf("Thus the mutual inductance between two coils is %1.2f H \n",M); mprintf("The induced emf in second coil when current changes in first coil is %3.0f V \n",E); //=================================END OF PROGRAM==============================
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wtperct=0.5 Dwater=0.998 //g/cm^3 Dsulfuric=1.834 //g/cm^3
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clc // Given that E = 5e-19 // energy of photon in J h = 6.62e-34 // Planck constant in J-sec c = 3e8 // speed of light in m/sec e = 1.6e-19 // charge on an electron in C // Sample Problem 5 on page no. 14.21 printf("\n # PROBLEM 5 # \n") printf("Standard formula used \n") printf(" E = h*c/lambda \n") lambda = c * h / E printf("\n Wavelength is %f Angstrom.",lambda * 10^10)
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function y = ifftn(A, varargin) //Compute the inverse N-dimensional discrete Fourier transform of A using a Fast Fourier Transform (FFT) algorithm. //Calling Sequence //Y = ifftn(A) //Y = ifftn(A, size) //Parameters //A: Matrix //Description //Compute the inverse N-dimensional discrete Fourier transform of A using a Fast Fourier Transform (FFT) algorithm. The optional vector argument SIZE may be used specify the dimensions of the array to be used. If an element of SIZE is smaller than the corresponding dimension of A, then the dimension of A is truncated prior to performing the inverse FFT. Otherwise, if an element of SIZE is larger than the corresponding dimension then A is resized and padded with zeros. //Examples //ifftn([2,3,4]) //ans = // 3. - 0.5 - 0.2886751i - 0.5 + 0.2886751i funcprot(0); funcprot(0); rhs = argn(2) if(rhs<1 | rhs>2) error("Wrong number of input arguments."); end select(rhs) case 1 then y = callOctave("ifftn",A); case 2 then y = callOctave("ifftn",A, varargin(1)); end endfunction
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<scriptConfig name="RR" script="RR"> <params> <param name="invt.pretest_delay" type="int">0</param> <param name="rr.RRnorm_up_min" type="float">2.0</param> <param name="rr.MSARR" type="float">2.5</param> <param name="rr.t_dwell" type="float">3.0</param> <param name="comm.slave_id" type="int">5</param> <param name="invt.verification_delay" type="int">5</param> <param name="invt.posttest_delay" type="int">10</param> <param name="rr.Ilow" type="float">20.0</param> <param name="rr.Irated" type="float">100.0</param> <param name="rr.RRnorm_up_max" type="float">100.0</param> <param name="comm.baudrate" type="int">9600</param> <param name="comm.ifc_name" type="string">COM7</param> <param name="datatrig.dsm_method" type="string">Disabled - Data from EUT</param> <param name="datatrig.trigger_method" type="string">Disabled - Data from EUT</param> <param name="pvsim.mode" type="string">Manual</param> <param name="comm.parity" type="string">N</param> <param name="comm.ifc_type" type="string">RTU</param> </params> </scriptConfig>
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//Ex4_13 clc IDSS=10*10^(-3) disp("IDSS = "+string(IDSS)+" ampere") // maximum drain current for n-channel DEMOSFET ID=IDSS // since VGS=0V, so ID=maximum VP=(-4) disp("VP= "+string(VP)+" volts") // pinch off voltage VGS=(0) disp("VGS= "+string(VGS)+" volts") // Gate to source voltage VDD=(10) disp("VDD= "+string(VDD)+" volts") // Drain supply voltage RL=0.5*10^(3) disp("RL= "+string(RL)+ " ohm") //Load resistance VDS=VDD-ID*RL disp("VDS=VDD-ID*RL= "+string(VDS)+" volts") // Drain to source voltage ,since VDS>VP DEMOSFET is in pinch off disp("VDS>VP,so pinch off region") RL=0.75*10^(3) disp("RL= "+string(RL)+ " ohm") // New Load resistance value VDS=VDD-ID*RL disp("VDS=VDD-ID*RL= "+string(VDS)+" volts") // New Drain to source voltage for RL=750 ohm disp("VDS<VP,so ohmic region")// since VDS < VP DEMOSFET is in ohmic region for RL=750 ohm and hence will not operate as a current source
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f_am=10; fr_am=455; fr_fm=10.7; f_fm=0.2; q_am=fr_am/f_am; q_fm=fr_fm/f_fm; disp("for AM the necessary Q value is"); disp(q_am); disp("for FM the necessary Q value is"); disp(q_fm);
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// Scilab Code Ex10.8 Maximum height of the potential barrier for alpha penetration: Pg:222 (2008) epsilon_0 = 8.854e-12; // Absolute electrical permittivity of free space, coulomb square per newton per metre square Z = 92; // Atomic number of U-92 nucleus z = 2; // Atomic number of He nucleus e = 1.6e-019; // Charge on an electron, coulomb R = 9.3e-015; // Radius of residual nucleus, m U = 1/(4*%pi*epsilon_0)*Z*z*e^2/(R*1.6e-013); // Maximum height of potential barrier, MeV printf("\nThe maximum height of the potential barrier for alpha penetration = %2d MeV", U); // Result // The maximum height of the potential barrier for alpha penetration = 28 MeV
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*.*....*...**...*...*.....**.**.*...*...***...**... .*...***...**.*...**........*..**.*.....**.*....*.* *..*......*......*.*.*.*....*..*..**..........*.... *.*...*.....**.*.*....*...................*...*..*. .**..*....*.*..*.*..*.*...**......*.*...*.........* .*...*.*......**.......**.*..**....**.**.*........* ...***..*..*..***..*.....***..*.......*.*..*....*** .***.*....**..**..*....*...*........***.*...****..* .*.*....*.*..*.**...*..*..*..*..*..*.*.*..*........ ..**.*.*..*.......*.*.*.**....*..*.***...***..**.*. *..*.......*..***........*.**.........*.**.**...... *.*.....**..*.*......*....*...*....**.*.*..*..*.... *.*..*.....*.**....*.*...***..*.**.*.......*.*.**.. ..*....*.**...*.**.......*.*...**.....*.*...**..... *.......***..**..*.....*....*...**..*.****.....**.* ...*.*...*...*..*....**..*.*.**....***.......****.. ..*.*.*.*...*......*.*.*.*..*.......*....*...*.*... .*....*...**......**...*.*..*.*...*.**..*..*..**... 0 0
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449d555969bfd7befe906877abab098c6e63a0e8
/1208/CH4/EX4.14.4/Exa14_4.sce
9399f1286b096e35959091780c1ad912da1424a5
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
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Exa14_4.sce
