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d6af8d3586b20189c9f9e50497f6deaaa12b8e91
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/Ashe Smooth Diagonal .sce
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refs/heads/master
2023-01-14T02:10:25.103083
2020-11-21T16:47:14
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sce
Ashe Smooth Diagonal .sce
Name=Ashe Diagonal Smooth PlayerCharacters=Aimer BotCharacters=Diagonal.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Aimer AddedBots=Diagonal.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=2 BotTeams=1 MapName=cube1wallwideriflesmooth.map MapScale=1.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=true TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Overwatch WeaponHeroTag=Ashe, Viper DifficultyTag=3 AuthorsTag=Tammas, Watsyurdeal BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=false BlockFCT=false Description=Track a ball that moves in a Diagonal pattern. GameVersion=2.0.2.0 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false LockFOVRange=false LockedFOVMin=103.0 LockedFOVMax=160.0 LockedFOVScale=Clamped Horizontal [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=Diagonal DodgeProfileNames=up DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=60.0 DodgeProfileMinChangeTime=60.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=react2 SeeThroughWalls=false NoDodging=false NoAiming=true AbilityUseTimer=0.05 UseAbilityFrequency=0.28 UseAbilityFreqMinTime=0.1 UseAbilityFreqMaxTime=0.18 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=Aimer MaxHealth=100.0 WeaponProfileNames=MG;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=500.0 Acceleration=16000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=0.0 Gravity=0.0 AirControl=1.0 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Spheroid MainBBHeight=20.0 MainBBRadius=10.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=react2 MaxHealth=10000.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.01 MaxRespawnDelay=0.01 StepUpHeight=75.0 CrouchHeightModifier=1.0 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=500.0 MaxCrouchSpeed=300.0 Acceleration=16000.0 AirAcceleration=16000.0 Friction=0.0 BrakingFrictionFactor=0.0 JumpVelocity=910.0 Gravity=0.0 AirControl=1.0 CanCrouch=true CanPogoJump=true CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=10 AirJumpVelocity=910.0 MainBBType=Spheroid MainBBHeight=50.0 MainBBRadius=25.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.0 JetpackFullFuelTime=6000.0 JetpackFuelIncPerSec=1000.0 JetpackFuelRegensInAir=true JetpackThrust=12000.0 JetpackMaxZVelocity=1300.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=down.abilmov;down2.abilmov;; HideWeapon=true AerialFriction=0.2 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=10000.0 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=true FlightObeysPitch=false FlightVelocityUp=500.0 FlightVelocityDown=500.0 [Dodge Profile] Name=up MaxTargetDistance=9999.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=1.6 MaxLRTimeChange=3.5 MinFBTimeChange=1.0 MaxFBTimeChange=2.0 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=80.0 DamageReactionResetTimer=0.3 JumpFrequency=1.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.01 MaxCrouchTime=0.01 MinJumpTime=0.01 MaxJumpTime=0.01 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.001 BlockedMovementReactionMax=0.001 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=MG Type=Hitscan ShotsPerClick=1 DamagePerShot=0.0 KnockbackFactor=0.1 TimeBetweenShots=0.046 Pierces=false 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=0.1 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=1.5 ReloadTimeFromPartial=1.5 DamageFalloffStartDistance=0.1 DamageFalloffStopDistance=0.1 DamageAtMaxRange=5.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.001 BounceOffWorld=true BounceFactor=0.6 BounceCount=0 HomingProjectileAcceleration=6000.0 ProjectileEnemyHitRadius=0.1 CanAimDownSight=true ADSZoomDelay=0.0 ADSZoomSensFactor=0.514667 ADSMoveFactor=0.8 ADSStartDelay=0.2 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=true DecalType=1 DecalSize=15.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot=MG Scoped StunDuration=0.0 CircularSpread=false 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=65.809998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=None ParticleMuzzleFlashScale=0.1 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=2.0,10.0,-2.6,2.4 SpreadSCA=2.0,10.0,-2.6,2.4 SpreadMSA=2.0,10.0,-2.6,2.4 SpreadMCA=2.0,10.0,-2.6,2.4 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=2.0,10.0,-2.6,2.4 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=2.0,10.0,-2.6,2.4 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.45 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.15 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=0.1 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=MG Scoped Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.1 TimeBetweenShots=0.046 Pierces=false 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=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=1.5 ReloadTimeFromPartial=1.5 DamageFalloffStartDistance=3000.0 DamageFalloffStopDistance=5500.0 DamageAtMaxRange=5.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.001 BounceOffWorld=true BounceFactor=0.6 BounceCount=0 HomingProjectileAcceleration=6000.0 ProjectileEnemyHitRadius=0.1 CanAimDownSight=true ADSZoomDelay=0.0 ADSZoomSensFactor=0.5147 ADSMoveFactor=0.8 ADSStartDelay=0.2 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=true DecalType=1 DecalSize=15.0 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=65.809998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Gunshot ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=None 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=0.0,0.1,-2.6,2.4 SpreadSCA=2.0,10.0,-2.6,2.4 SpreadMSA=0.0,0.1,-2.6,2.4 SpreadMCA=2.0,10.0,-2.6,2.4 SpreadSSH=2.0,10.0,-2.6,2.4 SpreadSCH=2.0,10.0,-2.6,2.4 SpreadMSH=2.0,10.0,-2.6,2.4 SpreadMCH=2.0,10.0,-2.6,2.4 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.45 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.15 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=0.1 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Movement Ability Profile] Name=down MaxCharges=1.0 ChargeTimer=3.9 ChargesRefundedOnKill=0.0 DelayAfterUse=0.05 FullyAuto=false AbilityDuration=2.0 LockDirectionForDuration=false NegateGravityForDuration=true MainVelocity=500.0 MainVelocityCanGoVertical=false MainVelocitySetToMovementKeys=true UpVelocity=-500.0 EndVelocityFactor=1.0 Hurtbox=false HurtboxRadius=50.0 HurtboxDamage=50.0 HurtboxGroundKnockbackFactor=1.0 HurtboxAirKnockbackFactor=1.0 AbilityBlocksTurning=false AbilityBlocksMovement=false AbilityBlocksAttack=false AttackCancelsAbility=false AbilityReloadsWeapon=false HealthRestore=0.0 AIUseInCombat=true AIUseOutOfCombat=true AIUseOnGround=true AIUseInAir=true AIReuseTimer=0.05 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=9999.0 AIMaxTargFOV=360.0 AIDamageReaction=false AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.0 AIDamageReactionMaxDelay=0.0 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=1000.0 AIDamageReactionResetTimer=1.0 [Movement Ability Profile] Name=down2 MaxCharges=1.0 ChargeTimer=3.5 ChargesRefundedOnKill=0.0 DelayAfterUse=0.05 FullyAuto=false AbilityDuration=1.5 LockDirectionForDuration=false NegateGravityForDuration=true MainVelocity=500.0 MainVelocityCanGoVertical=false MainVelocitySetToMovementKeys=true UpVelocity=-500.0 EndVelocityFactor=1.0 Hurtbox=false HurtboxRadius=50.0 HurtboxDamage=50.0 HurtboxGroundKnockbackFactor=1.0 HurtboxAirKnockbackFactor=1.0 AbilityBlocksTurning=false AbilityBlocksMovement=false AbilityBlocksAttack=false AttackCancelsAbility=false AbilityReloadsWeapon=false HealthRestore=0.0 AIUseInCombat=true AIUseOutOfCombat=true AIUseOnGround=true AIUseInAir=true 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clc clear close pie([53 42 62 20],[2 1 1 1],["parte 1","parte 2","parte 3","parte 4"]); // Valores, distâncias entre as fatias, rótulos.
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// Example 32_19 clc;funcprot(0); //Given data L_max=5;// MW P=7;// Plant capacity in MW // Calculation //(a) t=[0 12 6];// Time in hours x=[6 12 6]; a=[6 6 6]; b=[5 5 5];// MW for(i=1:3) L=(b(i)/a(i))*sqrt((2*a(i)*x(i))-((x(i))^2)); end b=5;// MW L_av=(%pi*b)/4;// Average load in MW // (i) F_l=L_av/L_max;// Load factor E=L_av*12;// Energy used during 12-hrs period MW hr CF=L_av/P;// Capacity factor printf('\n(a)The average load of the factory=%0.3f MW \n Load factor of the factory=%0.3f MW \n Energy consumed by the factory during 12 hours=%0.1f MW-hr \n Capacity factor=%0.3f',L_av,F_l,E,CF); //(b) b=5; a=4; t=[0 8 4];// Time in hours for(i=1:3) L(i)=2+((b/a)*sqrt((2*a*t(i))-(t(i))^2)); end L_av=(L(1)+L(2)+L(3))/3;// Average load in MW printf('\n(b)The average load of the factory=%0.2f MW',L_av); // The answer vary due to round off error
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clear; clc; // Example: 10.2 // Page: 399 printf("Example: 10.2 - Page: 399\n\n"); // Mathematics is involved in proving but just that no numerical computations are involved. // For prove refer to this example 10.2 on page number 399 of the book. printf(" Mathematics is involved in proving but just that no numerical computations are involved.\n\n"); printf(" For prove refer to this example 10.2 on page 399 of the book.");
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clc; v=440; // rated voltage of mootor no=2000; // no load speed n1=1000; // speed at full load torque Tl=0.5; // load torque as a fraction of rated torque n2=1050; // increased speed due to redued torque // field current is constant so flux is constant // since torqu gets reduced by half new armature current also gets reduced half i.e ia2=ia1/2; vd=(v*(n2-n1))/(n2-(n1/2)); printf('Armature voltage drop at full load is %d V',vd);
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clear; clc; close; x=poly(0,'x'); p1=(3*x-2); p2=(4*x-7); p3=p1*p2; disp(p3,"product=")
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clc //initialisation of variables clear d= 0.366 //ft i= 12 //CALCULATIONS pd= d*i //RESULTS printf ('Required pipe diameter = %.2f in',pd)
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d=3//inches(Diameter of shaft) u=0.4//ft/sec dy=0.003//inches L=8//inches(length of sleeve) f=20//lb( Shear Force)
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//CAPTION:Operation_of_a_Four-Cavity_Klystron //chapter_no.-9, page_no.-386 //Example_no.9-3-2 clc; //(a) Calculate_the_dc_electron_velocity V0=18*(10^3); v0=.593*(10^6)*sqrt(V0); disp(v0,'the_dc_electron_velocity(in m/s)is ='); //(b) Calculate_the_dc_electron_phase_constant f=(10*(10^9));//Operating_frequency w=2*%pi*f Be=w/v0; disp(Be,'the_dc_electron_phase_constant(in rads/m)is ='); //(c) Calculate_the_plasma_frequency po=1*(10^-8);//dc_electron_beam_current_density wp=((1.759*(10^11)*po)/(8.854*(10^-12)))^(1/2); disp(wp,'the_plasma_frequency(in rad/s)is ='); //(d) Calculate_the_reduced_plasma_frequency_for_R=0.5 R=0.5; wq=R*wp; disp(wq,'the_reduced_plasma_frequency_for_R=0.5(in rad/s)is ='); //(e) Calculate_the_reduced_plasma_phase_constant Bq=wq/v0; disp(Bq,'the_reduced_plasma_phase_constant(in rad/m)is ='); //(f) Calculate_the_transit_time_across_the_input_gap d=1*(10^-2);//gap_distance t=d/v0; t=t*(10^9); disp(t,'the_transit_time_across_the_input_gap(in ns)is ='); //(g) Calculate_the_electron_velocity_leaving_the_input_gap V1=10; Bi=1;//beam_coupling_coefficient Vt1=v0*(1+(((Bi*V1)/(2*V0))*sin(w*t*(10^-9)))); disp(Vt1,'the_electron_velocity_leaving_the_input_gap(in m/s)is =');
