P6DofRocketSolidPropellantObject Class Reference

#include <P6DofRocketSolidPropellantObject.hpp>

Inheritance diagram for P6DofRocketSolidPropellantObject:

Collaboration diagram for P6DofRocketSolidPropellantObject:

Public Member Functions
	P6DofRocketSolidPropellantObject (P6DofScenario *aScenario)
	~P6DofRocketSolidPropellantObject () override
P6DofRocketSolidPropellantObject &	operator= (const P6DofRocketSolidPropellantObject &other)=delete
std::string	GetClassType () override
bool	ProcessInput (UtInput &aInput) override
bool	Initialize (int64_t aSimTime_nanosec) override
P6DofRocketSolidPropellantObject *	Clone () const
void	DeriveFrom (const P6DofRocketSolidPropellantObject *aSrc)
void	SetControlInputHandles (const P6DofFlightControlSystem *aFlightControls) override
void	SetControlInputValues (const P6DofFlightControlSystem *aFlightControls) override
void	IgniteNow ()
void	CalculateThrust (double aDeltaT_sec, double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad, P6DofForceAndMomentsObject &aForceAndMoment, double &aFuelBurnRate_pps, double &aFuelBurned_lbs) override
void	UpdateThrust (double aDeltaT_sec, double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad, P6DofForceAndMomentsObject &aForceAndMoment, double &aFuelBurnRate_pps, double &aFuelBurned_lbs) override
double	GetPercentMaxThrust () const
double	GetCurrentPropellant_lbs () const
double	GetFuelBurnRate_pph () const override
double	GetMaxPropellant_lbs () const
double	GetMaximumPotentialThrust_lbs (double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad) override
double	GetMinimumPotentialThrust_lbs (double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad) override
void	CalculateCurrentMassProperties () override
void	SetThrottlePosition (double aThrottleLeverPosition) override
double	GetThrottlePosition () const override
void	Ignite (int64_t aIgniteTimeInFrame_nanosec) override
void	Shutdown (int64_t aTerminateTime_nanosec=0) override
Public Member Functions inherited from P6DofThrustProducerObject
	P6DofThrustProducerObject (P6DofScenario *aScenario)
	~P6DofThrustProducerObject () override
P6DofThrustProducerObject &	operator= (const P6DofThrustProducerObject &other)=delete
void	SetParentPropulsionSystem (P6DofPropulsionSystem *aParent)
double	GetThrust_lbs () const
double	GetForwardThrust_lbs () const
void	SetThrustReferenceOffsetAttitude (const UtVec3dX &aReferenceLocation_ft, UtVec3dX &aThrustYPR_rad)
void	SetThrustVectoringEnabled (bool aThrustVectoringEnabled)
bool	ThrustVectoringEnabled () const
void	SetThrustVectoringYaw_deg (double aThrustVectoringYaw_deg)
void	SetThrustVectoringPitch_deg (double aThrustVectoringPitch_deg)
double	GetThrustVectoringYaw_deg () const
double	GetThrustVectoringPitch_deg () const
void	SetThrustReverserEnabled (bool aThrustReverserEnabled)
bool	ThrustReverserEnabled () const
void	SetThrustReverserSetting (double aThrustReverserSetting)
double	GetThrustReverserSetting () const
void	GetThrustLocation (UtVec3dX &aThrustLocation_ft) const
void	GetThrustInstalledAnglesYPR (UtVec3dX &aThrustYPR_rad) const
void	GetCurrentThrustVectorDirection (UtVec3dX &aDirection) const
void	CalcCurrentThrustVectors ()
const P6DofForceAndMomentsObject &	GetThrustForceAndAndMoment () const
P6DofMassProperties *	GetMassProperties () const
virtual bool	AfterburnerIsPresent () const
bool	EngineOperating () const
virtual bool	MayHaveEngineOperating () const
bool	EngineSmoking () const
virtual bool	MayProduceEngineSmoke () const
bool	AfterburnerOn () const
bool	Contrailing () const
virtual bool	MayContrail () const
bool	ProducingSmokeTrail () const
void	MakeEngineSmoke (bool aSmoking)
Public Member Functions inherited from P6DofObject
	P6DofObject (P6DofScenario *aScenario)
virtual	~P6DofObject ()=default
P6DofObject *	Clone () const
P6DofScenario *	GetScenario () const
std::string	GetName () const
void	SetName (const std::string &aName)
P6DofVehicle *	GetParentVehicle () const
virtual void	SetParentVehicle (P6DofVehicle *aParentVehicle)