//Exa 14(iv) clc; clear; close; //given data : inINV=50000;//initial investment in Rs. and equal for all projects life=5;//in years salvage=0;//in Rs. TaxRate=55;//in % //depreciation type :Straight line D=inINV/life;//in Rs //cash flows before tax of 1st,2nd,3rd,4th and 5th years CBFT1=10000;//in Rs. CBFT2=11000;//in Rs. CBFT3=14000;//in Rs. CBFT4=15000;//in Rs. CBFT5=25000;//in Rs. //Income before tax after depreciation IBT1=CBFT1-D;//in Rs. IBT2=CBFT2-D;//in Rs. IBT3=CBFT3-D;//in Rs. IBT4=CBFT4-D;//in Rs. IBT5=CBFT5-D;//in Rs. //Net income after Tax (55%) and depreciation IATD1=IBT1-(IBT1*55)/100;//in Rs IATD2=IBT2-(IBT2*55)/100;//in Rs IATD3=IBT3-(IBT3*55)/100;//in Rs IATD4=IBT4-(IBT4*55)/100;//in Rs IATD5=IBT5-(IBT5*55)/100;//in Rs //Average annual income after tax and depreciation IATD=(IATD1+IATD2+IATD3+IATD4+IATD5)/5;//in Rs. //Average Investment AvgInv=(inINV+salvage)/2;//in Rs //Annual cash inflows ACI1=IATD1+D;//in RS ACI2=IATD2+D;//in RS ACI3=IATD3+D;//in RS ACI4=IATD4+D;//in RS ACI5=IATD5+D;//in RS //P.V factor at 10% rate of discount PV1=0.909; PV2=0.826; PV3=0.751; PV4=0.683; PV5=0.621; //Present value for all cash in flows at 10% discount Rate P1=ACI1*PV1;// in Rs P2=ACI2*PV2;// in Rs P3=ACI3*PV3;// in Rs P4=ACI4*PV4;// in Rs P5=ACI5*PV5;// in Rs //Total Present Value P=P1+P2+P3+P4+P5;// in Rs //Project A : Cummulative cash in flows of 1st,2nd,3rd,4th and 5th years CumCIF1=ACI1;//in Rs. CumCIF2=ACI1+ACI2;//in Rs. CumCIF3=ACI1+ACI2+ACI3;//in Rs. CumCIF4=ACI1+ACI2+ACI3+ACI4;//in Rs. CumCIF5=ACI1+ACI2+ACI3+ACI4+ACI5;//in Rs. //part (iv) Profitability index at 10% discount rate PI=P/inINV;//unitless disp(PI,"Part(iv) Profitability index at 10% discount rate : ");
fd5174e2b559ddd867eb4873a1a109e113a8067a
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/test/calls.tst
b23210416447b6b565cf09e63f698daaaf9ef5e3
[]
no_license
goldenpartner/Assignment1
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refs/heads/master
2021-01-12T11:54:30.972457
2016-10-18T03:33:30
2016-10-18T03:33:30
69,310,866
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calls.tst
ADD s0, 01 OUTPUT s0, 00 loop: CALL NZ, loop OUTPUT sF, 00 death: JUMP death
68e26ea57490618dcfcc4e7eaa269f04ea465d6f
8217f7986187902617ad1bf89cb789618a90dd0a
/browsable_source/2.2/Unix/scilab-2.2/macros/percent/%lsslp.sci
fdc1e885d94115e3389185cc3c9cd0688997948f
[ "LicenseRef-scancode-warranty-disclaimer", "LicenseRef-scancode-public-domain", "MIT" ]
permissive
clg55/Scilab-Workbench
4ebc01d2daea5026ad07fbfc53e16d4b29179502
9f8fd29c7f2a98100fa9aed8b58f6768d24a1875
refs/heads/master
2023-05-31T04:06:22.931111
2022-09-13T14:41:51
2022-09-13T14:41:51
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%lsslp.sci
function [sr]=%lsslp(s,p) //sr=%lsslp(s,p) <=> sr=s\p // p matrice de polynomes // s representation d'etat d'un systeme lineaire //! //origine S Steer INRIA 1992 sr=s\tlist('lss',[],[],[],p,[],[])
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449d555969bfd7befe906877abab098c6e63a0e8
/409/CH25/EX25.10/Example25_10.sce
51da40c191d09d8f25043e10da2f85a3b2e3c8f2
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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clear ; clc; // Example 25.10 printf('Example 25.10\n\n'); //page no. 788 // Solution // Given Ex_hv = 29770.0 ;// Experimental heating value of given coal - [kJ/kg] // Coal analysis C = 71.0/100 ;//Fraction of C in coal H2 = 5.6/100 ;// Fraction of H2 in coal N2 = 1.6/100 ;// Fraction of N2 in coal S = 2.7/100 ;// Fraction of S in coal ash = 6.1/100 ;// Fraction of ash in coal O2 = 13.0/100 ;//Fraction of O2 in coal //Higher heating value (HHV) by Dulong formula HHV = 14544*C + 62028*(H2 - O2/8) + 4050*S ;// Higher heating value (HHV) by Dulong formula -[Btu/lb] HHV_SI = HHV *1.055/0.454 ;// HHV in SI unt - [kJ/kg] printf('The experimental heating value - %.0f kJ.\n',Ex_hv) ; printf(' Higher heating value (HHV) by Dulong formula - %.0f kJ.\n',HHV_SI) ; printf('\n The two values are quite close.' ) ;
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clc //initialization of variables clear b=2 //cm h=2 //cm T=2000 //kg-cm V=250 //kg M=2000 //kg-cm // calculations Mmax=M*6/(b*h*b) Vmax=3*V/(2*b*h) Zt=0.208*b^2*h Tmax=T/(Zt) sigma=Mmax printf('points A,B,') printf('\n sigma=%d kg/cm^2 (tension)',sigma) printf('\n points C,D,') printf('\n sigma=%d kg/cm^2 (cmpression)',sigma) tau=Vmax+Tmax printf('\n point E') printf('\n tau=%.2f kg/cm^2 shear',tau) tau=Vmax-Tmax printf('\n tau=%.2f kg/cm^2 shear',tau) // at G sigma_x=sigma sigma_y=0 tau_xy=Tmax sigma_1=(sigma_x+sigma_y)/2+sqrt((1/2*(sigma_x-sigma_y))^2+tau_xy^2) sigma_2=(sigma_x+sigma_y)/2-sqrt((1/2*(sigma_x-sigma_y))^2+tau_xy^2) // results printf('\n at point G') printf('\n sigma_1 = %d kg/cm^2 (tension)',sigma_1) printf('\n sigma_2 = %d kg/cm^2 (compression)',sigma_2) // Question was asked only to find out at A,B,C,D,E,F and G
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//Introduction to Fiber Optics by A. Ghatak and K. Thyagarajan, Cambridge, New Delhi, 1999 //Example 2.4 //OS=Windows XP sp3 //Scilab version 5.5.2 clc; clear; //given Case(1) n1=1;//refractive index of air n2=1.45;//refractive index of silica R=[(n1-n2)/(n1+n2)]^2;//corresponding energy reflection coefficient mprintf("Energy reflection coefficient for air-silica interface=%.2f",R); //given Case(2) n1=1;//refractive index of air n2=3.6;//refractive index of GaAs R=[(n1-n2)/(n1+n2)]^2;//corresponding energy reflection coefficient mprintf("\n Energy reflection coefficient for GaAs-air interface=%.2f",R);
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clc //calc thickness of liquid strip at the bottom of the industrial centrifuge //Let difference between heights at bottom and top be d d=20;//in r_a=14;//in f=1000/60;//rps g=32.2;//ft/s^2 r_b=[(r_a)^2-2*(d)*g*12/(2*(%pi)*f)^2]^0.5;//in disp("The thickness of water strip at bottom of industrial centrifuge") disp(r_b) disp("in")