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clc; e1=-13.6; //in eV disp((e1/4),"Energy of first excited state in eV = "); //displaying result disp((e1/9),"Energy of second excited state in eV = "); //displaying result disp((e1/16),"Energy of third excited state in eV = "); //displaying result
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function function_style() sda() // remet a plat les proprietes des axes par defaut a = gda(); // a est le handle sur ces axes par defaut a.title.font_size = 1; a.title.font_style = %helvetica_bold; a.x_label.font_size = %14pts; a.x_label.font_style = %helvetica_italic; a.y_label.font_size = %14pts; a.y_label.font_style = %helvetica_italic; a.z_label.font_size = %14pts; a.z_label.font_style = %helvetica_italic; a.font_size = %14pts; endfunction
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// vectors are (2,3,1),(2,1,2),(3,2,1) clear;close;clc; A=[2 3 1;2 1 2;3 2 1]; disp(A,'A='); [m,n]=size(A); for k=1:n V(:,k)=A(:,k); for j=1:k-1 R(j,k)=V(:,j)'*A(:,k); V(:,k)=V(:,k)-R(j,k)*V(:,j); end R(k,k)=norm(V(:,k)); V(:,k)=V(:,k)/R(k,k); end disp(V,'Q');
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//OptoElectronics and Fibre Optics Communication, by C.K Sarkar and B.C Sarkar //Example 5.2 //OS=Windows 10 ////Scilab version Scilab 6.0.0-beta-2(64 bit) clc; clear; //given n=3.8;//refractive index L=200*10^-4;//length in cm W=100*10^-4;//width in cm Beta=20*10^-3;//gain factor in A/cm^3 alpha=10;//loss coefficient per cm R1=((n-1)/(n+1))^2;//reflectivity c1=((alpha+((1/L)*(log(1/R1)))))//constant value Jth=(1/Beta)*c1;//threshold current density in A/cm^2 mprintf("\n Threshold current density is= %.2f x10^3 A/cm^2",Jth*1e-3);//multiplication by 1e-3 to convert the ratio to 10^-3 Ith=Jth*L*W;//threshold current in A mprintf("\n Threshold current is =%.2f mA",Ith*1e3);//the answer vary due to rouding
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function r=%s_h_s(a,b) //computes a&b for a and b matrices of scalar // Copyright INRIA if a==[]|b==[] then r=[] else r=(a<>0)&(b<>0) end
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//Chapter 9 : Eigenvalues and Eigenvectors //Example 9.1 //Scilab 6.0.1 //Windows 10 clear; clc; A=[0 1;-1 0]; disp(A,'A=') l=poly(0,'lambda') p=-l I=eye(2,2) B=A-(l*I) db=det(B) disp(db,'det=') r=roots(db) disp(r,'roots=') mprintf('since it has no real roots, A has no real eigen values') eig=spec(A) disp(eig,'eigen values=')
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M = csvRead('Salary_Data.csv') M(or(isnan(M),'c'),:) = [] data = M chdir('..') toolbox_basedir = pwd() chdir('tests') getd(toolbox_basedir + '/macros') models = mgetl('../macros/models') numfiles = size(models) for i = 23:numfiles(1) model = models(i) disp('Running ' + string(i) + ' of ' + string(numfiles(1)) + ' : ' + model) machineLearn(model, data, toolbox_basedir, '') end
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// Example 12.1: (a) RD // (b) Product RC // (c) Reasonable value of R and C clc, clear fo=8e3; // in hertz mu=59; rd=10; // in kilo-ohms disp("Part (a)"); RD=29*rd/(mu-29); // in kilo-ohms disp(RD,"RD (kΩ​) ="); disp("Part (b)"); RC=1/(2*%pi*fo*sqrt(6)); // in seconds RC=RC*1e6; // in micro-seconds disp(RC,"Product RC (µs) ="); disp("Part (c)"); R=50; // in kilo-ohms C=RC/R; // in nano-farad C=C*1e3; // in pico-farad disp(R,"Reasonable value of R (kΩ​) ="); disp(C,"Reasonable value of C (pF) =");
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clear; clc; close; E = 10; //volts R = 0.33*10^(3); //ohms Vo = 0.7; //volts I = (E - Vo)/R; Id1 = I/2; Id2 = I/2; diary('C:\Users\DELL\Desktop\intern\chapter_2\2_10.txt'); disp(Vo,'Output Volatge is : '); disp(Id1,'Current through diode 1 is : '); disp(Id2,'Current through diode 2 is :')
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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 0.410192D+00 2 -0.594881D-02 0.298538D-02 3 -0.418965D-02 0.339572D-03 0.442730D+00 4 0.535329D-03 0.151182D-04 -0.583971D-02 0.373203D-02 5 0.441600D-03 0.239895D-04 0.632108D-03 0.124755D-03 0.428278D-02 6 0.293420D-04 0.347738D-04 0.536824D-03 -0.875918D-04 -0.656870D-04 7 -0.147865D-02 0.472849D-04 0.218205D-02 -0.201489D-03 0.276827D-03 8 -0.799944D-03 -0.253001D-04 -0.247362D-03 0.724071D-04 0.744089D-05 9 -0.459373D+00 0.966249D-02 -0.103067D+00 0.111147D-01 0.207074D+00 10 -0.110797D+00 -0.547491D-02 0.969322D-01 0.222795D-01 0.226707D+00 11 0.190178D+00 -0.122266D-01 -0.351301D+00 0.462141D-02 -0.124817D+00 12 -0.741277D-01 0.894243D-02 0.727284D+00 0.237252D-01 -0.397251D-01 13 -0.838990D-01 0.295374D-02 0.170866D+00 -0.692360D-02 0.264066D-02 14 0.222980D+00 -0.960234D-03 0.129426D+00 0.634272D-02 -0.425489D-03 15 -0.377982D+01 -0.793414D-02 0.151092D+00 0.385603D-01 -0.190200D+00 16 -0.355346D-02 -0.117895D-01 0.671077D-02 0.621508D-03 0.217305D-02 17 0.463733D-02 -0.105110D-04 -0.174866D-02 -0.547052D-03 -0.110957D-02 18 -0.866641D-01 0.828171D-01 0.340470D+00 0.163608D-01 0.111909D+00 19 0.694268D-01 -0.220437D-02 0.102724D+00 0.281661D-02 0.163944D-01 20 0.651522D+00 0.254313D-01 0.185595D+01 0.941487D-02 -0.297872D-01 21 -0.713466D-01 0.507478D-02 -0.126996D+00 0.290876D-02 -0.124134D-01 22 0.271761D-03 -0.692997D-03 0.135916D-02 -0.296908D-03 -0.923461D-03 23 0.144551D-01 0.208695D-02 -0.146160D-01 0.117805D-01 -0.466511D-03 24 -0.243314D-02 -0.240789D-03 0.172784D-02 -0.328878D-03 0.280085D-03 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.630129D-03 7 0.704015D-03 0.418235D-02 8 0.139549D-03 0.580291D-03 0.308613D-02 9 -0.341058D-01 -0.911509D-02 0.267531D-02 0.624734D+02 10 -0.128788D-01 0.203777D-01 0.691241D-02 0.113840D+02 0.239899D+02 11 0.219111D-01 -0.160924D-01 0.148246D-01 -0.888670D+01 -0.854680D+01 12 -0.285668D-01 0.364278D-02 0.814910D-01 0.104903D+02 0.779772D+00 13 0.467617D-01 0.142810D+00 0.263519D-01 -0.530628D+01 0.143359D+01 14 0.240348D-01 0.140262D+00 0.395638D+00 0.199312D+01 0.352803D+01 15 0.510970D-01 0.657009D-01 0.131387D-02 -0.188094D+02 -0.161055D+02 16 0.157879D-03 0.141335D-02 0.105592D-02 0.108162D+01 0.240657D+00 17 -0.243284D-03 -0.578414D-03 0.191585D-03 -0.176653D+00 -0.701204D-01 18 -0.478262D-01 -0.134121D+00 -0.289903D-03 0.153368D+02 0.759063D+01 19 -0.640126D-02 0.412321D-02 0.763665D-02 0.783083D+00 0.153852D+01 20 -0.201118D-01 -0.495088D-01 -0.347382D+00 -0.328004D+01 -0.441801D+01 21 0.569217D-02 -0.479960D-02 -0.111603D-01 -0.199337D+00 -0.124638D+01 22 0.623866D-05 -0.265589D-03 -0.182770D-04 -0.699526D-01 -0.716404D-01 23 0.210076D-03 0.125033D-02 -0.877986D-03 -0.787449D-01 0.197536D+00 24 -0.202607D-04 -0.292109D-03 0.176381D-03 0.226000D-01 0.118741D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.540648D+02 12 -0.634954D+01 0.168672D+03 13 -0.122406D+01 -0.345274D+01 0.150668D+02 14 -0.354968D+01 0.923506D+01 0.623401D+01 0.114091D+03 15 0.126628D+02 -0.550824D+01 0.647704D+01 -0.219294D+01 0.472061D+03 16 -0.325061D+00 -0.240350D+00 0.472956D-01 0.428170D+00 0.225322D+01 17 0.254906D-01 0.496558D-01 -0.280224D-01 -0.213399D-01 -0.198825D+01 18 -0.283164D+01 0.248663D+01 -0.561441D+01 0.325762D+01 -0.480117D+02 19 -0.421435D+00 0.132557D+01 -0.374034D+00 0.767903D+00 0.499916D+00 20 -0.113801D+01 -0.258572D+02 -0.476453D+00 -0.726292D+02 0.650233D+02 21 0.358566D+00 -0.207317D+01 0.292463D+00 -0.108078D+01 -0.430840D+00 22 0.397356D-02 0.366994D-01 -0.194616D-01 -0.368009D-01 0.166855D+00 23 -0.663517D-01 0.122889D+01 0.165277D+00 -0.329275D+00 0.771453D+00 24 -0.666340D-02 -0.138923D+00 -0.368978D-01 -0.293128D-01 -0.241254D+00 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.760576D+00 17 -0.616942D-01 0.230661D-01 18 0.645419D+00 0.702861D-01 0.320916D+03 19 0.127200D-01 -0.248222D-02 0.308150D+01 0.557849D+01 20 0.865698D+00 -0.312620D+00 -0.298185D+02 0.655551D+00 0.558783D+03 21 0.118160D-01 -0.687324D-02 0.252845D+01 -0.519642D+01 -0.100915D+01 22 -0.435774D-02 0.358529D-03 -0.139348D+01 -0.197967D-01 0.210136D+00 23 0.233384D-01 -0.726044D-02 -0.711434D+00 -0.569786D-01 0.562148D+01 24 -0.778706D-02 0.878496D-03 0.219044D+00 0.244883D-02 -0.245464D+01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.678806D+01 22 -0.723480D-01 0.135859D-01 23 -0.141818D-04 0.104405D-01 0.860950D+00 24 0.157702D-01 -0.183586D-02 -0.781996D-01 0.257678D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.170 1.000 3 -0.010 0.009 1.000 4 0.014 0.005 -0.144 1.000 5 0.011 0.007 0.015 0.031 1.000 6 0.002 0.025 0.032 -0.057 -0.040 7 -0.036 0.013 0.051 -0.051 0.065 8 -0.022 -0.008 -0.007 0.021 0.002 9 -0.091 0.022 -0.020 0.023 0.400 10 -0.035 -0.020 0.030 0.074 0.707 11 0.040 -0.030 -0.072 0.010 -0.259 12 -0.009 0.013 0.084 0.030 -0.047 13 -0.034 0.014 0.066 -0.029 0.010 14 0.033 -0.002 0.018 0.010 -0.001 15 -0.272 -0.007 0.010 0.029 -0.134 16 -0.006 -0.247 0.012 0.012 0.038 17 0.048 -0.001 -0.017 -0.059 -0.112 18 -0.008 0.085 0.029 0.015 0.095 19 0.046 -0.017 0.065 0.020 0.106 20 0.043 0.020 0.118 0.007 -0.019 21 -0.043 0.036 -0.073 0.018 -0.073 22 0.004 -0.109 0.018 -0.042 -0.121 23 0.024 0.041 -0.024 0.208 -0.008 24 -0.024 -0.027 0.016 -0.034 0.027 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.434 1.000 8 0.100 0.162 1.000 9 -0.172 -0.018 0.006 1.000 10 -0.105 0.064 0.025 0.294 1.000 11 0.119 -0.034 0.036 -0.153 -0.237 12 -0.088 0.004 0.113 0.102 0.012 13 0.480 0.569 0.122 -0.173 0.075 14 0.090 0.203 0.667 0.024 0.067 15 0.094 0.047 0.001 -0.110 -0.151 16 0.007 0.025 0.022 0.157 0.056 17 -0.064 -0.059 0.023 -0.147 -0.094 18 -0.106 -0.116 0.000 0.108 0.087 19 -0.108 0.027 0.058 0.042 0.133 20 -0.034 -0.032 -0.265 -0.018 -0.038 21 0.087 -0.028 -0.077 -0.010 -0.098 22 0.002 -0.035 -0.003 -0.076 -0.125 23 0.009 0.021 -0.017 -0.011 0.043 24 -0.005 -0.028 0.020 0.018 0.015 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 -0.066 1.000 13 -0.043 -0.068 1.000 14 -0.045 0.067 0.150 1.000 15 0.079 -0.020 0.077 -0.009 1.000 16 -0.051 -0.021 0.014 0.046 0.119 17 0.023 0.025 -0.048 -0.013 -0.603 18 -0.021 0.011 -0.081 0.017 -0.123 19 -0.024 0.043 -0.041 0.030 0.010 20 -0.007 -0.084 -0.005 -0.288 0.127 21 0.019 -0.061 0.029 -0.039 -0.008 22 0.005 0.024 -0.043 -0.030 0.066 23 -0.010 0.102 0.046 -0.033 0.038 24 -0.006 -0.067 -0.059 -0.017 -0.069 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.466 1.000 18 0.041 0.026 1.000 19 0.006 -0.007 0.073 1.000 20 0.042 -0.087 -0.070 0.012 1.000 21 0.005 -0.017 0.054 -0.844 -0.016 22 -0.043 0.020 -0.667 -0.072 0.076 23 0.029 -0.052 -0.043 -0.026 0.256 24 -0.056 0.036 0.076 0.006 -0.647 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.238 1.000 23 0.000 0.097 1.000 24 0.038 -0.098 -0.525 1.000
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//Funcao que recebe caminho da imagem e o t0 (Questao 1 - Celula ou Snowman) function [Img] = threshold (imagem,t); info = imfinfo(imagem); [Img] = gray_imread(imagem); for i=1:info.Height for j=1:info.Width if Img(i,j) > t then Img(i,j) = 0 else Img(i,j) = 1; end end end endfunction Caminho = input('Digite o caminho da imagem: '); T = input('Digite T: '); [Img] = threshold(Caminho,T); imshow(Img)
