#include <P6DofKinematicState.hpp>

Collaboration diagram for P6DofKinematicState:

Public Member Functions
	P6DofKinematicState ()
void	SetTheLastValues ()
void	UpdateAeroState (const P6DofAtmosphere aAtmosphere, const P6DofWind aWind, const int64_t aSimTime_nanosec, const double aDeltaT_sec)
void	GetAngleDeltas (double &aDeltaYaw_rad, double &aDeltaPitch_rad, double &aDeltaRoll_rad) const
void	SetAngleDeltas (double aDeltaYaw_rad, double aDeltaPitch_rad, double aDeltaRoll_rad)
void	RemoveAlphaForTesting (P6DofAtmosphere *aAtmospherePtr)
double	GetAlpha_deg () const
double	GetAlpha_rad () const
double	GetBeta_deg () const
double	GetBeta_rad () const
double	GetAlphaDot_dps () const
double	GetAlphaDot_rps () const
double	GetBetaDot_dps () const
double	GetBetaDot_rps () const
void	SetAlphaBetaDotToZero ()
UtDCM	GetDCM () const
void	SetDCM (const UtDCM &aDCM)
UtLLAPos	GetCurrentPositionLLA () const
double	GetSpeed_fps () const
double	GetSpeed_mps () const
double	GetSpeed_ktas () const
double	GetSpeed_kias () const
double	GetSpeed_Mach () const
UtVec3dX	GetVelocityNED_mps () const
double	GetLocalHeading_deg () const
double	GetLocalHeading_rad () const
double	GetLocalPitch_deg () const
double	GetLocalPitch_rad () const
double	GetLocalRoll_deg () const
double	GetLocalRoll_rad () const
void	SetLocalHeading_deg (double aHeading)
void	SetLocalPitch_deg (double aPitch)
void	SetLocalRoll_deg (double aRoll)
double	GetFlightPathAngle_rad () const
double	GetFlightPathAngle_deg () const
double	GetDynamicPressure_psf () const
double	GetStaticPressure_psf () const
double	GetAirDensity_slugs_per_ft3 () const
double	GetLat () const
double	GetLon () const
double	GetAlt_m () const
double	GetAlt_ft () const
void	SetAlt (double aAlt_m)
double	GetNx_g () const
double	GetNy_g () const
double	GetNz_g () const
double	GetPitchWCS () const
double	GetRollWCS () const
double	GetYawWCS () const
void	SetOrientationWCS (double aYaw_rad, double aPitch_rad, double aRoll_rad)
double	GetYawRate_rps () const
double	GetPitchRate_rps () const
double	GetRollRate_rps () const
double	GetYawRate_dps () const
double	GetPitchRate_dps () const
double	GetRollRate_dps () const
void	SetYawRate (double aYawRate_dps)
void	SetPitchRate (double aPitchRate_dps)
void	SetRollRate (double aRollRate_dps)
double	GetVerticalSpeed_fpm () const
double	GetLastDynamicPressure_psf () const
double	GetLastStaticPressure_psf () const
double	GetLastAltitudeMSL_ft () const
void	GetBodyAeroVectors (const UtDCM &aDCM, const UtVec3dX &aInertialVelVector, UtVec3dX &aLiftBodyVector, UtVec3dX &aDragBodyVector, UtVec3dX &aSideForceBodyVector) const
bool	UseSphericalEarth () const
bool	UseRotatingEarth () const
bool	IgnoreJettisonObjects () const
void	SetUseSphericalEarth (bool aValue)
void	SetUseRotatingEarth (bool aValue)