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import {StagePhaser} from "../phasers/StagePhaser"; import MathJs from 'mathjs'; import {Position} from "../../../../../blacksheep-geometry/lib"; import { Parameter } from "../../../Parameter"; export class GoldenRectanglePositioner { speed: Parameter; distance: Parameter; center: Position; stagePhaser: StagePhaser; myPhi: number; currentSize: number; currentPosition: Position; previousPosition: Position; previousPositionStartCorner : Position; constructor( speed : Parameter, distance : Parameter, center : Position, stagePhaser : StagePhaser ){ this.speed = speed; this.distance = distance; this.center = center; this.stagePhaser = stagePhaser; this.myPhi = MathJs.phi; //We are setting phi here - so we can play around with change the value of it later. this.currentSize =0; this.reset(); } reset() { this.stagePhaser.reset(); this.currentSize = this.distance.getValue(); this.currentPosition = new Position(this.center.x + this.currentSize * this.myPhi /2, this.center.y - this.currentSize/2); this.previousPosition =new Position( this.center.x + this.currentSize * this.myPhi /2, this.center.y - this.currentSize/2); //TODO: change this. To what? Jesus, this comment makes no sense } tick() { this.stagePhaser.tick(); let subPhase = this.stagePhaser.getSubPhase(); let previousSubPhase = this.stagePhaser.getPreviousSubPhase(); let stage = this.stagePhaser.getStage(); let subPhaseDiff, subPhaseDiffB; if (!this.stagePhaser.isOnCorner()) { subPhaseDiff = subPhase - previousSubPhase; } else { /*** This block sets the previousPositionStartCorner, and moves current position to the corner. Also, increases the value of currentSize */ subPhaseDiffB = 1 - previousSubPhase; subPhaseDiff = subPhase; this.previousPositionStartCorner = this.currentPosition.copy(); switch (stage) { case 0: this.currentPosition.update(this.currentPosition.x + subPhaseDiffB * this.currentSize, this.currentPosition.y); break; case 1: this.currentPosition.update(this.currentPosition.x, this.currentPosition.y + subPhaseDiffB * this.currentSize); break; case 2: this.currentPosition.update(this.currentPosition.x - subPhaseDiffB * this.currentSize, this.currentPosition.y ); break; case 3: this.currentPosition.update(this.currentPosition.x, this.currentPosition.y - subPhaseDiffB * this.currentSize); break; } this.currentSize = this.currentSize * this.myPhi; } this.previousPosition.updateFromPosition(this.currentPosition); switch(stage){ case 0: this.currentPosition.update(this.currentPosition.x, (this.currentPosition.y + subPhaseDiff * this.currentSize)) ; break; case 1: this.currentPosition.update(this.currentPosition.x - (subPhaseDiff * this.currentSize), this.currentPosition.y ); break; case 2: this.currentPosition.update(this.currentPosition.x, this.currentPosition.y - (subPhaseDiff * this.currentSize)) ; break; case 3: this.currentPosition.update(this.currentPosition.x + (subPhaseDiff * this.currentSize), this.currentPosition.y ); break; } } //Return a single position getPosition() : Position { return this.currentPosition; } getPreviousPosition() : Position{ return this.previousPosition; } getStartCorner() : Position { return this.previousPositionStartCorner; } getMyPhi() : number{ return this.myPhi; } }
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function y = qei_sim2(u1) in = u1; out = u1; out = modulo(in, 2*%pi); out = out * (500/%pi); y = out; endfunction
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//Example 4_17 clc(); clear; //To find the lattice parameter of Lead lemda=1.5*10^-10 //units in meters theta=34 //units in degrees n=1 h=2 k=0 l=2 a=(n*lemda)/(2*sin(theta))*sqrt(h^2+k^2+l^2)*10^10 printf("the lattice parameter of the Lead is %.3f angstrom",a)
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V=11;Phase=3;F=60;IncExe=150;DecExe=50;Xs=10; Power=80000; Vt=V/sqrt(Phase) Vt=Vt*1000 Ef=IncExe/100 Ef1=DecExe/100 Ia=(Vt-(Ef*Vt))/(Xs) Pf=cos(90/90*%pi/2) Ia1=(Vt-(Ef1*Vt))/(Xs) Pf1=cos(90/90*%pi/2) Ia=Power/(Phase*Vt) function[x,y]=polar2rect(r,theta) x=r*cos(theta*%pi/180); y=r*sin(theta*%pi/180); endfunction [x1,y1]=polar2rect(4.2,0) [x2,y2]=polar2rect(10,90) X1=x1+%i*y1 X2=x2+%i*y2 X=X1*X2 function[r,theta]=rect2polar(x,y) r=sqrt(x^2+y^2); theta=atan(y/x)*180/%pi; endfunction [a,b]=rect2polar(Vt,42)
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//Variable Declaration p1=0.87 // probability of Repair on the engine p2=0.36 // probability of drive train p3=0.29 // probability of rapair as well as drive train //Calculation P = p1+p2-p3 // Required probability //Results printf ( "probability of at least one kind of repair: %.2f",P)
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//chapter 21 Ex 8 clc; clear; close; SI=4/9; rate=sqrt(SI*100); t=rate; //since both are numerfically equal mprintf("The rate is %.2f percent and the time is %.2f years",rate,t);
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clc,clear printf('Example 5.21\n\n') V_ph=2000 R_a=0.8 I_sc=100,I_a=I_sc V_OC=500 I_f=2.5 Z_s=V_OC/I_sc X_s=sqrt(Z_s^2- R_a^2) I_a_FL=100 //Part(i) phi1=acos(1) //and lagging E_ph1=sqrt((V_ph*cos(phi1)+I_a*R_a)^2+(V_ph*sin(phi1)+I_a*X_s)^2) regulation1=100*(E_ph1-V_ph)/V_ph printf('Regulation at upf is %.2f percent\n',regulation1) //Part(ii) phi2=acos(0.8) E_ph2=sqrt((V_ph*cos(phi2)+I_a*R_a)^2+(V_ph*sin(phi2)-I_a*X_s)^2) regulation2=100*(E_ph2-V_ph)/V_ph printf('Regulation at 0.8 leading pf is %.2f percent\n',regulation2) //Part(iii) phi3=acos(0.71) E_ph3=sqrt((V_ph*cos(phi3)+I_a*R_a)^2+(V_ph*sin(phi3)+I_a*X_s)^2) regulation3=100*(E_ph3-V_ph)/V_ph printf('Regulation at 0.71 lagging pf is %.2f percent\n',regulation3)
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//Chapter 3 : Systems of Linear Equations //Example 3.22 //Scilab 6.0.1 //Windows 10 clear; clc; A=[1 2 0 0; 2 1 -1 1; 5 4 -2 2]; disp(A,'A=') mprintf('the rows of the matrix are linearly dependent\n') t=A(1,:)+2*A(2,:); mprintf('this follows from the fact that\n') mprintf('A3=A1+2A2') disp(t)