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clc; R1=2; //resisitance in Ohm R2=4; //resistance in Ohm R3=5; //resistance in Ohm R=(R1^-1)+(R2^-1)+(R3^-1); //calculating parallel resistance Rp=(1/R); disp(Rp,"Resisitance in Ohm = "); //displaying result
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// Example 13.1: dc input power, ac output power, Efficiency clc, clear Ib=5e-3; // Base current in amperes // From Fig. 13.8 RB=1.5e3; // in ohms RC=16; // in ohms bta=40; VCC=18; // in volts VBE=0.7; // in volts IBQ=(VCC-VBE)/RB; // in amperes ICQ=bta*IBQ; // in amperes Pi_dc=VCC*ICQ; // dc input power in watts Ic=bta*Ib; // in amperes Po_ac=Ic^2*RC; // ac output power eta=Po_ac*100/Pi_dc; // Efficiency in percentage disp(Pi_dc,"dc input power (W) ="); disp(Po_ac,"ac output power (W) ="); disp(eta,"Efficiency (%) =");
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// Harriot P., 2003, Chemical Reactor Design (I-Edition), Marcel Dekker, Inc., USA, pp 436. //Chapter-6 Ex6.4.a Pg No.251 //Title:Conversion in packed bed for same superficial velocity //==================================================================================================================== clear clc //INPUT L=2.5;//Lendth of bed(ft) X_A=0.95;//Conversion L_a=3;//Length of section a (ft) L_b=2;//Length of section b (ft) //CALCULATION k_rho_L_by_u=log(1/(1-X_A));//First Order reactions //For Section a k_rho_L_by_u_a=k_rho_L_by_u*(L_a/L); X_A_section_a=(1-exp(-k_rho_L_by_u_a)); //For Section b k_rho_L_by_u_b=k_rho_L_by_u*(L_b/L);//Dimensionless Group based on ideal plug flow for first order reaction X_A_section_b=(1-exp(-k_rho_L_by_u_b)); X_A_Ave=(X_A_section_b+X_A_section_a)/2; Percent_X_A_Ave=X_A_Ave*100 //OUTPUT //Console Output mprintf('\n\tThe average converion when each section has same superficial velocity:%0.1f%%',Percent_X_A_Ave ); //File Output fid= mopen('.\Chapter6_Ex4_a_Output.txt','w'); mfprintf(fid,'\n\tThe average converion when each section has same superficial velocity:%0.1f%%',Percent_X_A_Ave ); mclose(fid); //=======================================================END OF PROGRAM=================================================
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clc clear //Input data p1=1.05//Inlet pressure in kg/cm^2 T1=15+273//Inlet temperature in K p2=33.4//Pressure at the end of adiabatic compression in kg/cm^2 r=5//The ratio of expansion Cp=0.238//Specific heat at constant pressure in kJ/kg.K Cv=0.17//Specific heat at constant volume in kJ/kg.K g=1.4//Ratio of specific heats //Calculations r1=(p2/p1)^(1/g)//Compression ratio k=r1/r//Cutoff ratio T2=(p2/p1)^((g-1)/g)*T1//Temperature at the end of adiabatic compression in K T3=T2*k//Temperature at the end of constant pressure heat addition in K T4=T3*(1/r)^(g-1)//Temperature at the end of adiabatic expansion in K qa=(Cp*(T3-T2))//Heat added in kcal/kg of air qre=(Cv*(T4-T1))//Heat rejected in kcal/kg of air nt=((qa-qre)/qa)*100//Ideal thermal efficiency in percent //Output printf('The ideal thermal efficiency is %3.1f percent',nt)
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// Assumption, Bus 1 is considered as Slack bus. function gauss(report); global busdat; global linedat; Y = ybus(); // Calling program "ybus.sci" to get Y-Bus. busd = busdat; // Calling "busdatas.sci" for bus data. BMva= 100; // Base MVA bus = busd(:,1); // Bus number. nbus = max(bus); // To get no. of buses type_bus = busd(:,2); // Type of Bus 1-Slack, 2-PV, 3-PQ. V = busd(:,3); // Initial Bus Voltages. del = busd(:,4); // Initial Bus Voltage Angles. Pg = busd(:,5)/ BMva; // Pgi, Real Power injected into the buses. Qg = busd(:,6)/ BMva; // Qgi, Reactive Power injected into the buses. Pl = busd(:,7)/ BMva; // Pli, Real Power Drawn from the buses. Ql = busd(:,8)/ BMva; // QLi, Reactive Power Drawn from the buses. Qmin = busd(:,9)/ BMva; // Minimum Reactive Power Limit Qmax = busd(:,10)/ BMva; // Maximum Reactive Power Limit P = Pg-Pl; // Pi = PGi - PLi, Real Power at the buses. Q = Qg-Ql; // Qi = QGi - QLi, Reactive Power at the buses. Vprev = V; toler = 1; // Tolerence. iteration = 1; // iteration starting while (toler > 0.00001) // Start of while loop for i = 2:nbus sumyv = 0; for k = 1:nbus if i ~= k sumyv = sumyv + Y(i,k)* V(k); // Vk * Yik end end if type_bus(i) == 2 // Computing Qi for PV bus Q(i) = -imag(conj(V(i))*(sumyv + Y(i,i)*V(i))); if (Q(i) > Qmax(i)) | (Q(i) < Qmin(i)) // Checking for Qi Violation. if Q(i) < Qmin(i) // Whether violated the lower limit. Q(i) = Qmin(i); else // No, violated the upper limit. Q(i) = Qmax(i); end type_bus(i) = 3; // If Violated, change PV bus to PQ bus. end end V(i) = (1/Y(i,i))*((P(i)-(%i)*Q(i))/conj(V(i)) - sumyv); // Compute Bus Voltages. if type_bus(i) == 2 // For PV Buses, Voltage Magnitude remains same, but Angle changes. V(i) = pol2rect(abs(Vprev(i)), atan(imag(V(i)), real((V(i))))); end end iteration = iteration + 1; // Increment iteration count. toler = max(abs(abs(V) - abs(Vprev))); // Calculate tolerance. Vprev = V; // Vprev is required for next iteration, V(i) = pol2rect(abs(Vprev(i)), atan(imag(V(i)), real((V(i))); end // End of while loop / Iteration Ang = atan(imag(V), real(V)); // Final Bus Voltage Angles in Degree. loadflow(nbus, V, Ang, BMva, 'gs', report); endfunction
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clear clc Vt=10.95 V=11 S=100 I=round(S*1e7/(sqrt(3)*V*1e3))/10 //Error in evaluation of base current in textbook vt=Vt/V pf=.8 P=40 Il=round(P*1e7/(sqrt(3)*Vt*pf*1e3))/10 Il=Il * exp (%i * acos(pf))/I x1g=.2 x2g=.2 x0g=.05 Sm=50 x1m=.2 * S/Sm x2m=.2 * S/Sm x0m=.05 xt1=.05 xt2=.05 xt0=.15 V=vt+ (Il * %i * x0m) x0m=.05* S/Sm Ia1=V/(%i*((x1g*(x1m+xt1)/(x1g+x1m+xt1))+(x2g*(x2m+xt2)/(x2g+x2m+xt2))+(x0g*(x0m+xt0)/(x0g+x0m+xt0)))) Ia1=round(Ia1 * 1000)/1000 Ig1=round((Ia1 * (x1m + xt1)/(x1m+x1g+xt1) + Il)*1000)/1000 Im1=round((Ia1 * (x1g)/(x1m+x1g+xt1) - Il)*1000)/1000 Ig2=round((Ia1 * (x2m + xt2)/(x2m+x2g+xt2))*1000)/1000 Im2=round((Ia1 * (x2g)/(x2m+x2g+xt2))*1000)/1000 Ig0=round((Ia1 * (x0m + xt0)/(x0m+x0g+xt0))*100)/100 Im0=round((Ia1 * (x0g)/(x0m+x0g+xt0))*100)/100 Im=round((Im1+Im2+Im0)*1000) *1e-3 Ig=round((Ig1+Ig2+Ig0)*1000) *1e-3 mprintf("\nCurrent Through motor = %.2f, ang (%.1f) deg", abs(Im)*I, atand(imag(Im)/real(Im))+180) mprintf("\nCurrent Through generator = %.2f, ang (%.1f) deg", abs(Ig)*I, atand(imag(Ig)/real(Ig))) disp("Error in evaluation of base current in textbook")
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clear // //thevenin's theorem //all the values are derived from the figures z1=complex(8,-6) z2=complex(0,5) zth=(z1*z2)/(z1+z2) printf("\n zth") vth=complex(-17.71,141.54) zload=complex(4,3) I=vth/(zth+zload) printf("\n I")
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//Example 8.2 // Dipole moment of slab clc; clear; //given data : D=5D-4;// displacement vector magnitude in m2 P=4D-4;// Polarisation vector magnitude in m2 E=D-P;// Field Intensity in m2 V=.5;// volume of slab in m3 k=D/E;// dielectric contant p=P*V;//total dipole moment in m5 disp(k,"Dielectric constant") disp(p,"total dipole contant in m5")
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// sum 17-2 clc; clear; l=60; d=60; r=d/2; ho=0.008; c=0.04; S=0.0446; nj=1260/60; W=6000; p=W/(l*d); u=S*(c/r)^2*p/nj; u=u*10^9; // printing data in scilab o/p window printf("u is %0.3f cP ",u);
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mode(1) // // Demo of fminimax_v2.sci // // A basic case : // we provide only the objective function and the nonlinear constraint // function function f = myfun(x) f(1)= 2*x(1)^2 + x(2)^2 - 48*x(1) - 40*x(2) + 304; //Objectives f(2)= -x(1)^2 - 3*x(2)^2; f(3)= x(1) + 3*x(2) -18; f(4)= -x(1) - x(2); f(5)= x(1) + x(2) - 8; endfunction halt() // Press return to continue // The initial guess x0 = [0.1,0.1]; // The expected solution : only 4 digits are guaranteed xopt = [4 4] fopt = [0 -64 -2 -8 0] maxfopt = 0 // Run fminimax [x,fval,maxfval,exitflag,output,lambda] = fminimax(myfun, x0) halt() // Press return to continue // A case where we provide the gradient of the objective // functions and the Jacobian matrix of the constraints. // The objective function and its gradient function f = myfun(x) f(1)= 2*x(1)^2 + x(2)^2 - 48*x(1) - 40*x(2) + 304; f(2)= -x(1)^2 - 3*x(2)^2; f(3)= x(1) + 3*x(2) -18; f(4)= -x(1) - x(2); f(5)= x(1) + x(2) - 8; endfunction halt() // Press return to continue // Defining gradient of myfun function G = myfungrad(x) G = [ 4*x(1) - 48, -2*x(1), 1, -1, 1; 2*x(2) - 40, -6*x(2), 3, -1, 1; ]' endfunction halt() // Press return to continue halt() // Press return to continue // The nonlinear constraints and the Jacobian // matrix of the constraints function [c,ceq] = confungrad(x) // Inequality constraints c(1) = 1.5 + x(1)*x(2) - x(1) - x(2) c(2) = -x(1)*x(2) - 10 // No nonlinear equality constraints ceq=[] endfunction halt() // Press return to continue halt() // Press return to continue // Defining gradient of confungrad function [DC,DCeq] = cgrad(x) // DC(:,i) = gradient of the i-th constraint // DC = [ // Dc1/Dx1 Dc1/Dx2 // Dc2/Dx1 Dc2/Dx2 // ] DC= [ x(2)-1, -x(2) x(1)-1, -x(1) ]' DCeq = []' endfunction halt() // Press return to continue // Test with both gradient of objective and gradient of constraints minimaxOptions = list("GradObj","ON","GradCon","ON"); // The initial guess x0 = [0,10]; // The expected solution : only 4 digits are guaranteed xopt = [0.92791 7.93551] fopt = [6.73443 -189.778 6.73443 -8.86342 0.86342] maxfopt = 6.73443 // Run fminimax [x,fval,maxfval,exitflag,output] = fminimax(myfun,x0,[],[],[],[],[],[], confungrad,minimaxOptions,myfungrad,cgrad) halt() // Press return to continue halt() // Press return to continue //========= E N D === O F === D E M O =========//
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//LTi Systems characterized by Linear Constant //Coefficient Difference equations //Inverse Z Transform //z = %z; syms n z; H1 = (26/15)/(z-(1/2)); H2 = (7/3)/(z-2); H3 = (18/5)/(z-3); F1 = H1*z^(n)*(z-(1/2)); F2 = H2*z^(n)*(z-2); F3 = H3*z^(n)*(z-3); h1 = limit(F1,z,1/2); disp(h1,'h1[n]=') h2 = limit(F2,z,2); disp(h2,'h2[n]=') h3 = limit(F3,z,3); disp(h3,'h3[n]=') h = h1-h2+h3; disp(h,'h[n]=')
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function [x,y,typ]=CLINDUMMY_f(job,arg1,arg2) // Copyright INRIA x=[];y=[];typ=[] select job case 'plot' then standard_draw(arg1) case 'getinputs' then [x,y,typ]=standard_inputs(arg1) case 'getoutputs' then [x,y,typ]=standard_outputs(arg1) case 'getorigin' then [x,y]=standard_origin(arg1) case 'set' then x=arg1 x(3)(11)=[] //compatibility case 'define' then x0=0; model=list('cdummy',[],[],[],[],x0,[],[],[],'c',[],[%f %t],' ',list()) gr_i=['xstringb(orig(1),orig(2),[''DUMMY'';''CLSS''],sz(1),sz(2),''fill'');'] x=standard_define([3 2],model,[],gr_i) end
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//Exa 7.4 clc; clear; close; //Given data l=30;//in cm l=l*10^-2;//in meter A=1;//in cm^2 A=A*10^-4;//in meter^2 N=300;//turns of wire i=0.032;//in Ampere FI_B=2*10^-6;//in weber meu_o=4*%pi*10^-7;//permeability of free space in weber/amp-meter B=FI_B/A;//in weber/meter^2 disp(B,"Flux Density in weber/meter^2 : "); H=N*i/l;//in amp-turn/meter disp(H,"magnetic Intensity in amp-turn/meter : "); meu=B/H;//in weber/Amp-meter disp(meu,"Permeability in weber/amp-meter :"); meu_r=meu/meu_o;//Relative Permeability disp(meu_r,"Relative Permeability : "); //Answer of relative permeability is wrong in the book.