Protected Member Functions
	P6DofRocketSolidPropellantObject (const P6DofRocketSolidPropellantObject &aSrc)
void	CalculateThrust (double aDeltaT_sec, double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad, P6DofForceAndMomentsObject &aForceAndMoment, double &aFuelBurnRate_pps, double &aFuelBurned_lbs, bool aUpdateData)
double	Thrust_lbs (double aBurnTime_Sec, double aAlt_ft, double &aMassFlow_pps)
bool	MayProduceSmokeTrail () const override
Protected Member Functions inherited from P6DofThrustProducerObject
	P6DofThrustProducerObject (const P6DofThrustProducerObject &aSrc)
void	DeriveFrom (const P6DofThrustProducerObject *aSrc)
void	SetMassProperties (P6DofMassProperties *aMassProperties)
UtVec3dX	CalcThrustVectorFromThrust (double aThrust_lbs)
void	CalcThrustProducerFM (double aThrustMagnitude_lbs, P6DofForceAndMomentsObject &aForceAndMoment)
Protected Member Functions inherited from P6DofObject
	P6DofObject (const P6DofObject &aSrc)=default
P6DofObject &	operator= (const P6DofObject &other)=default

Protected Attributes
UtCloneablePtr< UtTable::Curve >	mThrustSeaLevelVersusTime
UtCloneablePtr< UtTable::Curve >	mThrustVacuumVersusTime
UtCloneablePtr< UtTable::Curve >	mIspAlt
double	mIspSeaLevel
double	mIspVacuum
double	mRatedThrust_lbs
double	mLastThrust_lbs
double	mPropellantMass_lbs
double	mMaxPropellantMass_lbs
bool	mIsBurning
double	mBurnTime_sec
double	mCurrentFuelBurnRate_pph
UtVec3dX	mPropellantCmLocation_ft
ThrustControlInputValueData *	mThrottleSettingYaw
ThrustControlInputValueData *	mThrottleSettingPitch
bool	mGenerateSmokeTrail
Protected Attributes inherited from P6DofThrustProducerObject
P6DofPropulsionSystem *	mParentPropulsionSystemPtr
std::string	mTypeOfThrustProducer
UtVec3dX	mNominalThrustVectorDirection
UtVec3dX	mCurrentThrustVectorDirection
UtVec3dX	mReferenceLocation_ft
UtVec3dX	mThrustLocation_ft
P6DofForceAndMomentsObject	mCurrentThrustFM_lbs_ftlbs
UtVec3dX	mThrustInstalledAnglesYPR_rad
double	mThrustOffset_ft
bool	mThrustVectoringEnabled
double	mThrustVectorYaw_rad
double	mThrustVectorPitch_rad
bool	mThrustReverserEnabled
double	mThrustReverserSetting
bool	mShutdownInProgress
int64_t	mShutdownFraction_nanosec
int64_t	mIgniteTimeInFrame_nanosec
bool	mInOpRefAreaValid
double	mInOpRefArea_ft2
P6DofMassProperties *	mMassPropertiesPtr
double	mCurrentThrustFactor
bool	mAfterburnerPresent
bool	mEngineOperating
bool	mEngineSmoking
bool	mAfterburnerOn
bool	mContrailing
bool	mProducingSmokeTrail
bool	mEngineDamageSmokeActivated
Protected Attributes inherited from P6DofObject
P6DofScenario *	mScenario
P6DofVehicle *	mParentVehicle
std::string	mObjName

Additional Inherited Members
Static Public Member Functions inherited from P6DofThrustProducerObject
static void	SetControlInputHandle (const P6DofFlightControlSystem *aFlightControls, ThrustControlInputValueData *aControlInput)
static void	SetControlInputValue (const P6DofFlightControlSystem *aFlightControls, ThrustControlInputValueData *aControlInput)