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//scilab 5.4.1 clear; clc; printf("\t\t\tProblem Number 7.23\n\n\n"); // Chapter 7 : Mixtures Of Ideal Gases // Problem 7.23 (page no. 358) // Solution //The cooling tower //From the Steam tables, //For water: h100F=68.05; //Btu/lbm //enthalpy at 100 F h70F=38.09; //Btu/lbm //enthalpy at 70 F //For air: h=20.4; //Unit:Btu/lb //at inlet,total heat/lb dry air w=38.2; //Unit:grains/lb //at inlet,moisture pickup/lb dry air (at 60F D.B. and 50% R.H.) H=52.1; //Unit:Btu/lb //at outlet,total heat/lb dry air W=194.0; //Unit:grains/lb //at outlet,moisture pickup/lb dry air (at 90F D.B. and 90% R.H.) //Per pound of dry air,the heat interchange is H-h Btu per pound of dry air. //Per pound of dry air,the moisture increase is (W-w)/7000 lb per pound of dry air. //From the equation, ma*(H-h) = 200000*h100F - mwout*h70F //ma=mass of air mwout=mass of cooled water //and ma*((W-w)/7000) = 200000 - mwout //Solving the latter equation for mwout,we have mwout=200000-(ma*((W-w)/7000)) //Substituting this into the heat balance yields, // ma*(H-h) = 200000*h100F - 200000*h70F + ma*h70F*((W-w)/7000) //Solving gives us, ma=(200000*(h100F-h70F))/((H-h)-(h70F*((W-w)/7000))); //The amount of air required per hour //Unit:lbm/hr of dry air printf("The amount of air required per hour is %f lbm/hr of dry air\n",ma); printf("The amount of water lost per hour due to evaporation is %f lbm/hr\n",ma*((W-w)/7000)); //note that the water evaporated is slightly over 2% of the incoming water,and this is the makeup that has to be furnished to the tower. //answer are slightly differ because of value of (W-w)/7000 is given 0.0233 instead of 0.0225
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function data = mdaq_ai_read(link_id, channels, ai_range, bipolar) data = []; if argn(2) <> 4 then disp("ERROR: Wrong input arguments!"); return; end if link_id < 0 then disp("ERROR: Wrong link ID!") return; end ch_count = max(size(channels)); if ch_count < 1 | ch_count > 8 then disp("ERROR: Wrong AI channel setup!") return; end if max(channels) > 8 then disp("ERROR: Wrong AI channel setup!") return; end result = []; [data result] = call("sci_mlink_ai_read",.. link_id, 1, "i",.. channels, 2, "i",.. ch_count, 3, "i",.. ai_range, 4, "i",.. bipolar, 5, "i",.. "out",.. [1, ch_count], 6, "d",.. [1, 1], 7, "i"); if result < 0 then mdaq_error(result); end endfunction
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// Ex 75 Page 414 clc;clear;close; // Given Ebb=400;//V Emm=250;//V Ibb=25;//A Po=2.5*10**3;//W m=Emm/Ebb;//modulation index Pbb=Ebb*Ibb eta=Po/Pbb*100;//% P=Po*(1+m**2/2);//W Pdo=Pbb-Po;//W Pd=Pdo*(1+m**2/2);//W printf("\n carrier power under modulated condition = %0.2f kW",P/1000) printf("\n plate circuit efficiency = %.f percent",eta) printf("\n plate dissipation under unmodulated condition = %.1f kW",Pdo/1000) printf("\n plate dissipation under modulated condition = %.2f kW",Pd/1000)
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//Finding resistance and cost //Example 15.39(pg. 418) clc clear m=2//weight of water to be heated in kg t2=98,t1=15//temp in degreeC s=1//specific heat of water V=200//voltage in volts H=m*s*(t2-t1)//energy required to raise the temp of water in kcal H1=H*4200//energy in Watt-sec or Joules e=0.85//efficiency of kettle E=H1/e//energy input required in watt-sec E1=E/(1000*3600)//energy input in kWh c=35//cost per unit in paise C=c*E1//ocst of energy used in paise t=10/60//time in hrs W=E1*1000/t//wattage of kettle in watts R=V*V/W//resistance of heating element in ohms printf('Thus the resistance of heating element is %2.0f ohms\n',R) printf('And the cost of energy used is %2.0f paisa',C)
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function Px = poly_Gregory_Newton(varargin) // // Polinomio de Gregory-Newton usando dispositivo pratico // // parametros de entrada: // x: vetor contendo as abscissas, // y: vetor contendo as ordenadas, // [Exibe]: Parâmetro opcional de exibição da tabela de Dif. finitas // // parametro de saida: // Px: polinômio interpolador // // Processa parâmetros [lhs,rhs]=argn(); if rhs < 2 then error('Número insuficiente de argumentos: informe os vetores x e y'); end x = varargin(1); y = varargin(2); if rhs >= 3 then Exibe = varargin(3); else Exibe = %F; end n = length(x); if n < 2 then error('Poucos pontos (<2) para interpolar'); end eps = 0.0000000001; space = abs(x(2) - x(1)); for i = 2:n if abs(abs(x(i) - x(i-1)) - space) > eps then error('O método de Gregory-Newton exige espaçamento igual'); end end // Inicializa a matriz de diferenças finitas for i = 1:n Delta_y(i,1) = y(i); end // Construção das diferenças finitas for k = 2:n for i = 1:n-k+1 Delta_y(i,k) = Delta_y(i+1,k-1) - Delta_y(i,k-1); end end // Exibe a tabela if Exibe then mprintf('\nInterpolação via polinômios de Gregory-Newton\n') mprintf('\n Tabela de diferenças finitas') mprintf('\n i x(i) y(i) ') for j = 1:n-1 mprintf(' DifFin%i', j) end mprintf('\n') for i = 1:n mprintf('%3i %11.6f', i-1, x(i)) for j = 1:n+1-i mprintf(' %11.6f', Delta_y(i,j)) end mprintf('\n') end end // Geração do polinomio interpolador X = poly(0, 'x'); u = (X - x(1)) / (x(2)-x(1)); Px = Delta_y(1,n); for i = n-1:-1:1 Px = Px * (u - i + 1) / i + Delta_y(1,i); end; endfunction
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example_5_6.sce
//Chapter 5 //Example 5.6 //page 149 //to find incident and reflected voltages clear;clc; R=0.125; X=0.4; y=%i*2.8*10^(-6); z=R+%i*X; r=sqrt(y*z); //propogation constant a=real(r); //attenuation constant b=imag(r); //phase constant //(a) At the receiving-end; Vr=220000; Inci_vol=Vr/(sqrt(3)*2); Refl_vol=Vr/(sqrt(3)*2); printf('\n\nIncident Vvoltage=%0.2f kV',Inci_vol/1000); printf('\nReflected Vvoltage=%0.2f kV',Refl_vol/1000); //(b) At 200km from the receiving-end x=200; Inci_vol=Inci_vol*exp(a*x)*exp(%i*b*x); Refl_vol=Refl_vol*exp(-a*x)*exp(-%i*b*x); printf('\n\nIncident voltage=%0.2f @ %0.1f deg kV',abs(Inci_vol)/1000,atand(imag(Inci_vol)/real(Inci_vol))); printf('\nReflected voltage=%0.2f @ %0.1f deg kV',abs(Refl_vol)/1000,atand(imag(Refl_vol)/real(Refl_vol))); //(c) Resultant voltage at 200km from the receiving-end res=Inci_vol+Refl_vol; printf('\n\nResultant line-to-line voltage at 200km =%0.2f kV',abs(res)*sqrt(3)/1000);