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//Example 4_4 clc; clear; close; format('v',6) //given data : c=3*10^8;//m/s//Speed of light h=1.05*10^-34;//Js//Planks Constant mc_GaAs=0.067;//mo mc_InAs=0.01;//mo k=0.01;///per Angstrum mc_GaAs=mc_GaAs*0.91*10^-30;//kg mc_InAs=mc_InAs*0.91*10^-30;//kg E_GaAs=h^2*(3*k*10^10)^2/2/mc_GaAs;//J E_GaAs=E_GaAs/(1.6*10^-19)*1000;//meV disp(E_GaAs,"Energy of the electron in GaAs(meV)"); E_InAs=h^2*(3*k*10^10)^2/2/mc_InAs;//J E_InAs=E_InAs/(1.6*10^-19)*1000;//meV disp(E_InAs,"Energy of the electron in InAs(meV)"); //Answer given in the textbook is wrong.
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//Example 7.14 // resistance clc; clear; close; //given data : alfa=20*10^-6; //resistance temperature coefficient in per degree celcius R=120; // in ohm E=400; // in MN/m^2 Gf=2; Me=200*10^9; // modulus of elasticity in N/m^2 Cs=(1/10)*E*10^6; // in N/m^2 e=Cs/Me; dR=R*Gf*e*10^3; // t=20; // temerature in degree celcius dR1=R*alfa*t*10^3; disp(dR,"resistance due to change in stress,dR(m-ohm) = ") disp(dR1,"resistance due to change of temperature,dR1(m-ohm) = ") //ANSWER IS WRONG IN THE TEXTBOOK
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//Chapter 6, Problem 10 clc; C1=6*10^-6; //Capacitance of capacitor1 C2=4*10^-6; //Capacitance of capacitor2 C3=C1+C2; //Calculating equivalent capacitance in parallel C4=(C1*C2)/(C1+C2); //Calculating equivalent capacitance in series disp("(a)"); printf("In parallel, equivalent capacitance = %f uF",C3*10^6); disp("(b)") ;printf("In series, equivalent capacitance = %f uF",C4*10^6);
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F=60;P=4;N=1740;R1=0.5; R2=0.5;X1=1;X2=1;Xm=35; I=1.1;Peak=10;H=5;H1=7; Phase=3; Ns=120*F/P S1=(Ns-N)/Ns A=R2/S1 Z1=(Xm*%i)*(A+X1*%i)/(A+X2*%i+Xm*%i) Rth=12.08; Pg1=Phase*((I*Peak)/sqrt(2))^2*Rth Wsyn=(Ns/60)*2*%pi T1=Pg1/Wsyn Ns1=-(120*H*F)/P S2=(Ns1-N)/Ns1 B=R2/S2 Xm1=H*Xm hX2=H*X2 Z2=Xm1*%i*(B+hX2*%i)/(B+hX2*%i+Xm1*%i) Rth2=0.39; Pg2=Phase*((0.22*Peak)/sqrt(2))^2*Rth2 Wsyn2=(Ns1/60)*2*%pi T2=Pg2/Wsyn2 Ns3=(120*H1*F)/P S3=(Ns3-N)/Ns3 C=R2/S3 Xm3=H1*Xm hX3=H1*X2 Z3=Xm3*%i*(C+hX3*%i)/(C+hX3*%i+Xm3*%i) Rth3=0.54; Pg3=Phase*((0.16*Peak)/sqrt(2))^2*Rth3 Wsyn3=(Ns3/60)*2*%pi T3=Pg3/Wsyn3
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clc //initialisation of variables A= 500 //cm^2 m= 0.106 //mg N= 6*10^23 //molecules M= 284 //g mole^-1 d= 0.85 //g/cm^3 //CALCULATIONS A1= A*M/(N*m^10^-3) t= m*10^-3/(A*d) //RESULTS printf ('cross-sectional area = %.e cm^2 ',A1) printf ('\n thcikness t of the film = %.e cm ',t)
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//sinal 1 - Estela load('./xa_10_1.sod') S1 = x_a //sinal 2- Lais load('./xa_26_1.sod') S2 = x_a //sinal 3 - Willane load('./xa_43_1.sod') S3 = x_a S = [S1 S2 S3] function sigDelta = modDelta(sinal,tempoFim, passo, delta) sigDelta(1) = 0; for k=1:tempoFim/passo e(k) = sinal(k) - sigDelta(k); //sinal de erro e_q(k) = delta*sign(e(k)); //versão quantizada sigDelta(k+1) = sigDelta(k) + e_q(k); //aprox. do sinal quantizado end endfunction passo = 1e-2; tempoFinal = 2; delta = 0.1; t1 = 0 : 1/200 : 1 sinalFinal = modDelta(S,tempoFinal,passo,delta) plot2d3(t1,sinalFinal)
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errcatch(-1,"stop");mode(2);//Ex19_13 Pg-962 dec=175; //binary input oct=dec2oct(dec) //decimal output disp("The octal equivslent of 175 is") disp(oct) exit();
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clear; clc; printf("\t\t\tExample Number 7.6\n\n\n"); // cube cooling in air // Example 7.6 (page no.-336) // solution L = 0.2;// [m] side length of cube Ts = 60;// [degree celsius] surface temperature of cube Ta = 10;// [degree celsius] air temperature // this is an irregular solid so we use the information in the last entry of table 7-1(page no.-328) in the absence of a specific correlation for this geometry. // the properties were evaluated as v = 17.47*10^(-6);// [square meter/s] k = 0.02685;// [W/m degree celsius] Pr = 0.70;// prandtl number Beta = 3.25*10^(-3);// [K^(-1)] g = 9.8;// [square meter/s] acceleration due to gravity // the characteristic length is the distance a particle travels in the boundary layer, which is L/2 along the bottom plus L along the side plus L/2 on the top or Gr_into_Pr = (g*Beta*(Ts-Ta)*(2*L)^(3)*Pr)/(v^(2)); // from the last entry in table 7-1 we find C = 0.52; n = 1/4; // so that Nu = C*(Gr_into_Pr)^(n); h_bar = Nu*k/(2*L);// [W/square meter degree celsius] // the cube has six sides so the area is A = 6*L^(2);// [square meter] // the heat required is q = h_bar*A*(Ts-Ta);// [W] printf("heat transfer is %f W",q);
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b=[0.5 1 2 -3]; a=[1 1 -0.5]; n=3; [phi]=phasedelay(b,a,n)
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//Example 6.8 clc;clear;close; L=3;A=1/4; x=A*ones(1,L); //Calculation of DFT X=dft(x,-1); X=clean(X); disp(x,'Given Sequence is x(n): '); disp(X,'DFT of the Sequence is X(k): ');
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//Section-5,Example-3,Page no.-D.12 //To find the percentage of R_1 and R_2 left unreacted. clc; R_0=1 //(let) t_1=30 R_t=0.75*R_0 k_1=(2.303/t_1)*(log10(R_0/R_t)) t_2=35 R1_t=(R_0)/(10^((k_1*t_2)/2.303)) R1_tpr=100*R1_t disp(R1_tpr,'Percentage of R_1 left unreacted(%)') k_O=(1/t_1)*((1/R_t)-(1/R_0)) R2_t=(R_0)/((k_O*t_2)+R_0) R2_tpr=100*R2_t disp(R2_tpr,'Percentage of R_2 left unreacted(%)')
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ex1_1.sce
// Exa 1.1 clc; clear; close; format('v',5) // Given data R1=4;// in ohm R2= 6;// in ohm R3= 2;// in ohm V1= 24;// in V V2= 12;// in V // Applying KVL in Mesh ABEFA, V1 = (R1+R3)*I1 - R3*I2 (i) // Applying KVL in Mesh BCDEB, V2 = R3*I1 - (R2+R3)*I2 (ii) A= [(R1+R3) R3;-R3 -(R2+R3)];// assumed B= [V1 V2];// assumed I= B*A^-1;// Solving equations by matrix multiplication I1= I(1);// in A I2= I(2);// in A disp(I1,"The current through 4 ohm resistor in A is"); // current through 2 ohm resistor I= I1-I2;// in A disp(I,"The current through 2 ohm resistor in A is"); disp(I2,"The current through 6 ohm resistor in A is"); disp("That is "+string(abs(I2))+" A current flows in 6 ohm resistor from C to B")
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loadIPT.sce
exec macros/show.sci exec macros/imshow.sci exec macros/modified_if.sci exec macros/cmp.sci exec loader.sce //exec Octave/loader.sce exec macros/il2mat.sci exec macros/mat2il.sci S = dir('macros/more') for x=1:size(S(2), 1) exec('macros/more/'+S(2)(x)) end clear S clear x
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Ex17_14.sce
clear //Given u=-9.0 //cm y=1 y1=1.5 R=-15.0 //cm //Calculation v=1/(((y-y1)/R)-(y1/-u)) //Result printf("\n The value of distance is %0.3f cm",v)
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Ex2_48.sce
//CHAPTER 2- STEADY-STATE ANALYSIS OF SINGLE-PHASE A.C. CIRCUIT //Example 48 clc; disp("CHAPTER 2"); disp("EXAMPLE 48"); //VARIABLE INITIALIZATION pf1=0.8; //power factor of 1st circuit pf2=0.6; //power factor of 2nd circuit z=1; //this is an assumption //SOLUTION angle1=acos(pf1)*(180/%pi); //in degrees angle2=acos(pf2)*(180/%pi); //in degrees //function to convert from polar form to rectangular form function [x,y]=pol2rect(mag,angle); x=mag*cos(angle*(%pi/180)); //to convert the angle from degrees to radians y=mag*sin(angle*(%pi/180)); endfunction; [z1_x,z1_y]=pol2rect(z,angle1); [z2_x,z2_y]=pol2rect(z,angle2); nr=angle1+angle2; //numerator z_x=z1_x+z2_x; z_y=z1_y+z2_y; //function to convert from rectangular form to polar form function [z,angle]=rect2pol(x,y); I=sqrt((x^2)+(y^2)); angle=atan(y/x)*(180/%pi); //to convert the angle from radians to degrees endfunction; [z,angle]=rect2pol(z_x,z_y); angle_z=nr-angle; pf=cos(angle_z*(%pi/180)); disp(sprintf("The power factor of the combination is %f",pf)); //END
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ex3_5.sce
clc;clear; //Example 3.5 //given data Z=1; n=1; e=1.6*10^-19;//the charge on electron in C h=6.625*10^-34;//Plank's constant Eo=8.854*10^-12;//absolute permitivity of free space in F/m m=9.12*10^-31;//mass of electron in kg //calculations v=Z*e^2/(2*Eo*n*h); disp(v,'velcocity in m/s'); E=-m*Z^2*e^4/(8*(Eo*n*h)^2); disp(E,'energy of hydrogen atom in J'); f=m*Z^2*e^4/(4*Eo^2*(n*h)^3); disp(f,'frequecy in Hz')
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Ex6_12_7.sce
//Section-6,Example-1,Page no.-P.38 //To find the partial vapour pressure of benzene in the solution. clc; n_B=1000/78 n_n=1.5 p_Bbar=94.6 x_B=n_B/(n_B+n_n) p_B=x_B*p_Bbar disp(p_B,'Partial vapour pressure of benzene(Torr)')
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treinamentoRede_ESTOCASTICO.sce
clear; path_treina_ESTOCASTICO = get_absolute_file_path('treinamentoRede_ESTOCASTICO.sce'); exec( path_treina_ESTOCASTICO+"\..\..\..\_treinamento.sce" ); treinar( path_treina_ESTOCASTICO, "ESTOCASTICO" );
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main.sce