Constructor & Destructor Documentation

P6DofRocketSolidPropellantObject() [1/2]

P6DofRocketSolidPropellantObject::P6DofRocketSolidPropellantObject ( P6DofScenario * aScenario )

explicit

References mBurnTime_sec, mCurrentFuelBurnRate_pph, mGenerateSmokeTrail, mIsBurning, mIspAlt, mIspSeaLevel, mIspVacuum, mLastThrust_lbs, mMaxPropellantMass_lbs, mPropellantCmLocation_ft, mPropellantMass_lbs, mRatedThrust_lbs, mThrottleSettingPitch, mThrottleSettingYaw, mThrustSeaLevelVersusTime, mThrustVacuumVersusTime, P6DofThrustProducerObject::mTypeOfThrustProducer, P6DofThrustProducerObject::P6DofThrustProducerObject(), and P6DofThrustProducerObject::SetMassProperties().

Referenced by Clone(), DeriveFrom(), operator=(), P6DofRocketSolidPropellantObject(), and ProcessInput().

~P6DofRocketSolidPropellantObject()

P6DofRocketSolidPropellantObject::~P6DofRocketSolidPropellantObject ( )

override

References mThrottleSettingPitch, and mThrottleSettingYaw.

P6DofRocketSolidPropellantObject() [2/2]

P6DofRocketSolidPropellantObject::P6DofRocketSolidPropellantObject ( const P6DofRocketSolidPropellantObject & aSrc )

protected

References if(), mBurnTime_sec, mCurrentFuelBurnRate_pph, mGenerateSmokeTrail, mIsBurning, mIspAlt, mIspSeaLevel, mIspVacuum, mLastThrust_lbs, mMaxPropellantMass_lbs, mPropellantCmLocation_ft, mPropellantMass_lbs, mRatedThrust_lbs, mThrottleSettingPitch, mThrottleSettingYaw, mThrustSeaLevelVersusTime, mThrustVacuumVersusTime, P6DofRocketSolidPropellantObject(), and P6DofThrustProducerObject::P6DofThrustProducerObject().

Member Function Documentation

CalculateCurrentMassProperties()

void P6DofRocketSolidPropellantObject::CalculateCurrentMassProperties ( )

overridevirtual

Implements P6DofThrustProducerObject.

References P6DofThrustProducerObject::mMassPropertiesPtr, mPropellantCmLocation_ft, and mPropellantMass_lbs.

Referenced by DeriveFrom(), and Initialize().

CalculateThrust() [1/2]

void P6DofRocketSolidPropellantObject::CalculateThrust ( double aDeltaT_sec, double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad, P6DofForceAndMomentsObject & aForceAndMoment, double & aFuelBurnRate_pps, double & aFuelBurned_lbs )

overridevirtual

Implements P6DofThrustProducerObject.

References CalculateThrust().

Referenced by CalculateThrust(), GetMaximumPotentialThrust_lbs(), and UpdateThrust().

CalculateThrust() [2/2]

void P6DofRocketSolidPropellantObject::CalculateThrust ( double aDeltaT_sec, double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad, P6DofForceAndMomentsObject & aForceAndMoment, double & aFuelBurnRate_pps, double & aFuelBurned_lbs, bool aUpdateData )