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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: Rupak Rokade // Organization: FOSSEE, IIT Bombay mode(-1) lines(0) toolbox_title = "keras_toolbox"; Build_64Bits = %t; path_builder = get_absolute_file_path('builder_gateway_cpp.sce'); Function_Names = [ "ANN","sci_ANN","csci6"; "ANN_test","sci_ANN_test","csci6"; "image_train_tl","sci_image_train_tl","csci6"; "image_test_tl","sci_image_test_tl","csci6"; ]; //Name of all the files to be compiled Files = [ "sci_ANN.cpp"; "sci_ANN_test.cpp"; "sci_image_train_tl.cpp"; "sci_image_test_tl.cpp"; ] [a, opt] = getversion(); Version = opt(2); //Build_64Bits = %f; if getos()=="Windows" then third_dir = path_builder+filesep()+'..'+filesep()+'..'+filesep()+'thirdparty'; lib_base_dir = third_dir + filesep() + 'windows' + filesep() + 'lib' + filesep() + Version + filesep(); inc_base_dir = third_dir + filesep() + 'windows' + filesep() + 'include'; C_Flags=['-D__USE_DEPRECATED_STACK_FUNCTIONS__ -I -w '+path_builder+' '+ '-I '+inc_base_dir+' '] Linker_Flag = [lib_base_dir+"libraryname.lib "] elseif getos()=="Darwin" then //Mac third_dir = path_builder+filesep()+'..'+filesep()+'..'+filesep()+'thirdparty'; lib_base_dir = third_dir + filesep() + 'Mac' + filesep() + 'lib' + filesep() + Version + filesep(); inc_base_dir = third_dir + filesep() + 'Mac' + filesep() + 'include' ; C_Flags=["-D__USE_DEPRECATED_STACK_FUNCTIONS__ -w -fpermissive -I"+path_builder+" -I"+inc_base_dir+" -Wl,-rpath "+lib_base_dir+" "] Linker_Flag = ["-L"+lib_base_dir+" -lmul -Wl,-rpath="+lib_base_dir] else//LINUX third_dir = path_builder+filesep()+'..'+filesep()+'..'+filesep()+'thirdparty'; lib_base_dir = third_dir + filesep() + 'linux' + filesep() + 'lib' + filesep() + Version + filesep(); inc_base_dir = third_dir + filesep() + 'linux' + filesep() + 'include'; C_Flags = ["-I"+inc_base_dir]; Linker_Flag = ["-L" + lib_base_dir + " -lscikeras -lpython3.8 -Wl,-rpath="+lib_base_dir] end tbx_build_gateway(toolbox_title,Function_Names,Files,get_absolute_file_path("builder_gateway_cpp.sce"), [], Linker_Flag, C_Flags,[]); clear toolbox_title Function_Names Files Linker_Flag C_Flags;
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0.91893595 108.77778 96.333336 126.22222 103.77778 -37.333332 52.333332 -15.0 126.22222 0.2367968 -2.3554425 SKY 174.0 50.0 9 0.0 0.0 1.0000013 0.7601153 0.9444453 0.9525792 107.44444 94.666664 125.77778 101.888885 -38.333332 55.0 -16.666666 125.77778 0.2473368 -2.3372955 SKY 80.0 40.0 9 0.0 0.0 0.6111107 0.5741323 0.7222226 0.7722025 110.703705 96.22222 129.0 106.888885 -43.444443 54.88889 -11.444445 129.0 0.2540513 -2.4346924 SKY 67.0 71.0 9 0.0 0.0 1.6666666 0.8888911 1.4999987 0.29999846 125.96296 115.55556 140.88889 121.44444 -31.222221 44.77778 -13.555555 140.88889 0.17967218 -2.339758 SKY 92.0 56.0 9 0.0 0.0 0.44444275 0.029629406 0.8333333 0.5666677 126.0 115.888885 140.66667 121.44444 -30.333334 44.0 -13.666667 140.66667 0.17606053 -2.3267827 SKY 67.0 32.0 9 0.0 0.0 0.944444 1.0628421 1.7777786 1.3109215 126.22222 115.111115 142.22223 121.333336 -33.333332 48.0 -14.666667 142.22223 0.19062504 -2.333746 SKY 125.0 46.0 9 0.11111111 0.0 0.61110944 0.61161584 2.166668 0.7817352 124.55556 112.77778 141.0 119.888885 -35.333332 49.333332 -14.0 141.0 0.20012376 -2.357688 SKY 101.0 121.0 9 0.11111111 0.0 0.6666667 0.843274 1.5 0.88819396 3.4074075 1.1111112 6.0 3.1111112 -6.888889 7.7777777 -0.8888889 6.0 0.8435185 -2.5191648 FOLIAGE 21.0 122.0 9 0.0 0.0 0.44444445 0.4036867 0.44444445 0.4036867 0.5555556 0.0 1.2222222 0.44444445 -1.6666666 2.0 -0.33333334 1.2222222 0.5555556 -2.4445627 FOLIAGE 45.0 89.0 9 0.0 0.0 0.7777777 0.3407409 0.77777773 0.47407398 2.2962964 0.11111111 6.4444447 0.33333334 -6.5555553 12.444445 -5.888889 6.4444447 0.9861111 -2.1239047 FOLIAGE 18.0 87.0 9 0.0 0.0 1.5555555 1.9626132 1.8888887 1.7469552 2.925926 1.2222222 5.6666665 1.8888888 -5.111111 8.222222 -3.1111112 5.6666665 0.86277056 -2.2294934 FOLIAGE 52.0 102.0 9 0.0 0.0 0.72222227 0.50740725 0.8333333 0.5666668 2.8888888 0.6666667 6.3333335 1.6666666 -6.6666665 10.333333 -3.6666667 6.3333335 0.89973545 -2.2617195 FOLIAGE 54.0 91.0 9 0.0 0.0 1.4444443 1.540741 0.8333333 0.25555572 3.2592592 0.5555556 8.0 1.2222222 -8.111111 14.222222 -6.111111 8.0 0.94481075 -2.186723 FOLIAGE 80.0 87.0 9 0.0 0.11111111 24.388891 572.9964 44.722225 1386.3292 67.44444 58.77778 79.0 64.55556 -26.0 34.666668 -8.666667 79.0 0.30628127 -2.4221272 FOLIAGE 140.0 124.0 9 0.0 0.0 1.0 0.44444454 1.1111112 1.0518516 2.5185184 0.22222222 6.111111 1.2222222 -6.888889 10.777778 -3.8888888 6.111111 0.97376543 -2.267462 FOLIAGE 69.0 139.0 9 0.0 0.0 2.8333328 1.7732588 2.1111112 1.6688871 18.074074 16.0 22.555555 15.666667 -6.2222223 13.444445 -7.2222223 23.88889 0.38661182 -1.7028334 FOLIAGE 9.0 80.0 9 0.0 0.0 2.9444444 13.751853 16.666666 71.5111 23.62963 17.333334 31.666666 21.88889 -18.88889 24.11111 -5.2222223 31.666666 0.5142537 -2.4315135 FOLIAGE 6.0 81.0 9 0.0 0.11111111 4.111111 8.740745 5.722223 28.50741 12.481482 7.6666665 18.88889 10.888889 -14.444445 19.222221 -4.7777777 18.88889 0.6281558 -2.388561 FOLIAGE 74.0 129.0 9 0.0 0.0 0.22222222 0.029629637 0.11111111 0.029629635 0.5185185 0.0 1.5555556 0.0 -1.5555556 3.1111112 -1.5555556 1.5555556 1.0 -2.0943952 FOLIAGE 41.0 75.0 9 0.0 0.11111111 15.388889 19.136257 26.611113 31.71359 55.0 47.444443 65.44444 52.11111 -22.666666 31.333334 -8.666667 65.44444 0.29780185 -2.3567543 FOLIAGE 36.0 145.0 9 0.0 0.0 0.2777778 0.19629629 1.2777778 2.0629628 0.8518519 0.33333334 1.4444444 0.7777778 -1.5555556 1.7777778 -0.22222222 1.4444444 0.25185186 -2.5309503 FOLIAGE 94.0 144.0 9 0.0 0.0 0.44444442 0.118518494 0.49999997 0.1666667 1.1481482 0.0 3.4444444 0.0 -3.4444444 6.888889 -3.4444444 3.4444444 1.0 -2.0943952 FOLIAGE 18.0 90.0 9 0.0 0.0 1.0555555 0.37407416 0.6666667 0.22222227 2.8148148 0.5555556 6.888889 1.0 -6.7777777 12.222222 -5.4444447 6.888889 0.9261464 -2.1643226 FOLIAGE 68.0 103.0 9 0.0 0.0 0.66666675 0.57777774 1.111111 0.96296334 2.148148 0.11111111 5.6666665 0.6666667 -6.111111 10.555555 -4.4444447 5.6666665 0.9876543 -2.1854658 FOLIAGE 45.0 108.0 9 0.0 0.11111111 25.5 12.795401 27.277779 15.930981 49.814816 41.77778 61.11111 46.555557 -24.11111 33.88889 -9.777778 61.11111 0.35897508 -2.3604913 FOLIAGE 59.0 99.0 9 0.0 0.0 0.77777785 0.8296297 0.99999994 0.3555556 2.0370371 0.11111111 5.5555553 0.44444445 -5.7777777 10.555555 -4.7777777 5.5555553 0.9861111 -2.149743 FOLIAGE 67.0 136.0 9 0.0 0.0 6.722223 3.7083488 2.6666667 3.1972213 15.518518 9.0 25.333334 12.222222 -19.555555 29.444445 -9.888889 25.333334 0.66081303 -2.3075109 FOLIAGE 226.0 110.0 9 0.0 0.0 0.33333334 0.08888887 0.49999997 0.2111111 1.6666666 0.11111111 4.4444447 0.44444445 -4.6666665 8.333333 -3.6666667 4.4444447 0.9777778 -2.1559837 FOLIAGE 231.0 124.0 9 0.0 0.0 3.4444447 14.962965 1.8333334 6.4333353 3.0 1.4444444 5.888889 1.6666666 -4.6666665 8.666667 -4.0 5.888889 0.895369 -2.118937 FOLIAGE 103.0 125.0 9 0.0 0.0 0.9444445 0.82775915 0.83333343 0.6912146 1.7777778 0.44444445 3.8888888 1.0 -4.0 6.3333335 -2.3333333 3.8888888 0.9238095 -2.2375617 FOLIAGE 1.0 81.0 9 0.0 0.0 12.166667 267.45554 9.222222 205.36296 21.333334 14.0 30.555555 19.444445 -22.0 27.666666 -5.6666665 30.555555 0.5952822 -2.438409 FOLIAGE 230.0 124.0 9 0.0 0.0 0.2777778 0.10740743 0.2777778 0.15185183 0.6666667 0.0 2.0 0.0 -2.0 4.0 -2.0 2.0 1.0 -2.0943952 FOLIAGE 58.0 109.0 9 0.0 0.0 0.8888889 0.25185165 2.8333333 1.677777 4.296296 1.4444444 8.444445 3.0 -8.555555 12.444445 -3.8888888 8.444445 0.8644824 -2.2837873 FOLIAGE 59.0 120.0 9 0.0 0.0 2.1666667 1.9860634 1.4444441 1.8698385 19.074074 10.555555 33.11111 13.555555 -25.555555 42.11111 -16.555555 33.11111 0.6812664 -2.2312608 FOLIAGE 140.0 125.0 9 0.0 0.0 0.66666657 0.22222227 2.6666667 3.7777781 3.925926 1.5555556 7.7777777 2.4444444 -7.111111 11.555555 -4.4444447 7.7777777 0.85319865 -2.2342408 FOLIAGE 127.0 143.0 9 0.0 0.0 1.5 0.12222214 0.88888884 0.60740745 4.185185 0.8888889 9.444445 2.2222223 -9.888889 15.777778 -5.888889 9.444445 0.915376 -2.2574124 FOLIAGE 23.0 129.0 9 0.0 0.0 0.5 0.077777795 0.38888887 0.15185186 0.5185185 0.0 1.5555556 0.0 -1.5555556 3.1111112 -1.5555556 1.5555556 0.7777778 -2.0943952 FOLIAGE 191.0 119.0 9 0.0 0.0 1.1111107 1.2938615 0.9444459 0.772202 39.851852 36.22222 48.22222 35.11111 -10.888889 25.11111 -14.222222 48.22222 0.27171725 -2.0059998 CEMENT 219.0 80.0 9 0.0 0.0 1.2777767 0.3296295 0.6666667 0.9333318 39.703705 36.333336 48.22222 34.555557 -10.111111 25.555555 -15.444445 48.22222 0.28296396 -1.9626464 CEMENT 136.0 45.0 9 0.0 0.0 1.222222 1.5444059 2.0555553 1.5263131 53.074074 48.11111 63.77778 47.333332 -14.888889 32.11111 -17.222221 63.77778 0.25936732 -2.0459049 CEMENT 66.0 160.0 9 0.0 0.0 3.0000007 4.044447 2.777778 0.4296295 22.851852 18.222221 31.555555 18.777779 -13.888889 26.11111 -12.222222 31.555555 0.4260139 -2.1387258 CEMENT 190.0 105.0 9 0.0 0.0 1.8888893 2.2962983 2.166666 1.6777797 45.74074 41.22222 56.333332 39.666668 -13.555555 31.777779 -18.222221 56.333332 0.29599184 -1.9960818 CEMENT 37.0 78.0 9 0.0 0.0 1.0000006 0.17777735 2.5555565 2.8740728 43.814816 41.11111 51.88889 38.444443 -8.111111 24.222221 -16.11111 51.88889 0.25891644 -1.8860723 CEMENT 198.0 127.0 9 0.0 0.0 2.4444444 4.385187 8.555555 59.54075 40.74074 38.0 48.22222 36.0 -8.222222 22.444445 -14.222222 48.22222 0.24899939 -1.9083478 CEMENT 191.0 101.0 9 0.0 0.0 1.111112 0.7793635 1.1111113 1.186342 45.037037 39.0 57.11111 39.0 -18.11111 36.22222 -18.11111 57.11111 0.32273299 -2.0943027 CEMENT 243.0 120.0 9 0.0 0.0 4.4444447 4.359749 1.5555547 1.8338387 47.851852 44.77778 56.333332 42.444443 -9.222222 25.444445 -16.222221 56.333332 0.2453213 -1.9107349 CEMENT 230.0 117.0 9 0.0 0.0 3.2777786 0.92895794 1.4444433 0.86066324 39.037037 33.555557 49.77778 33.77778 -16.444445 32.22222 -15.777778 49.77778 0.33502588 -2.1062348 CEMENT 151.0 89.0 9 0.0 0.0 8.388889 4.577317 0.72222203 0.38968238 31.703703 27.333334 41.0 26.777779 -13.111111 27.88889 -14.777778 41.0 0.35127252 -2.0465415 CEMENT 176.0 100.0 9 0.0 0.0 1.9444441 0.7740748 1.4444447 0.6518514 55.37037 50.333332 66.88889 48.88889 -15.111111 34.555557 -19.444445 66.88889 0.26862052 -2.00619 CEMENT 118.0 126.0 9 0.0 0.0 0.6666667 0.39999974 1.8333336 2.1222224 20.555555 16.11111 28.666666 16.88889 -13.333333 24.333334 -11.0 28.666666 0.437078 -2.1588047 CEMENT 42.0 57.0 9 0.0 0.0 1.3888906 0.97562754 0.99999875 0.36514837 65.703705 59.444443 79.44444 58.22222 -18.777779 41.22222 -22.444445 79.44444 0.26677614 -2.0307028 CEMENT 217.0 148.0 9 0.0 0.0 2.0555556 2.551854 1.0555553 0.5074078 29.074074 21.444445 41.555557 24.222221 -22.88889 37.444443 -14.555555 41.555557 0.4837708 -2.2379715 CEMENT 14.0 146.0 9 0.11111111 0.0 0.888889 0.4740738 1.1111112 0.7407407 10.592592 8.0 15.666667 8.111112 -7.7777777 15.222222 -7.4444447 15.666667 0.48786426 -2.1089108 CEMENT 22.0 87.0 9 0.0 0.0 1.8888899 1.2590423 1.1666666 0.62361073 64.03704 55.77778 80.333336 56.0 -24.777779 48.88889 -24.11111 80.333336 0.30969977 -2.105073 CEMENT 130.0 32.0 9 0.0 0.0 1.1111113 1.047041 0.83333397 0.83665866 59.48148 54.22222 70.88889 53.333332 -15.777778 34.22222 -18.444445 70.88889 0.24900064 -2.042422 CEMENT 162.0 159.0 9 0.0 0.0 2.1666667 0.9603238 2.2222223 1.4555128 26.11111 25.222221 29.555555 23.555555 -2.6666667 10.333333 -7.6666665 29.555555 0.20284556 -1.8025542 CEMENT 150.0 158.0 9 0.0 0.0 2.166667 1.6333338 1.388889 0.41851807 8.444445 7.0 12.222222 6.111111 -4.3333335 11.333333 -7.0 12.222222 0.50308645 -1.9434487 CEMENT 163.0 68.0 9 0.0 0.0 1.833334 2.21111 1.5555559 0.96296287 56.77778 52.0 68.22222 50.11111 -14.333333 34.333332 -20.0 68.22222 0.26505277 -1.9843078 CEMENT 187.0 80.0 9 0.0 0.0 1.3333327 0.7111114 1.3333334 0.7111086 40.51852 37.77778 47.666668 36.11111 -8.222222 21.444445 -13.222222 47.666668 0.24472968 -1.942698 CEMENT 140.0 73.0 9 0.0 0.0 1.7222214 0.8277598 0.7777774 1.0036957 46.296295 45.666668 51.11111 42.11111 -1.8888888 14.444445 -12.555555 51.11111 0.1761556 -1.6815889 CEMENT 236.0 117.0 9 0.0 0.0 0.7777786 0.40368706 1.277778 0.74286777 45.88889 39.555557 58.444443 39.666668 -19.0 37.666668 -18.666666 58.444443 0.33047688 -2.0994802 CEMENT 112.0 90.0 9 0.0 0.0 7.38889 6.9455557 1.2777773 0.87981415 65.18519 57.666668 79.77778 58.11111 -22.555555 43.77778 -21.222221 