b = chdir('/home/elena/Documents/week2/lab_2'); exec('ADC.sce'); function noise=get_sinus(sin_freq, fs, sin_ampl) step_size = sin_freq*(2*%pi)/fs; part_len = size(recorded_data, "r") / fs samples = (1:fs*part_len)*step_size; noise = mtlb_t(sin_ampl*sin(samples)); endfunction function try_frequencies(n, record,fs, sin_ampl) f =figure(n); clf; counter = 1; for sin_freq = 120:10:210 noise = get_sinus(sin_freq, fs, sin_ampl); cleaned = record - noise; subplot(4,3,counter); plot(cleaned); xlabel('samples'); ylabel('Amplitude'); title('Cleaned record for sin frequency ' + string(sin_freq)); counter = counter + 1; show_window(n); xname('Frame number ' + string(n)); end endfunction quant_levels = (-1:0.001:0.5); sin_ampl = 0.1; fs_s =[32000, 22050, 32050, 22050, 32050, 32000, 32000 ,22050, 22050, 22050, 32000, 32000, 22050, 32000]; freq_s =[200, 150, 180, 120, 210, 180, 140, 120, 150, 210, 150, 190, 140, 210]; // The part required to find frequences /* for n=1:14 fs = fs_s(n); recorded_data = ADC(n, quant_levels, fs); shift = mean(recorded_data); try_frequencies(n, recorded_data, fs); end */ result = []; original_s = []; for n=1:14 recorded_data = ADC(n, quant_levels, fs_s(n)); shift = mean(recorded_data); recorded_data = recorded_data - shift; cleaned = recorded_data - get_sinus(freq_s(n), fs_s(n), sin_ampl); result(n).entries = cleaned; original_s(n).entries = recorded_data; //playsnd(cleaned, fs_s(n)); end for n=1:14 playsnd(result(n).entries, fs_s(n)); end
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Ex18_4.sce
//Example 18.4// n=8;//numbers Ni2+/ unit cell n1=2; //moment of Ni2+ m=n*n1 mprintf("m = %i ",m) a=18.4;// measured value of nickel ferrite e=((a-m)/a)*100 mprintf("\ne = %i percent",e)
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24_3.sce
clc //initialisation of variables R= 0.08205 //l-atm mole^-1 K^-1 T= 25 //C p= 1 //atm Mr= 226 //gms th= 3.82 //days t= 1620 //years //CALCULATIONS NRn= th/(Mr*t*365.26) V= NRn*R*(273+T)*1000/p //RESULTS printf ('millilitres of radon = %.2e ml',V)
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Exa_10_10.sce
//Maximally flat FIR filter design Fp=0.2; Fs=0.4; Fc=0.3; Ft=0.2; N0=1+0.5/Ft^2; N0=ceil(N0); alpha=(cos(%pi*Fc))^2; k=5;Mmin=14; L=Mmin-k; N=2*Mmin-1; disp(N,'Hence with this length we can get maximally flat FIR filter with no ripples in passband');
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clc; Voutpk=8; //volt Vf=1.8; //volt If=0.02; //Ampere Rs=(Voutpk-Vf)/If; //Ohm//v=r*i disp('Ohm',Rs,"Rs=");
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Ch010Ex1.sce
// Scilab code Ex10.1 : Pg:405 (2008) clc;clear; E = 1000; // Electric field applied to sodium chloride crystal, V/m P = 4.3e-008; // Polarization, Coulomb per meter square epsilon_0 = 8.85e-012; // Permittivity of free space, force per meter // Since P = epsilon_0*(epsilon_r-1)*E, solving for epsilon_r epsilon_r = 1 + P/(epsilon_0*E); // Relative permittivity of sodium chloride printf("\nThe relative permittivity of sodium chloride = %4.2f ", epsilon_r); // Result // The relative permittivity of sodium chloride = 5.86
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# REFERENCE: # EMSOFT paper inf = float('inf') plant_pvt_init_data = None # x0 = np.array([4, 5], [21, 22]) # v0 = np.array([[0.2, 0.5], [-0.5, 0.5]]) # Property initial_set = [[4.0, 21.0, -1.0, -1.0], [5.0, 22.0, 1.0, 1.0]] #initial_set = [[5., 21.22936519, -0.959, 0.], # [5., 21.22936519, -0.959, 0.078]] P = [[6., 7., -inf, -inf], [7., 8., inf, inf]] Q = [[7., 9., -inf, -inf], [8., 10., inf, inf]] R = [[1., 6., -inf, -inf], [2., 7., inf, inf]] S = [[22., 11., -inf, -inf], [23., 12., inf, inf]] error_set = R # P, Q, R T = 20.0 # S # T = 35.0 # Abstraction params: P, Q, R, S #grid_eps = [0.2, 0.2, 0.4, 0.4] grid_eps = [0.51]*4 delta_t = 5.0 num_samples = 5 MAX_ITER = 4 plant_description = 'python' plant_path = 'nav30.py' ############################################# ############## Don't care params ############ ############################################# initial_controller_integer_state = [] initial_controller_float_state = [] num_control_inputs = 0 min_smt_sample_dist = 0 ci = [[], []] pi = [[],[]] controller_path = None controller_path_dir_path = None initial_discrete_state = [] initial_private_state = [] # Viloations # # S # x0=[ 4.14327461 21.51742883 0.8471542 0.9884877 ] -> x=[ 22.44414369 11.999 0.22792075 -0.86384343], t=30.1382177243 # x0=[ 4.50024758 21.82478644 0.97146715 0.6993149 ] -> x=[ 22.4524101 11.999 0.22748131 -0.86401213], t=30.1798284278
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// File name: projects/01/Repeater16.tst load Repeater16.hdl, output-file Repeater16.out, compare-to Repeater16.cmp, output-list in%B3.1.3 out%B1.16.1; set in 0, eval, output; set in 1, eval, output;
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example8_1.sce
clear; clc; //Example8.1[Heating of water in a tube by Steam] //Given:- id=0.025;//Internal diameter[m] Tin=15;//Initial temp[degree Celcius] m_=0.3;//Flow rate[kg/s] h=800/1000;//avg heat transfer coefficient[W/m^2.degree Celcius] Tf=115;//Final temp of water[degree Celcius] Ts=120;//[degree Celcius] Hs=2203;//Heat of condensation of steam at 120 degree Celcius[kJ/kg] Tavg=(Tin+Tf)/2;//[degree Celcius] Cp=4187;//Sp Heat of water at Tavg[J/kg.degree Celcius] //Solution:- Q_=m_*Cp*(Tf-Tin)/1000;//[kW] disp("kW",Q_,"The rate of heat transfer is") del_Tf=Ts-Tf;//[degree Celcius] del_Tin=Ts-Tin;//[degree Celcius] ln_del_T=(del_Tf-del_Tin)/(log(del_Tf/del_Tin));//[degree Celcius] disp("degree Celcius",ln_del_T,"Logrithmic Mean temperature difference is") A=Q_/(h*ln_del_T);//[m^2] disp("m^2",A,"Heat Transfer surface area is") l=A/(%pi*id);//[m] disp("m",round(l),"Required tube length is")
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// Scilab code Exa11.3 : : Page-536 (2011) clc; clear; f = 200*10^6; // Frequency of the accelerator, cycle per sec M = 1.6724e-27; // Mass of the proton, Kg E = 45.3*1.6e-13; // Accelerating energy, joule L_f = round (1/f*sqrt(2*E/M)*100); // Length of the final drift tube, centi metre L_1 = 5.35*10^-2; // Length of the first drift tube, metre K_E = (1/2*M*L_1^2*f^2)/1.6e-13; // Kinetic energy of the injected proton, MeV E_inc = E/1.6e-13-K_E; // Increase in energy, MeV q = 1.6e-19; // Charge of the proton, C V = 1.49e+06; // Accelerating voltage, volts N = E_inc*1.6e-13/(q*V); // Number of drift protons L = 1/f*sqrt(2*q*V/M)*integrate('n^(1/2)', 'n', 0, N); // Total length of the accelerator, metre printf("\nThe length of the final drift tube = %d cm\nThe kinetic energy of the injected protons = %4.2f MeV\nThe total length of the accelerator = %3.1f metre", L_f, K_E, L); // Result // The length of the final drift tube = 47 cm // The kinetic energy of the injected protons = 0.60 MeV // The total length of the accelerator = 9.2 metre
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//Example_a_6_4 page no:235 clc; R1=5; I5mag=sqrt(600/5); V=I5mag*sqrt(50); apparent_power=3000; Itmag=apparent_power/V; Itang=45; I5ang=-45; Itreal=Itmag*cosd(Itang); Itimag=Itmag*sind(Itang); It=Itreal+(Itimag*%i); I5real=I5mag*cosd(I5ang); I5imag=I5mag*sind(I5ang); I5=I5real+(I5imag*%i); Iz=It-I5; Izmag=sqrt(real(Iz)^2+imag(Iz)^2); Izang=atand(imag(Iz)/real(Iz)); Zmag=V/Izmag; Zang=0-Izang; disp(Zmag,"the magnitude of impedence is (in ohm)"); disp(Zang,"the angle of impedence is (in degree)");
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clear; clc; disp("--------------Example 3.17---------------") L=9; // number of levels bits_per_level=log2(L); // formula to calculate number of bits per level printf("The number of bits per level is %3.2f bits.\n",bits_per_level); if(~(bits_per_level/10 == 0)) // if the number of bits is not an integer or power of 2 printf("This answer is not realistic. The number of bits sent per level needs to be an integer as well as a power of 2.\n"); r=nextpow2(bits_per_level); // find nearesr power of 2 bits=2^r; printf("Therefore %d bits can represent one level.",bits); // display result end
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clear; clc; //Caption:SCR Relaxation Oscillator Phase control Circuit //Given Data C=0.1;//in microF V=60;//in V Vb=32;//in V Vh=10;//holding voltage in V Ih=100;//in microA c=45;//conductance angle in degree cd = 360 - c;//angle in which capacitor will get charged td = (cd/360)*(1/60);//in ms //if the anode voltage is positive,the SCR will fire when vc=32V vc=32;//in V //let time constant = t = R*C //vc-Vh = (V-Vh)(1-exp(-td/t)) t = -td/log(1-((vc-Vh)/(V-Vh))); disp('sec',t,'time constant = '); R = t/C;//Resistance in K disp('K',R*1000,'R='); //end
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//Example 9.8: Reduction of state table clc // Clears the console disp("Given State Table") disp("q | x=0 x=1 | z") disp('--------------------------------') disp("A | C D | 1") disp("B | C D | 0") disp("C | B D | 1") disp("D | C A | 1") disp('Step 1 produces five SP Partitions') disp('P1 = (AB)(C)(D)') disp('P2 = (ABC)(D)') disp('P3 = (AD)(B)(C)') disp('P4 = (A)(BC)(D)') disp('P5 = (ABD)(C)') disp('Step 2 requires three sums') disp('P1 + P3 = (ABD)(C)--> P5') disp('P1 + P4 = (ABC)(D)--> P2') disp('P3 + P4 = (AD)(BC)--> P6') disp('only one new partition is found by step 2.')