void	SetIgnoreJettisonObjects (bool aValue)
void	SetPositionLLA (double aLat, double aLon, double aAlt_m)
void	SetAttitude_rad (double aHeading_rad, double aPitch_rad, double aRoll_rad)
void	SetVerticalSpeed_fpm (double aVertSpeed_fpm)
void	SetSpeed_fps (double aSpeed_fps)
void	SetSpeed_mps (double aSpeed_mps)
void	SetSpeed_mph (double aSpeed_mph)
void	SetSpeed_ktas (double aSpeed_ktas)
void	SetSpeed_kias (double aSpeed_kias)
void	SetSpeed_Mach (double aSpeed_Mach)
void	SetBodyAccel (double aNx_g, double aNy_g, double aNz_g)
void	SetLiftDragSideForceThrustWeight (double aLift_lbs, double aDrag_lbs, double aSideForce_lbs, double aThrust_lbs, double aWgt_lbs)
void	SetMomentAtCG (UtVec3dX aMoment_ftlbs)
void	SetVelocityNED (double aVelNorth_mps, double aVelEast_mps, double aVelDown_mps)
void	CalculateRates (int64_t aSimTime_nanosec)
void	CalculateSecondaryParameters (const P6DofAtmosphere *aAtmospherePtr)
void	CalcRangeSinceStart ()
double	GetLastNx_g () const
double	GetLastNy_g () const
double	GetLastNz_g () const
UtVec3dX	CalcNEDVecFromBodyVec (const UtVec3dX &aVecBody) const
UtVec3dX	CalcNEDVecFromInertialVec (const UtVec3dX &aVecInertial) const
UtVec3dX	CalcInertialVecFromBodyVec (const UtVec3dX &aVecBody) const
UtVec3dX	CalcInertialVecFromNEDVec (const UtVec3dX &aVecNED) const
UtVec3dX	CalcBodyVecFromNEDVec (const UtVec3dX &aVecNED) const
UtVec3dX	CalcBodyVecFromInertialVec (const UtVec3dX &aVecInertial) const
UtVec3dX	GetInertialVelocity () const
UtVec3dX	GetOmegaBody () const
void	SetOmegaBody (const UtVec3dX &aOmega)
UtVec3dX	GetOmegaBodyDot () const
void	SetOmegaBodyDot (const UtVec3dX &aOmegaDot)
UtVec3dX	GetLocationWGS () const
void	SetLocationWGS (const UtVec3dX &aWGS84_pos)
UtVec3dX	GetVelocityWGS () const
void	SetVelocityWGS (const UtVec3dX &aWGS84_vel)
UtVec3dX	GetLocationSpherical () const
void	SetLocationSpherical (const UtVec3dX &aSpherical_pos)
UtVec3dX	GetVelocitySpherical () const
void	SetVelocitySpherical (const UtVec3dX &aSpherical_vel)
void	ZeroVelocity ()
UtVec3dX	GetOmegaBodyDPS () const
bool	StartingLocationInitialized () const
void	SetStartingLatLon (double aLat, double aLon)
void	GetStartingLatLon (double &aLat, double &aLon) const
double	GetRangeSinceStart_km () const
double	GetApogee_km () const
void	SetInertialAccel (const UtVec3dX &aInertialAccel)
UtVec3dX	GetInertialAccel () const
void	SetRefEarthRadius ()
UtEntity &	GetUtEntity ()
const P6DofAtmosphere *	GetAtmospherePtr () const
double	GetLift () const
double	GetDrag () const
double	GetSideForce () const
UtVec3dX	GetMoment () const
double	GetYawMoment () const
double	GetPitchMoment () const
double	GetRollMoment () const
double	GetThrust () const
double	GetWeight () const
void	SetLastUpdateTime (int64_t aLastUpdate_nanosec)
void	ZeroKinematicsDuringTesting ()