79.77778 0.27834544 -2.108813 CEMENT 197.0 121.0 9 0.0 0.0 21.666666 17.3628 0.94444436 0.9047208 41.037037 37.444443 49.444443 36.22222 -10.777778 25.222221 -14.444445 49.444443 0.28057775 -1.9955361 CEMENT 141.0 17.0 9 0.11111111 0.22222222 3.7222226 4.4493027 5.0 2.319004 44.592594 40.333336 54.0 39.444443 -12.777778 28.222221 -15.444445 54.0 0.26818594 -2.030048 CEMENT 79.0 28.0 9 0.0 0.0 4.277777 3.7618961 0.8333333 0.6582806 62.407406 53.444443 79.111115 54.666668 -26.88889 50.11111 -23.222221 79.111115 0.32455578 -2.1445074 CEMENT 169.0 102.0 9 0.0 0.0 1.0 0.35555485 0.8888893 0.2962955 58.22222 53.444443 69.66667 51.555557 -14.333333 34.333332 -20.0 69.66667 0.25975996 -1.9855843 CEMENT 208.0 65.0 9 0.0 0.0 1.3888874 1.2367799 26.444445 25.537477 56.703705 52.666668 64.44444 53.0 -12.111111 23.222221 -11.111111 64.44444 0.19713038 -1.9708116 CEMENT 189.0 144.0 9 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 WINDOW 189.0 141.0 9 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 WINDOW 210.0 153.0 9 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 WINDOW 57.0 89.0 9 0.0 0.0 1.7222222 1.3066783 6.1666665 4.7034264 17.0 13.0 24.555555 13.444445 -12.0 22.666666 -10.666667 24.555555 0.47748852 -2.1297464 WINDOW 243.0 94.0 9 0.0 0.0 0.6666666 0.31111112 0.22222221 0.029629631 1.1851852 0.22222222 3.2222223 0.11111111 -2.8888888 6.111111 -3.2222223 3.2222223 0.9777778 -2.0712416 WINDOW 229.0 104.0 9 0.0 0.0 0.49999985 0.54772234 2.8333333 2.0412421 19.777779 16.333334 26.11111 16.88889 -10.333333 19.0 -8.666667 26.11111 0.37553233 -2.1506376 WINDOW 226.0 131.0 9 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 WINDOW 196.0 95.0 9 0.0 0.0 1.722222 1.1238165 1.3333335 1.264911 7.6296296 6.7777777 10.777778 5.3333335 -2.5555556 9.444445 -6.888889 10.777778 0.51256585 -1.7492584 WINDOW 43.0 152.0 9 0.0 0.0 1.9444445 1.7074082 1.2222222 0.8296299 1.5185186 1.0 2.8888888 0.6666667 -1.5555556 4.111111 -2.5555556 2.8888888 0.64867723 -1.9332389 WINDOW 54.0 133.0 9 0.0 0.0 1.5555557 1.0074074 0.50000006 0.3444443 5.3703704 3.6666667 9.0 3.4444444 -5.111111 10.888889 -5.7777777 9.0 0.6304714 -2.0480003 WINDOW 157.0 85.0 9 0.0 0.0 1.2222223 1.2412657 0.22222233 0.17213264 18.925926 14.555555 26.88889 15.333333 -13.111111 23.88889 -10.777778 26.88889 0.45902446 -2.1609125 WINDOW 96.0 94.0 9 0.0 0.0 0.7222226 0.28518537 0.44444466 0.42963016 20.222221 16.0 28.777779 15.888889 -12.666667 25.666666 -13.0 28.777779 0.45154575 -2.084893 WINDOW 152.0 155.0 9 0.0 0.0 0.5 0.61111104 10.777778 131.80739 7.296296 5.3333335 11.0 5.5555553 -5.888889 11.111111 -5.2222223 11.0 0.5 -2.115567 WINDOW 208.0 34.0 9 0.0 0.0 1.7222224 1.7309811 0.4444445 0.50184834 14.444445 10.777778 21.0 11.555555 -11.0 19.666666 -8.666667 21.0 0.479958 -2.1623826 WINDOW 222.0 62.0 9 0.0 0.0 0.27777782 0.2509242 0.6666667 0.55777335 6.4074073 4.111111 11.444445 3.6666667 -6.888889 15.111111 -8.222222 11.444445 0.68080807 -2.0341523 WINDOW 123.0 152.0 9 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 WINDOW 20.0 134.0 9 0.0 0.0 0.6666667 0.088888995 0.61111116 0.24074072 2.9629629 1.1111112 6.4444447 1.3333334 -5.5555553 10.444445 -4.888889 6.4444447 0.8292328 -2.133095 WINDOW 223.0 62.0 9 0.0 0.0 0.3333334 0.29814243 0.44444442 0.50184846 6.4444447 4.111111 11.444445 3.7777777 -7.0 15.0 -8.0 11.444445 0.6703704 -2.0487173 WINDOW 184.0 145.0 9 0.0 0.0 0.72222227 0.6116159 0.22222222 0.2721655 0.5555556 0.33333334 1.2222222 0.11111111 -0.6666667 2.0 -1.3333334 1.2222222 0.5277778 -1.9209436 WINDOW 225.0 58.0 9 0.0 0.0 0.3333335 0.42163706 0.4444445 0.34426522 8.333333 5.5555553 14.111111 5.3333335 -8.333333 17.333334 -9.0 14.111111 0.62222224 -2.0685637 WINDOW 58.0 113.0 9 0.0 0.0 3.4444447 1.2232318 0.7222223 0.38968182 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/3760/CH4/EX4.9/Ex4_9.sce
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[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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clc; A=2;//No of parallel paths for armature conductors P=6;//No. of poles If=2;//Field current Il=148;//Line current Ia=If+Il;//Armature current Z=480;//No of conductors //brushes on GNA, theta=0 ATd1=0//demagnetizing ampere turns ATc1=((Ia*Z)/(2*A*P))//Cross magnetizing ampere turns printf('When brushes are on GNA the demagnetizing ampere turns & Cross magnetizing ampere turns are equal to %f & %f ATs/pole respectively.\n',ATd1,ATc1); //brushes are shifted from GNA by 5 degrees electrical, theta=5 theta=5; ATd2=((2*theta*Ia*Z)/(180*2*A*P))//demagnetizing ampere turns ATc2=3000-ATd2;//Cross magnetizing ampere turns printf('When the brushes are shifted from GNA by 5 degrees electrical the demagnetizing ampere turns & Cross magnetizing ampere turns are equal to %f & %f ATs/pole respectively.\n',ATd2,ATc2); //brushes are shifted from GNA by 5 degrees mechanical, theta_m=5 theta_m=5;//mechanical angle theta_e=(P/2)*theta_m;//electrical angle ATd3=((2*theta_e*Ia*Z)/(180*2*A*P))//demagnetizing ampere turns ATc3=3000-ATd3;//Cross magnetizing ampere turns printf('When the brushes are shifted from GNA by 5 degrees mechnical the demagnetizing ampere turns & Cross magnetizing ampere turns are equal to %f & %f ATs/pole respectively',ATd3,ATc3);
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/pskdemod.sci
7cd27b6b457b5d564e7fa4b5e1a0cbc2a458c14c
[]
no_license
kUser18/comm_scilab
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c98d78ba55b73644bf32cf1f901b6c0e45d73bc2
refs/heads/master
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2018-09-30T20:35:50
2018-09-30T20:35:50
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sci
pskdemod.sci