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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 0.354193D+00 2 -0.241634D-02 0.301726D-02 3 0.162580D+00 -0.259457D-02 0.282286D+00 4 -0.256243D-02 0.115641D-02 -0.561260D-02 0.214152D-02 5 -0.534605D-03 0.112312D-03 -0.144546D-02 0.279951D-03 0.277590D-02 6 0.172132D-02 0.841078D-06 0.159235D-02 0.426053D-04 0.401311D-04 7 -0.152660D-02 0.611933D-04 -0.156427D-02 0.172355D-03 0.209245D-03 8 0.228686D-02 0.382661D-04 0.164616D-02 -0.311573D-04 0.222813D-03 9 -0.110352D+00 0.174329D-01 -0.122380D+00 0.699754D-02 0.101033D+00 10 -0.154913D+00 0.149672D-01 -0.241888D-01 0.310189D-01 0.196668D+00 11 -0.523176D-01 0.192870D-01 0.472688D-01 0.111615D-01 0.391342D-01 12 -0.719955D+00 0.176271D-01 -0.551598D+00 0.137790D-01 0.440325D-01 13 -0.104545D-01 -0.295588D-03 -0.398696D-01 0.580292D-02 0.302493D-01 14 -0.126956D+00 0.352900D-02 -0.329751D+00 0.130281D-01 0.317054D-01 15 -0.806744D+00 0.799696D-01 -0.518627D+00 0.451835D-01 -0.140975D+00 16 -0.383080D-01 -0.123425D-01 0.853968D-02 -0.711701D-02 0.646628D-03 17 -0.119121D-01 -0.212261D-02 -0.723236D-02 -0.740800D-03 -0.590139D-03 18 -0.794365D+00 0.392253D-01 -0.118658D+01 0.618212D-01 -0.135971D-01 19 -0.909690D-01 -0.528200D-02 0.750151D-01 -0.725195D-02 0.615677D-02 20 -0.145249D+01 0.561337D-01 -0.250066D+01 0.783909D-01 -0.240571D-01 21 0.957913D-01 -0.665474D-02 -0.454444D-03 -0.938396D-02 -0.631939D-02 22 -0.419541D-02 -0.648230D-03 -0.594144D-02 -0.362999D-03 -0.318523D-03 23 0.286564D-01 -0.714902D-02 0.358307D-01 -0.859080D-02 -0.590718D-03 24 -0.262465D-02 -0.171025D-03 0.654917D-03 -0.642929D-04 -0.530211D-05 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.169826D-02 7 0.865380D-03 0.193166D-02 8 0.397990D-03 -0.997411D-04 0.285803D-02 9 0.286857D-01 0.506565D-01 0.555724D-01 0.794361D+02 10 0.342979D-01 0.371839D-01 0.508864D-02 0.482245D+01 0.330275D+02 11 0.515191D-01 0.697213D-01 0.350805D-01 0.202327D+02 0.383115D+01 12 0.213443D-02 0.347014D-01 -0.123064D-02 0.265976D+02 0.653476D+01 13 0.961993D-01 0.949282D-01 0.187523D-01 0.220616D+01 0.674895D+01 14 0.455001D-01 0.450966D-01 0.110568D+00 0.722012D+01 0.420373D+01 15 -0.347129D-01 0.114180D-01 -0.949925D-01 -0.104491D+02 -0.212457D+02 16 -0.104238D-02 -0.155295D-02 -0.150797D-02 0.499497D+00 -0.576510D-01 17 -0.101346D-03 -0.229718D-03 0.458852D-03 -0.211989D+00 -0.280464D-01 18 -0.997151D-01 -0.633466D-01 -0.127520D+00 -0.564453D+01 -0.704432D+01 19 -0.150703D-01 0.779388D-03 -0.410318D-02 -0.289434D+00 0.592003D+00 20 -0.646657D-01 -0.864149D-02 -0.224468D+00 -0.709091D+01 -0.118902D+01 21 0.116435D-01 -0.642389D-02 0.998203D-03 0.718337D+00 -0.704696D+00 22 -0.912613D-04 -0.864259D-04 0.616073D-03 -0.900401D-01 -0.181096D-01 23 -0.987599D-03 -0.406296D-02 -0.399783D-02 0.239021D+00 -0.772791D-01 24 -0.866079D-05 0.166457D-03 0.725030D-03 -0.663681D-01 -0.137826D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.530018D+02 12 0.525381D+01 0.114498D+03 13 0.390074D+01 0.131824D+01 0.134089D+02 14 0.118798D+01 0.323775D+01 0.561437D+01 0.280002D+02 15 -0.338916D+01 0.933331D+00 -0.272122D+01 -0.786758D+01 0.373396D+03 16 -0.144721D-01 0.514389D+00 -0.700815D-01 -0.684237D-01 0.868892D+00 17 -0.107663D+00 -0.143297D+00 -0.200447D-02 0.363599D-01 -0.184785D+01 18 -0.956860D+01 -0.863578D+01 -0.753951D+01 -0.102393D+02 0.188726D+03 19 0.351121D+00 0.313562D+01 -0.394874D+00 -0.793658D+00 0.132152D+01 20 -0.582468D+00 -0.173651D+02 -0.384628D+01 -0.163941D+02 0.998942D+02 21 0.342734D+00 -0.264029D+01 -0.952103D-02 0.475155D+00 -0.188711D+01 22 -0.912384D-01 -0.411500D-01 -0.406675D-02 0.601828D-01 -0.896481D+00 23 0.345647D+00 0.673132D+00 -0.296767D+00 -0.290040D+00 -0.917630D+00 24 -0.741128D-01 -0.904412D-01 0.224074D-01 0.616321D-01 -0.375173D+00 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.509883D+00 17 -0.178938D-01 0.219180D-01 18 -0.121139D+00 -0.946608D+00 0.210278D+03 19 0.283011D+00 -0.322293D-01 0.170950D+01 0.372891D+01 20 -0.795328D+00 -0.456350D+00 0.152568D+03 0.142442D+01 0.247762D+03 21 0.272633D+00 0.600199D-02 -0.167448D+01 -0.311840D+01 -0.223970D+01 22 -0.118092D-01 0.114765D-01 -0.925171D+00 -0.421990D-01 -0.633637D+00 23 0.199107D+00 -0.716629D-02 -0.759853D+00 0.135844D+00 0.709220D+00 24 -0.603461D-02 0.650041D-02 -0.527936D+00 -0.233101D-01 -0.962974D+00 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.404831D+01 22 -0.268024D-02 0.121617D-01 23 0.514577D+00 -0.208759D-01 0.557528D+00 24 -0.217414D-01 0.816735D-02 -0.512500D-01 0.124184D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.074 1.000 3 0.514 -0.089 1.000 4 -0.093 0.455 -0.228 1.000 5 -0.017 0.039 -0.052 0.115 1.000 6 0.070 0.000 0.073 0.022 0.018 7 -0.058 0.025 -0.067 0.085 0.090 8 0.072 0.013 0.058 -0.013 0.079 9 -0.021 0.036 -0.026 0.017 0.215 10 -0.045 0.047 -0.008 0.117 0.650 11 -0.012 0.048 0.012 0.033 0.102 12 -0.113 0.030 -0.097 0.028 0.078 13 -0.005 -0.001 -0.020 0.034 0.157 14 -0.040 0.012 -0.117 0.053 0.114 15 -0.070 0.075 -0.051 0.051 -0.138 16 -0.090 -0.315 0.023 -0.215 0.017 17 -0.135 -0.261 -0.092 -0.108 -0.076 18 -0.092 0.049 -0.154 0.092 -0.018 19 -0.079 -0.050 0.073 -0.081 0.061 20 -0.155 0.065 -0.299 0.108 -0.029 21 0.080 -0.060 0.000 -0.101 -0.060 22 -0.064 -0.107 -0.101 -0.071 -0.055 23 0.064 -0.174 0.090 -0.249 -0.015 24 -0.040 -0.028 0.011 -0.012 -0.001 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.478 1.000 8 0.181 -0.042 1.000 9 0.078 0.129 0.117 1.000 10 0.145 0.147 0.017 0.094 1.000 11 0.172 0.218 0.090 0.312 0.092 12 0.005 0.074 -0.002 0.279 0.106 13 0.637 0.590 0.096 0.068 0.321 14 0.209 0.194 0.391 0.153 0.138 15 -0.044 0.013 -0.092 -0.061 -0.191 16 -0.035 -0.049 -0.040 0.078 -0.014 17 -0.017 -0.035 0.058 -0.161 -0.033 18 -0.167 -0.099 -0.164 -0.044 -0.085 19 -0.189 0.009 -0.040 -0.017 0.053 20 -0.100 -0.012 -0.267 -0.051 -0.013 21 0.140 -0.073 0.009 0.040 -0.061 22 -0.020 -0.018 0.104 -0.092 -0.029 23 -0.032 -0.124 -0.100 0.036 -0.018 24 -0.002 0.034 0.122 -0.067 -0.022 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 0.067 1.000 13 0.146 0.034 1.000 14 0.031 0.057 0.290 1.000 15 -0.024 0.005 -0.038 -0.077 1.000 16 -0.003 0.067 -0.027 -0.018 0.063 17 -0.100 -0.090 -0.004 0.046 -0.646 18 -0.091 -0.056 -0.142 -0.133 0.674 19 0.025 0.152 -0.056 -0.078 0.035 20 -0.005 -0.103 -0.067 -0.197 0.328 21 0.023 -0.123 -0.001 0.045 -0.049 22 -0.114 -0.035 -0.010 0.103 -0.421 23 0.064 0.084 -0.109 -0.073 -0.064 24 -0.091 -0.076 0.055 0.105 -0.174 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.169 1.000 18 -0.012 -0.441 1.000 19 0.205 -0.113 0.061 1.000 20 -0.071 -0.196 0.668 0.047 1.000 21 0.190 0.020 -0.057 -0.803 -0.071 22 -0.150 0.703 -0.579 -0.198 -0.365 23 0.373 -0.065 -0.070 0.094 0.060 24 -0.076 0.394 -0.327 -0.108 -0.549 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.012 1.000 23 0.343 -0.254 1.000 24 -0.097 0.665 -0.616 1.000
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clf; clear; t = 0:0.01:20 function ts=f(t) if t<2 then ts = sin (10*t) else ts = 0 end endfunction subplot(221); plot(t,f); function ns=f2(t) ns = (sin (4*t)/5 - sin (2*t)/5 + sin (9*t)/7 - sin(8*t)/6)/2 ; endfunction rd = grand(1,1,"uin",2,9); subplot(222) plot(t,f2); function rs=f1(t) // rs = (f(t-rd)*14)/15 + f2(t); if t>rd&t<(2+rd) then rs = (f(t-rd)*14)/15 + f2(t); //sin (4*t)/5 - sin (2*t)/5 + sin (9*t)/7 - sin(8*t)/6 ; else rs = f2(t);//sin (4*t)/5 - sin (2*t)/5 + sin (9*t)/7 - sin(8*t)/6; end endfunction subplot(223) plot(t,f1); for n = 1:11 function ts1=f0(t) ts1 = f(t-n) endfunction function new=g(t) new = f0(t) * f1(t); endfunction intvalue = intg(0,20,g); if n==1 then td=n maxi= intvalue else if intvalue>maxi then td=n maxi=intvalue end end end disp(td,"Delay : ");
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// A Textbook of Fluid Mecahnics and Hydraulic Machines - By R K Bansal // Chapter 1-Properties of Fluid // Problem 1.20 //Given Data Set in the Problem(SI Units) w=16 t=25 T=273+t p=0.25*10^6 g=9.81 //Calculations //1)Density density=w/g mprintf("The Density of the gas is %f kg/m^3 \n",density) //2)Gas consatnt R=p/(density*T) mprintf("The gas constant is %f Nm/kg-K \n",R)
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@relation abalone @attribute Sex{M,F,I} @attribute Length real[0.075,0.815] @attribute Diameter real[0.055,0.65] @attribute Height real[0.0,1.13] @attribute Whole_weight real[0.002,2.8255] @attribute Shucked_weight real[0.001,1.488] @attribute Viscera_weight real[5.0E-4,0.76] @attribute Shell_weight real[0.0015,1.005] @attribute Rings{15,7,9,10,8,20,16,19,14,11,12,18,13,5,4,6,21,17,22,1,3,26,23,29,2,27,25,24} @inputs Sex,Length,Diameter,Height,Whole_weight,Shucked_weight,Viscera_weight,Shell_weight @outputs Rings @data 9 7 10 7 12 7 10 7 12 7 18 7 8 7 7 7 9 7 13 7 9 7 12 7 13 7 9 7 9 7 10 7 5 7 14 7 9 7 14 7 8 7 9 7 9 7 14 7 22 7 3 7 5 7 10 7 7 7 15 7 13 7 12 7 4 7 19 7 5 7 8 7 9 7 8 7 20 7 16 7 15 7 12 7 14 7 6 7 14 7 11 7 9 7 8 7 19 7 16 7 17 7 21 7 16 7 15 7 15 7 10 7 6 7 5 7 20 7 10 7 14 7 10 7 7 7 13 7 13 7 13 7 10 7 12 7 17 7 8 7 9 7 7 7 10 7 10 7 2 7 15 7 14 7 13 7 20 7 13 7 15 7 9 7 11 7 10 7 6 7 9 7 10 7 12 7 8 7 8 7 12 7 11 7 9 7 4 7 6 7 6 7 7 7 7 7 7 7 8 7 7 7 9 7 9 7 11 7 8 7 10 7 8 7 11 7 10 7 11 7 6 7 7 7 6 7 8 7 9 7 9 7 7 7 9 7 10 7 9 7 9 7 9 7 11 7 5 7 5 7 4 7 7 7 6 7 7 7 6 7 7 7 7 7 10 7 9 7 10 7 8 7 10 7 10 7 9 7 9 7 10 7 12 7 9 7 10 7 10 7 12 7 12 7 12 7 14 7 6 7 6 7 8 7 8 7 11 7 10 7 10 7 5 7 8 7 7 7 6 7 7 7 6 7 8 7 7 7 9 7 8 7 10 7 10 7 10 7 10 7 10 7 11 7 10 7 11 7 9 7 9 7 9 7 11 7 14 7 7 7 8 7 10 7 10 7 9 7 8 7 8 7 9 7 8 7 8 7 9 7 9 7 9 7 8 7 11 7 9 7 11 7 11 7 10 7 10 7 11 7 9 7 10 7 10 7 12 7 10 7 12 7 4 7 6 7 7 7 8 7 7 7 9 7 9 7 9 7 11 7 8 7 6 7 12 7 9 7 9 7 12 7 17 7 10 7 8 7 9 7 7 7 6 7 6 7 12 7 13 7 9 7 12 7 16 7 14 7 13 7 12 7 15 7 23 7 18 7 12 7 18 7 5 7 16 7 11 7 17 7 12 7 10 7 10 7 10 15 15 7 10 7 6 7 5 7 17 7 14 7 14 7 19 7 6 7 7 7 8 7 11 7 13 7 13 7 7 7 6 7 7 7 11 7 9 7 13 7 10 7 5 7 8 7 6 7 9 7 8 7 9 7 9 7 8 7 9 7 8 7 9 7 9 7 9 7 8 7 10 7 11 7 8 7 11 7 8 7 11 7 11 7 10 7 4 7 7 7 9 7 10 7 12 7 11 7 11 7 6 7 11 7 9 7 8 7 11 7 9 7 11 7 10 7 10 7 10 7 8 7 9 7 8 7 8 7 10 7 10 7 8 7 12 7 9 7 11 7 11 7 11 7 8 7 11 7 10 7 8 7 8 7 7 7 9 7 6 7 11 7 8 7 7 7 10 7 13 7 11 7 15 7 18 7 10 7 13 7 15 7 13 7 16 7 12 7 4 7 13 7 11 7 13 7 14 7 11 7 17 7 10 7 5 7 7 7 13 7 8 7 7 7 7 7 10 7 12 7 7 7 8 7 8 7 11 7 10 7 9 7 11 7 11 7 7 7 6 7 8 7 9 7 10 7 11 7 11 7 11 7 8 7 10 7 7 7 8 7 11 7 11 7 13 7 11 7 9 7 12 7 7 7 7 7 8 7 9 7 9 7 9 7 10 7 10 7 7 7 8 7 8 7 9 7 7 7 10 7 11 7 18 7 11 7 8 7 7 7 6 7 6 7 11 7 9 7 9 7 8 7 10 7 9 7 8 7 9 7 11 7 7 7 8 7
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//equation// ieee(2) s=%s; m=s^6+2*s^5+7*s^4+10*s^3+14*s^2+8*s+8 routh=routh_t(m); disp(routh,"routh=") c=0; for i=1:n if (routh(i,1)<0) c=c+1; end end if(c>=1) printf("system is unstable") else ("system is stable") end
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latcfilt12.sce
k=[12 3 4 5 67 8 9]; zi=[1 2 3 4 5 6 7]; [f,g,zf] = latcfilt(k,'ic',zi); disp(f); disp(g); disp(zf); //output //!--error 10000 //wrong input data type //at line 36 of function latcfilt called by : //[f,g,zf] = latcfilt(k,'ic',zi); //matlab //Ladder filter coefficients (V) must be a double precision 2-D //array.