protected

References P6DofForceAndMomentsObject::AddForceAndMomentAtReferencePoint(), P6DofThrustProducerObject::CalcThrustProducerFM(), P6DofThrustProducerObject::CalcThrustVectorFromThrust(), P6DofUtils::cEPSILON_SIMTIME_SEC, P6DofForceAndMomentsObject::ClearForcesAndMoments(), P6DofObject::GetParentVehicle(), P6DofObject::GetScenario(), P6DofUtils::LimitThrottleNormalized(), P6DofThrustProducerObject::mAfterburnerOn, mBurnTime_sec, P6DofThrustProducerObject::mContrailing, mCurrentFuelBurnRate_pph, P6DofThrustProducerObject::mCurrentThrustFM_lbs_ftlbs, P6DofThrustProducerObject::mEngineDamageSmokeActivated, P6DofThrustProducerObject::mEngineOperating, P6DofThrustProducerObject::mEngineSmoking, mGenerateSmokeTrail, P6DofThrustProducerObject::mIgniteTimeInFrame_nanosec, mIsBurning, mLastThrust_lbs, P6DofForceAndMomentsObject::MoveRefPoint_ft(), P6DofThrustProducerObject::mProducingSmokeTrail, mPropellantMass_lbs, P6DofThrustProducerObject::mShutdownFraction_nanosec, P6DofThrustProducerObject::mShutdownInProgress, P6DofThrustProducerObject::mThrustLocation_ft, Thrust_lbs(), P6DofUtils::TimeToTime(), and P6DofVehicle::WithinContrailAltitudeBand().

Clone()

P6DofRocketSolidPropellantObject * P6DofRocketSolidPropellantObject::Clone

(

)

const

References P6DofRocketSolidPropellantObject().

DeriveFrom()

void P6DofRocketSolidPropellantObject::DeriveFrom

(

const P6DofRocketSolidPropellantObject *

aSrc

)

References CalculateCurrentMassProperties(), P6DofThrustProducerObject::DeriveFrom(), mBurnTime_sec, mCurrentFuelBurnRate_pph, mGenerateSmokeTrail, mIsBurning, mIspAlt, mIspSeaLevel, mIspVacuum, mLastThrust_lbs, mMaxPropellantMass_lbs, mPropellantCmLocation_ft, mPropellantMass_lbs, mRatedThrust_lbs, mThrottleSettingPitch, mThrottleSettingYaw, mThrustSeaLevelVersusTime, mThrustVacuumVersusTime, and P6DofRocketSolidPropellantObject().

Referenced by P6DofPropulsionSystem::Initialize(), and ProcessInput().

GetClassType()

std::string P6DofRocketSolidPropellantObject::GetClassType ( )

inlineoverridevirtual

Implements P6DofThrustProducerObject.

GetCurrentPropellant_lbs()

double P6DofRocketSolidPropellantObject::GetCurrentPropellant_lbs

(

)

const

References mPropellantMass_lbs.

Referenced by P6DofVehicle::CalcTotalFuelFlowAndQuantity().

GetFuelBurnRate_pph()

double P6DofRocketSolidPropellantObject::GetFuelBurnRate_pph ( ) const

overridevirtual

Implements P6DofThrustProducerObject.

References mCurrentFuelBurnRate_pph.

GetMaximumPotentialThrust_lbs()

double P6DofRocketSolidPropellantObject::GetMaximumPotentialThrust_lbs ( double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad )

overridevirtual

Implements P6DofThrustProducerObject.

References CalculateThrust(), and P6DofForceAndMomentsObject::GetForceMagnitude_lbs().

GetMaxPropellant_lbs()

double P6DofRocketSolidPropellantObject::GetMaxPropellant_lbs

(

)

const

References mMaxPropellantMass_lbs.

Referenced by P6DofVehicle::CalcTotalFuelFlowAndQuantity().

GetMinimumPotentialThrust_lbs()

double P6DofRocketSolidPropellantObject::GetMinimumPotentialThrust_lbs ( double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad )

overridevirtual

Implements P6DofThrustProducerObject.

GetPercentMaxThrust()

double P6DofRocketSolidPropellantObject::GetPercentMaxThrust

(

)

const

References mLastThrust_lbs, and mRatedThrust_lbs.

GetThrottlePosition()

double P6DofRocketSolidPropellantObject::GetThrottlePosition ( ) const

overridevirtual

Implements P6DofThrustProducerObject.

References mIsBurning.

Ignite()

void P6DofRocketSolidPropellantObject::Ignite ( int64_t aIgniteTimeInFrame_nanosec )

overridevirtual

Implements P6DofThrustProducerObject.

References P6DofThrustProducerObject::mIgniteTimeInFrame_nanosec, and mIsBurning.

IgniteNow()

void P6DofRocketSolidPropellantObject::IgniteNow ( )

inline

References mIsBurning.