function signal = pskdemod(psk, m, phi, datatype) // //Function Description //pskdemod: This function demodulates a matrix of psk modulated //baseband signals (constellation points or complex numbers) into integers. // //Calling sequence:- //signal = pskdemod(psk, m) //signal = pskdemod(psk, m, phi) //signal = pskdemod(psk, m, phi, datatype) // //Parameters: //psk: complex - matrix // The matrix of psk signals to be demodulated. //m: int - scalar // The total number of constellation points. // Must be greater than or equal to 1. //phi is taken to be zero if not specified. //phi: float - scalar // The initial phase (in radian) of the PSK signal. //datatype is assumed to be "Bin" if not specified. //datatype: string // Should be either "Bin", "bin", "Gray" or "gray" // If "Bin" or "bin", then the encoding of the signal is assumed // to be binary. // If "Gray" or "gray", then the signal is assumed to be // Gray coded, and is converted to binary before // modulation. // //Example Usage // Using only the signal and the number of constellation points //signal = pskdemod(psk, m) // // Specifying the initial phase //signal = pskdemod(psk, m, phi) // // Specifying the encoding //signal = pskdemod(psk, m, phi, datatype) // //Authors //Devdatta Kathale // //Function Description Ends // //Find the number of arguments, and act accordingly select(argn(2)) case 0 then error('pskdemod: Need at least 2 arguments.') case 1 then error('pskdemod: Need at least 2 arguments.') case 2 then phi = 0 datatype = "Bin" if m < ceil(m) | m<1 then error('pskdemod: m must be an integer greater than 0') end case 3 then datatype = "Bin" if m < ceil(m) | m<1 then error('pskdemod: m must be an integer greater than 0') end case 4 then if m < ceil(m) | m<1 then error('pskdemod: m must be an integer greater than 0') end if datatype == "Gray" | datatype == "gray" then //Convert gray coded x into binary // //Obtain Gray code of the integers 0:m-1 binary = 0:m-1 grayIndex=bitxor(binary, floor(binary/2)) // elseif datatype == "Bin" | datatype == "bin" then //no need to change x=x else error("pskdemod: Type must be either ''Gray'' or ''Bin''.") end end // //Find the complex phase exponents unitPhase = (2*%pi * 1.0/m) // //Compute the argument of the inputs, and round to the nearest psk phase psk_dim = size(psk) [phase, mag] = phasemag(psk) phase = phase * %pi/180 phase = phase - phi phase = phase + unitPhase/2 phase(phase<0) = phase(phase<0)+2*%pi phase = phase / unitPhase phase = floor(phase) signal = phase // //Gray code case if datatype == "Gray" | datatype == "gray" then signal = grayIndex(signal+1) end signal = matrix(signal, psk_dim) endfunction
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11_8.sce
clc //initialization of variables v=600 //ft/sec T=60+460 //R P=14.7 //lb/in^2 Pratio=6 Tin=1540+460 //R cp=0.264 cpratio=1.35 //calculations Pt2byP1=(1+ (cpratio-1)*v^2 /(cpratio*2*32.2*53.3*T))^(3.86) Pt3byP1=Pt2byP1*Pratio eta=1- 1/(Pt3byP1)^0.259 Tt3=T*(Pt3byP1)^((cpratio-1)/cpratio) Q=cp*(Tin-Tt3) V6=sqrt(eta*2*32.2*778*Q + v^2) Fn=(V6-v)/32.2 //resullts printf("Thermal efficiency = %.2f ",eta) printf("\n thrust per pound of air per sec = %.1f lb-sec/lbm",Fn) //The answers are a bit different due to rounding off error in textbook
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ex25_14.sce
clc;clear; //Example 25.13 //conversion of binary to decimal //given values X=10.101;//binary number //calculation Z=(1*2^1)+(0*2^0)+(1*2^-1)+(0*2^-2)+(1*2^-3); disp(Z,'decimal equivalent of the given binary number is')
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Ch03Ex18.sce
// Scilab code Ex3.18: Pg 101 (2008) clc; clear; V = 400; // Supply voltage, V E = 0.5e06; // Dielectric strength, V/m // Since E = V/d, solving for d d = V/E; // Thickness of dielectric, m printf("\nThe minimum thickness of dielectric required = %3.1fmm", d/1e-03); // Result // The minimum thickness of dielectric required = 0.8 mm
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Example4_1.sce
//clear// //Caption: Program to find the work involved 'W' in moving a charge 'Q' along shorter arc of a circle //Example4.1 //page 84 clc; x = sym('x'); y = sym('y'); z = sym('z'); y1 = sym('y1'); y = sqrt(1-x^2); Q = 2; //charge in coulombs Edot_dL1 = integ(y,x); disp(Edot_dL1,'E.dx*ax =') Edot_dL1 = limit(Edot_dL1,x,0.8)-limit(Edot_dL1,x,1); disp(Edot_dL1,'Value of E.dx*ax =') Edot_dL2 = 0; disp(Edot_dL2,'Value of E.dz*az=') x = sqrt(1-y1^2); Edot_dL3 = integ(x,y1) disp(Edot_dL3,'E.dy*ay=') Edot_dL3 = limit(Edot_dL3,y1,0.6)-limit(Edot_dL3,y1,0); disp(Edot_dL3,'Value of E.dy*ay =') W = -Q*(Edot_dL1+Edot_dL2+Edot_dL3); disp(W,'Work done in moving a point charge along shorter arc of circle in Joules, W=') //Result // E.dx*ax = asin(x)/2+x*sqrt(1-x^2)/2 // Value of E.dx*ax = (25*asin(4/5)+12)/50-%pi/4 // Value of E.dz*az = 0. // E.dy*ay = asin(y1)/2+y1*sqrt(1-y1^2)/2 // Value of E.dy*ay = (25*asin(3/5)+12)/50 //Work done in moving a point charge along shorter arc of circle in Joules, W = // -2*((25*asin(4/5)+12)/50+(25*asin(3/5)+12)/50-%pi/4) //Which is equivalent to // -2*((25*0.9272952+12)/50+(25*0.6435011+12)/50-%pi/4) = -0.96 Joules
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/convergenceBino.sce
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convergenceBino.sce
exec("histcFix.sci",-1) N = 10^3 // taille de l'échantillon // parametres de la loi B(n,p) n = 100 // valeur max de n p = .5 clf() // fixer les axes a = gca() a.data_bounds = [0,0;1,.4*sqrt(n/p/(1-p))] a.auto_scale = "off" for k = floor(linspace(2,n)) // frame par frame ech = grand(1,N,"bin",k,p) x = linspace(0,1,k+1) drawlater() delete(a.children) // histogramme empirique histplot(x,(ech+.5)/k) // distribution théorique plot(x+.5/k,binomial(p,k)*k) // sleep(40) // décommenter si trop rapide drawnow() end
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/source/2.5/tests/examples/mean.man.tst
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mean.man.tst
clear;lines(0); A=[1,2,10;7,7.1,7.01]; mean(A) mean(A,'r') mean(A,'c')
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// sum 3-28 clc; clear; rho=0.0078*9.81*10^-6; sigc=150; g=9.81; V=sqrt(sigc*g/rho)*10^-3; R=1; w=V/R; N=w*60/(2*%pi); // printing data in scilab o/p window printf("N is %0.3f rpm ",N);
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Example3_1.sce
//Example 3.1 clear; clc; R=10; C=40*10^(-6); L=5*10^(-3); Hsnum=(R/L)*%s; Hsden=((%s^(2))+(R/L)*%s+(1/(L*C))); Hs=Hsnum/Hsden;//Transfer Function h=syslin('c',Hs); plzr(h); zeroes=roots(Hsnum); poles=roots(Hsden);