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clear; clc i=100 L=4e-3 C=300e-12 E=i* sqrt(L/C) T=1/ sqrt(L*C) mprintf("e= %.0f *1e3 sin( %.3f *1e6 t) kV",E/1e3,T/1e6)
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//(14.3) Measurements show that at a temperature T and a pressure of 1 atm, the equilibrium mixture for the system of Example 14.2 has the composition yCO = 0.298,yO2 = .149, yCO2 = .553.Determine the temperature T of the mixture, in K. //solution yCO = .298 //solving yCO = 2z/(2 + z) z = 2*yCO/(2 - yCO) p = 1 //in atm pref = 1 //in atm K = (z/(1-z))*(z/(2 + z))^.5*(p/pref)^.5 //with this value of K, table A-27 gives T = 2881 printf('the temperature T of the mixture in kelvin is: %f',T)
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2014-12-22T17:34:50
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fillTE.sci
function[TE] = fillTE(a, t0, T) exec('fillTV.sci', -1); deff('[x] = f(t)', 'x = 3 / 2 * exp(-t) - 1 / 2 * cos(t) + 1 / 2 * sin(t)'); TE = abs(f(T) - fillTV(a, t0, T)); endfunction
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step-batch-7/juice-mildshower
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2022-12-30T19:13:03
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JavaScript
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testInvalidInputForSave02.tst
node beverage.js --save --empId 1234 --qty 3 Please give a valid set of input.
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16Ex3.sce
//chapter 16 Ex 3 clc; clear; close; //let pipes be A and B t12=12; //time taken by A and B to fill tank together AB1hour=1/t12; //part filled by both in 1 hour //Let reservoir be filled by pipe 1 in x hours, thus other in (10+x)hours, thus the equation that is formed is (1/x)+1/(10+x)=1/12; on solving we get mycoeff=[-120 -14 1]; p=poly(mycoeff,"x","coeff"); r=roots(p); v=int32([20 -6]); a=v(1); b=v(2); if a>0 then mprintf("Thus the time taken by both pipes individually are %d hours and %d hours respectively to fill the tank",a,a+10); end
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Ex2_7.sce
//Example 2.7 clc clear function [f,df] = fun7(x) f = x.*exp(x) - 2; df = x.*exp(x) + exp(x); endfunction xold = 1; maxit = 2; iter = 1; while (1) [fx,dfx] = fun7(xold); xnew = xold - fx/dfx; if iter == maxit then break end xold = xnew; iter = iter + 1; end root = round(xnew*10^3) / 10^3; disp(root,"root = ")
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//Problem 33.15: (a) Convert the circuit to the left of terminals AB in Figure 33.72 to an equivalent Th´evenin circuit by initially converting to a Norton equivalent circuit. (b) Determine the magnitude of the current flowing in the (1.8+i4) ohm impedance connected between terminals A and B of Figure 33.72. //initializing the variables: E1 = 12; // in volts E2 = 24; // in volts Z1 = 3; // in ohm Z2 = 2; // in ohm R1 = %i*4; // in ohm R2 = 1.8; // in ohm //calculation: Z3 = R1 + R2 //For the branch containing the E1 source, conversion to a Norton equivalent network gives Isc1 = E1/Z1 //For the branch containing the E2 source, conversion to a Norton equivalent circuit gives Isc2 = E2/Z2 //Thus Figure 33.73 shows a network equivalent to Figure 33.72. From Figure 33.73, the total short-circuit current Isc = Isc1 + Isc2 //the total impedance is given by z = Z1*Z2/(Z1 + Z2) //Thus Figure 33.73 simplifies to Figure 33.74. //The open-circuit voltage across AB of Figure 33.74, E E = Isc*z //the impedance ‘looking in’ at AB,is z //the Th´evenin equivalent circuit is as shown in Figure 33.75. R = 1.8 + %i*4; // in ohm //when R impedance is connected to terminals AB of Figure 33.75, the current I flowing is given by I = E/(z + R) Imag = (real(I)^2 + imag(I)^2)^0.5 printf("\n\n Result \n\n") printf("\n the magnitude of the current flowing (1.8 + i4) ohm resistor is %.2f A", Imag)
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clear ; clc; // Example 19.1 printf('Example 19.1\n\n'); //Page No. 563 // Solution // Use phase rule to get degree of freedom(F) = 2-P+C // (a) N1 = 1; P1 = 1 ;// Number of phases present C1 = 1 ;//Number of components present F1 = 2-P1+C1 ;//Number of degree of freedom printf('\n (a) Number of degree of freedom of pure benzene is %i. Therefore %i additional intensive variables must be specified to fix the system.\n ',F1,F1); // (b) N2 = 1; P2 = 2 ;// Number of phases present C2 = 1 ;//Number of components present F2 = 2-P2+C2 ;//Number of degree of freedom printf('(b) Number of degree of freedom of a mixture of ice and water only is %i. Therefore %i additional intensive variables must be specified to fix the system.\n ',F2,F2); // (c) N3 = 2; P3 = 2 ;// Number of phases present C3 = 2 ;//Number of components present F3 = 2-P3+C3 ;//Number of degree of freedom printf('(c) Number of degree of freedom of a mixture of liquid benzene,benzene vapour and helium gas is %i. Therefore %i additional intensive variables must be specified to fix the system.\n ',F3,F3); // (d) N4 = 2; P4 = 2 ;// Number of phases present C4 = 2 ;//Number of components present F4 = 2-P4+C4 ;//Number of degree of freedom printf('(d) Number of degree of freedom of a mixture of salt and water designed to achieve a specific vapour pressure is %i. Therefore %i additional intensive variables must be specified to fix the system.\n ',F4,F4);
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//chapter 6 Ex 9 clc; clear; close; total=11; avg11=60; avg6first=58; avg6last=63; num6=(((avg6first*6)+(avg6last*6))-avg11*total); mprintf("The 6th number is %d",num6);
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psy007/NNPC-CHEMICAL-SIM-
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gibbsRxn.tst
$thermo = VirtualMaterials.SRK / -> $thermo #Peng-Robinson thermo + METHANE WATER CARBON_MONOXIDE CARBON_DIOXIDE BGS-HYDROGEN units SI # A Equilibrum reactor - isothermal, no pressure drop rxn = EquiliReactor.EquilibriumReactor() cd /rxn In.P = 100 In.T = 1000 K In.MoleFlow = 5 In.Fraction = 0.4 0.6 0 0 0 #In.Fraction = 1.95862592784202e-002 9.93197945149974e-002 0.175637702766885 3.57267224820499e-002 0.669729520957648 Out.P = 100 Out.T = 1000 K 'OutQ = 100000 NumberRxn = 2 Rxn0.Formula = Shift:1*3+1*4-!2-1*1 Rxn1.Formula = reforming:1*2+3*4-1*1-!0 CalculationOption = 2 In Out OutQ copy / paste / cd /RootClone.rxn In Out OutQ
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clc clear //Input data u=1500 //Flight velocity in m/s eff=0.75 //Propulsive efficiency //calculation //Converting relation eff=(2*sig)/(1+sig^2) into 2nd degree polynomial of sig sig=((2-(sqrt(4-(4*eff*eff))))/(2*eff)) //Jet speed ratio Cj=u/sig //Jet velocity in m/s //Output printf('Jet velocity is %3.2f m/s',Cj)
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ColinGilbert/projectzombie
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2021-01-22T02:07:58.275092
2015-04-06T00:57:57
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TOLERANCE = 0.0001 //Setting abitrarily. Mainly we want to avoid C/0.0000001 as this creates a large //number for our C's. In our case, this won't be a case because of the way //we are computing distance transforms based on pixels. That's why we don't set to %eps (machine eps) //ALSO NOTE: We're not worrying too much about floating point details right now as this is //mainly for protyping. Safe to say we have to think hard about this later-on. function y = Pcliff(d,params) scale=-80 if d > TOLERANCE then y = scale/(d**2) else y = scale end endfunction function y = isInRange(d,l,r) if (d >= l) & (d <= r) then y = %t else y = %f end endfunction //This is temorary so we can create a Unit potential map to examine. //Later we probably want to implement this so it gets apply a potential map, //instead of creating two potential maps. function y = Popp(d,params) if isInRange(d,0,params.D-2) y = params.P(1)(d,params.D) elseif isInRange(d,params.D-2,params.D) y = params.P(2)(d,params.D) elseif isInRange(d,params.D-2,params.R) y = params.P(3)(d,params.D) else y = 0 end y = y * params.WEIGHT endfunction function Y = GetPotentialMap(X, P, params) Y = [] for c=X, v = [] for e=c' //column turns into row vector to do for each element in column. v = [v; P(e,params)] //append each P(e) into rows. In the end producing a N column vector. end Y = [Y,v] //append the column vector. In the end producing a MxN transformed output matrix. end endfunction function Y = GetDistanceMapObstacles(fileName) RGB = ReadImage('data\testcitymap_new.png') Image = RGB2Gray(RGB) EdgeImage = ~SegmentByThreshold(Image, 1) Y = double(DistanceTransform(EdgeImage)) endfunction function Y=GetEdgeImageUnits(Units, Image, UnitDesc) if ~exists("UnitDesc","l") UnitDesc = [1,1] //A 1 x 1 sized Unit end for c=Units, for i=0:UnitDesc(1)-1 //number of rows for j=0:UnitDesc(2)-1 //number of cols Image(c(1,:)+i, c(2,:)+j) = uint8(1) end end end Y = ~SegmentByThreshold(Image, 1) endfunction //This function will get the distance map for a given set of units with position vectors as a //2xN matric. Where each column vector is the position of the unit. function Z = GetDistanceMapUnits(X,Image) for c=X, Image(c(1,:),c(2,:)) = uint8(1) end EdgeImage = ~SegmentByThreshold(Image, 1) Z = double(DistanceTransform(EdgeImage)) endfunction //Utility function to save the edge image for units out. function Z = WriteEdgeImageUnit(X,Image) for c=X, for i=0:10, for j=0:10 Image(c(1,:)+i,c(2,:)+j) = uint8(1) end end end EdgeImage = ~SegmentByThreshold(Image, 1) WriteImage(uint8(EdgeImage), 'data\EdgeImageBase.png') Z=[] endfunction function Y = GetParamsTList() Y = tlist(["PARAM_LIST","D","R","P","WEIGHT"],[],[],[],[0.1429]) endfunction //This function will get a vector of potential functions of OPP Units. function Y = OPPUPotential() function i = OPPUP1(d,D) scale = 240.0 if d < TOLERANCE i = 80 else i = scale/(d*(D-2)) end endfunction function j = OPPUP2(d,D) scale = 240.0 if d < TOLERANCE j = 80 else j = scale end endfunction function k = OPPUP3(d,D) scale = 240.0 scale2 = 0.24 if d < TOLERANCE k = 80 else k = scale-scale2*(d-D) end endfunction Y = list(OPPUP1,OPPUP2,OPPUP3) endfunction //This function will get a vector of potential functions of OPP Base. function Y = OPPBPotential() function i = OPPBP1(d,D) scale = 360.0 if d < TOLERANCE i = 0 else i = scale/((D-2)*d) end endfunction function j = OPPBP2(d,D) scale = 360.0 if d < TOLERANCE j = 0 else j = scale end endfunction function k = OPPBP3(d,D) scale = 360.0 if d < TOLERANCE k = 0 else k = scale - (d - D)*0.32 end endfunction Y = list(OPPBP1,OPPBP2,OPPBP3) endfunction function Y = GetBiasedScaledPMap(X,bias) [nr,nc] = size(X) for i=1:nr, for j=1:nc, t = X(i,j) if t > 0.0 X(i,j) = X(i,j) * bias end end end Y = [] endfunction OPPU_Tank = GetParamsTList() OPPU_Tank.D = 7 OPPU_Tank.R = 68 OPPU_Tank.P = OPPUPotential() OPPU_Base = GetParamsTList() OPPU_Base.D = 12 OPPU_Base.R = 1000 OPPU_Base.P = OPPBPotential() BasePos = [61 39 250 131] WORKING_PATH="E:/Users/gnulinux/projects/prjz/scilab/potential_path/" function Y = ComputeEdgeImages() path = pwd() disp("Path is: " + path) BaseEdgeImg = uint8(zeros(512,512)) ObsEdgeImg = uint8(zeros(512,512)) RGB = ReadImage(WORKING_PATH+'data/testcitymap_new.png') Image = RGB2Gray(RGB) ObsEdgeImg = ~SegmentByThreshold(Image, 1) BaseEdgeImg = GetEdgeImageUnits(BasePos,BaseEdgeImg,[10,10]) Y = tlist(["EdgeImages","BaseEdgeImg","ObsEdgeImg"],[BaseEdgeImg],[ObsEdgeImg]) endfunction function WriteEdgeImagesAsPng(EdgeImages) nc = size(EdgeImages) for i=2:nc, WriteImage(uint8(EdgeImages(i)), WORKING_PATH+'data/'+EdgeImages(1)(i)+'.png') end endfunction function Y = GetDistanceMaps() DMapBase = read(WORKING_PATH+'data/BaseEdgeImg.mtd',-1,512) DMapObs = read(WORKING_PATH+'data/ObsEdgeImg.mtd',-1,512) Y = tlist(["DistanceMapsList","DMapBase","DMapObs"],[DMapBase],[DMapObs]) endfunction function Y = GetPotentialMaps(DMaps) PMapObs = GetPotentialMap(DMaps.DMapObs, Pcliff, 0) PMapBase = GetPotentialMap(DMaps.DMapBase, Popp, OPPU_Base) PMapCombined = PMapObs + PMapBase Y = tlist(["PMapsList","PMapObs","PMapBase","PMapCombined"],[PMapObs],[PMapBase],[PMapCombined]) endfunction function Y = GetResults() BaseImage = uint8(zeros(512,512)) DistanceMapObs = GetDistanceMapObstacles() DistanceMapBase = GetDistanceMapUnits(BasePos,BaseImage) WriteEdgeImageUnit(BasePos,BaseImage) clear('BaseImage') PMapObs = GetPotentialMap(DistanceMapObs, Pcliff, 0) PMapBase = GetPotentialMap(DistanceMapBase, Popp, OPPU_Base) PMapCombined = PMapObs + PMapBase Y = tlist(["PMapNavResults","PMapObs","PMapBase","PMapCombined","DistanceMapObs","DistanceMapBase"],[PMapObs],[PMapBase],[PMapCombined],[DistanceMapObs], [DistanceMapBase]) endfunction function Y = GetBaseImage() Y = uint8(zeros(512,512)) endfunction
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Total index levels = 1 Total number of nodes = 9 Total number of items = 24 Dumping level #0 [Node 2] flags = 0, dge_link = 4 lft_link = -1, rgt_link = -1 Item #0, data = b, link = 0 Item #1, data = c, link = 3 Item #2, data = d, link = 1 Dumping level #1 [Node 0] flags = 5, dge_link = 5 lft_link = -1, rgt_link = 5 Item #0, data = a, link = -1 Item #1, data = a, link = -1 Item #2, data = a, link = -1 Item #3, data = a, link = -1 Item #4, data = a, link = -1 [Node 5] flags = 1, dge_link = 0 lft_link = 0, rgt_link = 3 Item #0, data = a, link = -1 [Node 3] flags = 5, dge_link = 6 lft_link = 5, rgt_link = 6 Item #0, data = b, link = -1 Item #1, data = b, link = -1 Item #2, data = b, link = -1 Item #3, data = b, link = -1 Item #4, data = b, link = -1 [Node 6] flags = 1, dge_link = 3 lft_link = 3, rgt_link = 1 Item #0, data = b, link = -1 [Node 1] flags = 5, dge_link = 7 lft_link = 6, rgt_link = 7 Item #0, data = c, link = -1 Item #1, data = c, link = -1 Item #2, data = c, link = -1 Item #3, data = c, link = -1 Item #4, data = c, link = -1 [Node 7] flags = 1, dge_link = 1 lft_link = 1, rgt_link = 4 Item #0, data = c, link = -1 [Node 4] flags = 7, dge_link = 8 lft_link = 7, rgt_link = 8 Item #0, data = d, link = -1 Item #1, data = d, link = -1 Item #2, data = d, link = -1 Item #3, data = d, link = -1 Item #4, data = d, link = -1 [Node 8] flags = 1, dge_link = 4 lft_link = 4, rgt_link = -1 Item #0, data = d, link = -1
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//resistance per square //given clc l=30d-3//metre t=0.1d-6//metre Rp=0.3//ohm delta_s=4.1d+7//mho/m w=l/(Rp*t*delta_s)//metre w=round(w*1000)/1000///rounding off decimals disp(t*1d+6, w*1000,l*1d+3 ,'the design parameter of planer resistor are in mm and um')//millimetre
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Engineering Thermodynamics by Onkar Singh,Chapter 2,Example 5") disp("let the conversion relation be X=aC+b") disp("where C is temperature in degree celcius,a&b are constants and X is temperature in X degree ") disp("at freezing point,temperature=0 degree celcius,0 degree X") disp("so by equation X=aC+b") X=0;//temperature in degree X C=0;//temperature in degree celcius disp("we get b=0") b=0; disp("at boiling point,temperature=100 degree celcius,1000 degree X") X=1000;//temperature in degree X C=100;//temperature in degree celcius a=(X-b)/C disp("conversion relation") disp("X=10*C") disp("absolute zero temperature in degree celcius=-273.15") disp("absolute zero temperature in degree X=") 10*-273.15
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<?xml version="1.0" encoding="utf-8"?> <test> <description>Euler Isentropic Vortex P=3 GAUSS</description> <executable>CompressibleFlowSolver</executable> <parameters>IsentropicVortex16_P3_GAUSS.xml</parameters> <files> <file description="Session File">IsentropicVortex16_P3_GAUSS.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="rho" tolerance="1e-12">0.00474302</value> <value variable="rhou" tolerance="1e-12">0.00947318</value> <value variable="rhov" tolerance="1e-12">0.00869843</value> <value variable="E" tolerance="1e-12">0.0254323</value> </metric> <metric type="Linf" id="2"> <value variable="rho" tolerance="1e-12">0.00539172</value> <value variable="rhou" tolerance="1e-12">0.0113971</value> <value variable="rhov" tolerance="1e-12">0.0117187</value> <value variable="E" tolerance="1e-12">0.0374887</value> </metric> </metrics> </test>
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exec('testplot3d.sce',-1) //to delete F=gcf(); // le handle de la figure // les 3 surfacesde type Fac3d F.children(2:4).children // le titre de chaque tracé F.children(2:4).title.text // couleurs de l'affichage F.children(2:4).children.color_flag F.children(2:4).children.color_mode F.children(2:4).children.hiddencolor
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//Chapter 17, Example 17.2 clc //Initialisation C=10**-6 //capacitance in farad RG=10**6 //resistance in ohm pi=3.14 //pi //Calculation fc=1/(2*pi*C*RG) //frequency in Hz //Results printf("Fc = %.2f Hz",fc )
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RGB=imread('C:\Users\Mohammed Kesury\Desktop\Sem 6\DIP\peppers_color.tif') figure imshow(RGB) figure R=RGB(:,:,1) imhist(R,20,'red') figure G=RGB(:,:,2) imhist(G,20,'green') figure B=RGB(:,:,3) imhist(B,20,'blue')
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clc; clear; function z=f(x,y) z=2*x*y + 2*x - x^2 - 2*y^2 endfunction x=-1; y=1; dfx=2*y+2-2*x; dfy=2*x-4*y; //the function can thus be expressed along h axis as //f((x+dfx*h),(y+dfy*h)) disp("180*h^2 + 72*h - 7","The final equation is=")
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clear; clc; printf("\t\t\tProblem Number 3.1\n\n\n"); // Chapter 3 : The First Law Of Thermodynamics // Problem 3.1 (page no. 91) // Solution //For a constant volume process, 10 Btu/lbm heat is added to the system //We can consider thet a tank having a fixed volume has heat added to it //Under these conditions,the mechanical work done on or by the system must be 0 //u2-u1=q printf("Heat has been converted to internal energy of the working fluid\n"); //So, printf(" So,Change in internal energy u2-u1=10 Btu/Lbm");
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ifeq ($(OS),Windows_NT) ifeq ($(shell uname -s),) # not in a bash-like shell CLEANUP = del /F /Q MKDIR = mkdir else # in a bash-like shell, like msys CLEANUP = rm -f MKDIR = mkdir -p endif TARGET_EXTENSION=.exe else CLEANUP = rm -f MKDIR = mkdir -p TARGET_EXTENSION=out endif .PHONY: cleantest .PHONY: test PATHU = tools/Unity/src/ PATHS = ./ PATHT = test/ PATHB = build/ PATHD = build/depends/ PATHO = build/objs/ PATHR = build/results/ BUILD_PATHS = $(PATHB) $(PATHD) $(PATHO) $(PATHR) TSTSRC = $(wildcard $(PATHT)*.c) COMPILE=gcc -c LINK=gcc DEPEND=gcc -MM -MG -MF TCFLAGS =-Iinclude -I$(PATHU) -I$(PATHS) -DTEST $(DEFS) RESULTS = $(patsubst $(PATHT)Test%.c,$(PATHR)Test%.txt,$(TSTSRC) ) ORGSRC = $(patsubst $(PATHT)Test%.c,%.c,$(TSTSRC)) ALLSRC = $(foreach w,$(ORGSRC),$(shell find . -name $(w))) ALLOBJ = $(foreach s,$(ALLSRC),$(PATHO)$(notdir $(s:.c=.o))) PASSED = `grep -s PASS $(PATHR)*.txt` FAIL = `grep -s FAIL $(PATHR)*.txt` IGNORE = `grep -s IGNORE $(PATHR)*.txt` define create_rule = $(eval test_o := $(PATHO)$(notdir $(1:.c=.o))) $(test_o) : $(1) $(Q)$(COMPILE) $(TCFLAGS) $(1) -o $(test_o) endef test: $(BUILD_PATHS) $(RESULTS) @echo "\n TEST IGNORES:" @echo "$(IGNORE)" @echo " TEST FAILURES:" @echo "$(FAIL)" @echo " TEST PASSED:" @echo "$(PASSED)" $(PATHR)%.txt: $(PATHB)%.$(TARGET_EXTENSION) @echo " TESTING " $@ $< @-./$< > $@ 2>&1 $(PATHB)Test%.$(TARGET_EXTENSION): $(PATHO)Test%.o $(PATHO)%.o $(PATHO)unity.o #$(PATHD)Test%.d $(Q)$(LINK) -o $@ $^ $(PATHO)%.o:: $(PATHT)%.c $(Q)$(COMPILE) $(TCFLAGS) $< -o $@ $(PATHO)%.o:: $(PATHS)%.c $(Q)$(COMPILE) $(TCFLAGS) $< -o $@ $(PATHO)%.o:: $(PATHU)%.c $(PATHU)%.h $(Q)$(COMPILE) $(TCFLAGS) $< -o $@ $(PATHD)%.d:: $(PATHT)%.c $(DEPEND) $@ $< $(PATHB): $(Q)$(MKDIR) $(PATHB) $(PATHD): $(Q)$(MKDIR) $(PATHD) $(PATHO): $(Q)$(MKDIR) $(PATHO) $(PATHR): $(Q)$(MKDIR) $(PATHR) $(foreach test_s,$(ALLSRC),$(eval $(call create_rule,$(test_s)))) cleantest: $(CLEANUP) $(PATHO)*.o $(CLEANUP) $(PATHB)*.$(TARGET_EXTENSION) $(CLEANUP) $(PATHR)*.txt .PRECIOUS: $(PATHB)Test%.$(TARGET_EXTENSION) .PRECIOUS: $(PATHD)%.d .PRECIOUS: $(PATHO)%.o .PRECIOUS: $(PATHR)%.txt
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int main(void) { int p, q; &p * &q; }
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Ex6_6.sce
clc //given that P_m = 2.3e-14 // permissibility coefficient of CO2 through PET P_1 = 400// Pressure inside bottle in KPa P_2 = 0.4 // Pressure outside bottle in KPa A = 500 // Surface area of bottle in cm^2 x = 0.05 // wall thickness of bottle in cm V = 750 // volume in cm^3 printf("\Example 6.6\n") J = -P_m*(P_2-P_1)*1e3/x // calculation of diffusion flux printf("\n Part A:") printf("\n Diffusion flux is %0.1e cm^3 STP/(cm^2-s)",J) printf("\n\n Part B:") V_co2 = J*A t = V/V_co2 // calculation of self life printf("\n Self life for bottle of pop is %d days (or about %d months).", t/(60*60*24),t/(60*60*24*30)) // Answer in book is 97 days. It is because of considering different number of significant figure
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clc // H_L=1.2*v^2/2/g // H_L=4*f*L_eq/d*V^2/2/g // L_eq=60*d // H_L=240*f*v^2/2/g // Combining the two equations for head loss // 1.2*v^2/2/g=240*f*v^2/2/g f=1.2/240; disp("Friction factor =") disp(f)
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ex1_23_9.sce
//Exa 1.23.9 clc; clear; close; // Given data N_V = 1.04 * 10^19;// in cm^-3 T1 = 300;// in K T2 = 400;// in K del_E = 0.27;// in eV N_V = N_V * (T2/T1)^1.5;// in cm^-3 KT = (0.0259) * (T2/T1);// in eV P_o = N_V * exp(-(del_E)/KT);// in cm^-3 disp(P_o,"The thermal equilibrium hole concentration in silicon in cm^-3 is ");