Referenced by SetThrottlePosition().

Initialize()

bool P6DofRocketSolidPropellantObject::Initialize ( int64_t aSimTime_nanosec )

overridevirtual

Implements P6DofThrustProducerObject.

References CalculateCurrentMassProperties(), mIspAlt, mIspSeaLevel, and mIspVacuum.

MayProduceSmokeTrail()

bool P6DofRocketSolidPropellantObject::MayProduceSmokeTrail ( ) const

inlineoverrideprotectedvirtual

Reimplemented from P6DofThrustProducerObject.

References mGenerateSmokeTrail.

operator=()

P6DofRocketSolidPropellantObject & P6DofRocketSolidPropellantObject::operator= ( const P6DofRocketSolidPropellantObject & other )

delete

References P6DofRocketSolidPropellantObject().

ProcessInput()

bool P6DofRocketSolidPropellantObject::ProcessInput ( UtInput & aInput )

overridevirtual

Implements P6DofThrustProducerObject.

References DeriveFrom(), P6DofObject::GetScenario(), mGenerateSmokeTrail, P6DofThrustProducerObject::mInOpRefArea_ft2, P6DofThrustProducerObject::mInOpRefAreaValid, mIspAlt, mMaxPropellantMass_lbs, mPropellantCmLocation_ft, mPropellantMass_lbs, mRatedThrust_lbs, mThrottleSettingPitch, mThrottleSettingYaw, P6DofThrustProducerObject::mThrustOffset_ft, mThrustSeaLevelVersusTime, mThrustVacuumVersusTime, P6DofThrustProducerObject::mThrustVectoringEnabled, P6DofRocketSolidPropellantObject(), and P6DofObject::SetName().

Referenced by P6DofTypeManager::ProcessInput().

SetControlInputHandles()

void P6DofRocketSolidPropellantObject::SetControlInputHandles ( const P6DofFlightControlSystem * aFlightControls )

overridevirtual

Implements P6DofThrustProducerObject.

References mThrottleSettingPitch, mThrottleSettingYaw, and P6DofThrustProducerObject::SetControlInputHandle().

SetControlInputValues()

void P6DofRocketSolidPropellantObject::SetControlInputValues ( const P6DofFlightControlSystem * aFlightControls )

overridevirtual

Implements P6DofThrustProducerObject.

References mThrottleSettingPitch, mThrottleSettingYaw, and P6DofThrustProducerObject::SetControlInputValue().

SetThrottlePosition()

void P6DofRocketSolidPropellantObject::SetThrottlePosition ( double aThrottleLeverPosition )

overridevirtual

Implements P6DofThrustProducerObject.

References IgniteNow(), and P6DofUtils::LimitThrottleNormalized().

Shutdown()

void P6DofRocketSolidPropellantObject::Shutdown ( int64_t aTerminateTime_nanosec = 0 )

overridevirtual

Implements P6DofThrustProducerObject.

References mIsBurning, P6DofThrustProducerObject::mShutdownFraction_nanosec, and P6DofThrustProducerObject::mShutdownInProgress.

Thrust_lbs()

double P6DofRocketSolidPropellantObject::Thrust_lbs ( double aBurnTime_Sec, double aAlt_ft, double & aMassFlow_pps )

protected

References mIspAlt, mIspSeaLevel, mIspVacuum, mThrustSeaLevelVersusTime, and mThrustVacuumVersusTime.

Referenced by CalculateThrust().

UpdateThrust()

void P6DofRocketSolidPropellantObject::UpdateThrust ( double aDeltaT_sec, double aAlt_ft, double aDynPress_lbsqft, double aStatPress_lbssqft, double aSpeed_fps, double aMach, double aAlpha_rad, double aBeta_rad, P6DofForceAndMomentsObject & aForceAndMoment, double & aFuelBurnRate_pps, double & aFuelBurned_lbs )

overridevirtual

Implements P6DofThrustProducerObject.

References CalculateThrust().

Member Data Documentation

mBurnTime_sec

double P6DofRocketSolidPropellantObject::mBurnTime_sec

protected

Referenced by CalculateThrust(), DeriveFrom(), P6DofRocketSolidPropellantObject(), and P6DofRocketSolidPropellantObject().

mCurrentFuelBurnRate_pph

double P6DofRocketSolidPropellantObject::mCurrentFuelBurnRate_pph

protected

Referenced by CalculateThrust(), DeriveFrom(), GetFuelBurnRate_pph(), P6DofRocketSolidPropellantObject(), and P6DofRocketSolidPropellantObject().

mGenerateSmokeTrail

bool P6DofRocketSolidPropellantObject::mGenerateSmokeTrail

protected

Referenced by CalculateThrust(), DeriveFrom(), MayProduceSmokeTrail(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), and ProcessInput().

mIsBurning

bool P6DofRocketSolidPropellantObject::mIsBurning

protected

Referenced by CalculateThrust(), DeriveFrom(), GetThrottlePosition(), Ignite(), IgniteNow(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), and Shutdown().

mIspAlt

UtCloneablePtr<UtTable::Curve> P6DofRocketSolidPropellantObject::mIspAlt

protected

Referenced by DeriveFrom(), Initialize(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), ProcessInput(), and Thrust_lbs().

mIspSeaLevel

double P6DofRocketSolidPropellantObject::mIspSeaLevel

protected

Referenced by DeriveFrom(), Initialize(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), and Thrust_lbs().

mIspVacuum

double P6DofRocketSolidPropellantObject::mIspVacuum

protected

Referenced by DeriveFrom(), Initialize(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), and Thrust_lbs().

mLastThrust_lbs

double P6DofRocketSolidPropellantObject::mLastThrust_lbs

protected

Referenced by CalculateThrust(), DeriveFrom(), GetPercentMaxThrust(), P6DofRocketSolidPropellantObject(), and P6DofRocketSolidPropellantObject().

mMaxPropellantMass_lbs

double P6DofRocketSolidPropellantObject::mMaxPropellantMass_lbs

protected

Referenced by DeriveFrom(), GetMaxPropellant_lbs(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), and ProcessInput().

mPropellantCmLocation_ft

UtVec3dX P6DofRocketSolidPropellantObject::mPropellantCmLocation_ft

protected

Referenced by CalculateCurrentMassProperties(), DeriveFrom(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), and ProcessInput().

mPropellantMass_lbs

double P6DofRocketSolidPropellantObject::mPropellantMass_lbs

protected

Referenced by CalculateCurrentMassProperties(), CalculateThrust(), DeriveFrom(), GetCurrentPropellant_lbs(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), and ProcessInput().

mRatedThrust_lbs

double P6DofRocketSolidPropellantObject::mRatedThrust_lbs

protected

Referenced by DeriveFrom(), GetPercentMaxThrust(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), and ProcessInput().

mThrottleSettingPitch

ThrustControlInputValueData* P6DofRocketSolidPropellantObject::mThrottleSettingPitch

protected

Referenced by DeriveFrom(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), ProcessInput(), SetControlInputHandles(), SetControlInputValues(), and ~P6DofRocketSolidPropellantObject().

mThrottleSettingYaw

ThrustControlInputValueData* P6DofRocketSolidPropellantObject::mThrottleSettingYaw

protected

Referenced by DeriveFrom(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), ProcessInput(), SetControlInputHandles(), SetControlInputValues(), and ~P6DofRocketSolidPropellantObject().

mThrustSeaLevelVersusTime

UtCloneablePtr<UtTable::Curve> P6DofRocketSolidPropellantObject::mThrustSeaLevelVersusTime

protected

Referenced by DeriveFrom(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), ProcessInput(), and Thrust_lbs().

mThrustVacuumVersusTime

UtCloneablePtr<UtTable::Curve> P6DofRocketSolidPropellantObject::mThrustVacuumVersusTime

protected

Referenced by DeriveFrom(), P6DofRocketSolidPropellantObject(), P6DofRocketSolidPropellantObject(), ProcessInput(), and Thrust_lbs().

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The documentation for this class was generated from the following files:

• P6DofRocketSolidPropellantObject.hpp
• P6DofRocketSolidPropellantObject.cpp