Static Public Member Functions
static bool	CalculateLLAofRelativePoint (const P6DofTerrain *aTerrainPtr, const P6DofKinematicState &aKinematicState, const UtVec3dX &aBodyRelPos_m, const UtVec3dX &aBodyRelCompressionVector, const UtVec3dX &aBodyRelRollingVector, UtVec3dX &aGearVelNED_mps, double &aLat, double &aLon, double &aAlt_m, double &aHeightAboveTerrain_m, UtVec3dX &aCompressionVectorNED, UtVec3dX &aRollingVectorInSurfaceNED, UtVec3dX &aNormalVectorNED, UtVec3dX &aSurfaceSpeedVectorNED_mps, double &aFrictionMultiplier, double &aCompression_m)
static UtVec3dX	NormalizedGravitationalAccelVec (const P6DofGravity *aGravityPtr, const double aLat, const double aLon, const double aAlt_m, const bool aUseSphericalEarth)

Protected Attributes
bool	mUseSphericalEarth
bool	mUseRotatingEarth
bool	mIgnoreJettisonObjects
UtVec3dX	mWGS84_pos
UtVec3dX	mWGS84_vel
UtVec3dX	mSpherical_pos
UtVec3dX	mSpherical_vel
UtVec3dX	mInertialAccel
UtDCM	mDCM
UtEntity	mUtEntity
UtVec3dX	mOmega
UtVec3dX	mOmegaDot
double	mNx_g
double	mNy_g
double	mNz_g
double	mLift_lbs
double	mThrust_lbs
double	mDrag_lbs
double	mSideForce_lbs
double	mWgt_lbs
UtVec3dX	mMoment_ftlbs
double	mRho_slugs_per_ft3
double	mDynamicPressure_psf
double	mStaticPressure_psf
double	mLat
double	mLon
double	mAlt_m
double	mRadarAlt_m
double	mVelNorth_mps
double	mVelEast_mps
double	mVelDown_mps
double	mAlpha_deg
double	mBeta_deg
double	mAlphaDot_dps
double	mBetaDot_dps
double	mSpeed_fps
double	mSpeed_ktas
double	mSpeed_kias
double	mSpeed_Mach
double	mVertSpeed_fpm
double	mYawRate_dps
double	mPitchRate_dps
double	mRollRate_dps
double	mLocalHeading_deg
double	mLocalPitch_deg
double	mLocalRoll_deg
double	mWcsYaw_rad
double	mWcsPitch_rad
double	mWcsRoll_rad
double	mApogee_km
double	mFlightPathAngle_rad
double	mRefEarthRadius_m
double	mRangeSinceStart_km
double	mStartingLat
double	mStartingLon
bool	mStartingLocationInitialized
double	mLastNx
double	mLastNy
double	mLastNz
double	mLastDynamicPressure_psf
double	mLastStaticPressure_psf
double	mLastAlt_m
const P6DofAtmosphere *	mAtmospherePtr
double	mDeltaYaw_rad
double	mDeltaPitch_rad
double	mDeltaRoll_rad
int64_t	mLastUpdate_nanosec = -1
double	mLastAlpha_deg = 0.0
double	mLastBeta_deg = 0.0

Static Protected Attributes
static const double	gSphericalEarthRadius_m = 6371000.0

Constructor & Destructor Documentation

◆ P6DofKinematicState()

P6DofKinematicState::P6DofKinematicState ( )

References mAlpha_deg, mAlphaDot_dps, mAlt_m, mApogee_km, mAtmospherePtr, mBeta_deg, mBetaDot_dps, mDCM, mDeltaPitch_rad, mDeltaRoll_rad, mDeltaYaw_rad, mDrag_lbs, mDynamicPressure_psf, mFlightPathAngle_rad, mIgnoreJettisonObjects, mInertialAccel, mLastAlt_m, mLastDynamicPressure_psf, mLastNx, mLastNy, mLastNz, mLastStaticPressure_psf, mLat, mLift_lbs, mLocalHeading_deg, mLocalPitch_deg, mLocalRoll_deg, mLon, mMoment_ftlbs, mNx_g, mNy_g, mNz_g, mOmega, mOmegaDot, mPitchRate_dps, mRadarAlt_m, mRangeSinceStart_km, mRefEarthRadius_m, mRho_slugs_per_ft3, mRollRate_dps, mSideForce_lbs, mSpeed_fps, mSpeed_kias, mSpeed_ktas, mSpeed_Mach, mSpherical_pos, mSpherical_vel, mStartingLat, mStartingLocationInitialized, mStartingLon, mStaticPressure_psf, mThrust_lbs, mUseRotatingEarth, mUseSphericalEarth, mVelDown_mps, mVelEast_mps, mVelNorth_mps, mVertSpeed_fpm, mWcsPitch_rad, mWcsRoll_rad, mWcsYaw_rad, mWGS84_pos, mWGS84_vel, mWgt_lbs, and mYawRate_dps.

Referenced by CalculateLLAofRelativePoint().

Member Function Documentation

◆ CalcBodyVecFromInertialVec()

UtVec3dX P6DofKinematicState::CalcBodyVecFromInertialVec ( const UtVec3dX & aVecInertial ) const

References mDCM, and mUseSphericalEarth.

Referenced by P6DofIntegrator::CalculateFM().

◆ CalcBodyVecFromNEDVec()

UtVec3dX P6DofKinematicState::CalcBodyVecFromNEDVec ( const UtVec3dX & aVecNED ) const

References P6DofUtils::GetSphericalNEDAngles(), mDCM, mLocalHeading_deg, mLocalPitch_deg, mLocalRoll_deg, mSpherical_pos, mUseSphericalEarth, and mWGS84_pos.

Referenced by CalcInertialVecFromNEDVec().

◆ CalcInertialVecFromBodyVec()

UtVec3dX P6DofKinematicState::CalcInertialVecFromBodyVec ( const UtVec3dX & aVecBody ) const

References mDCM, and mUseSphericalEarth.

Referenced by CalcInertialVecFromNEDVec(), CalcNEDVecFromBodyVec(), P6DofIntegrator::CalculateFM(), and P6DofIntegrator::PropagateUsingFM().

◆ CalcInertialVecFromNEDVec()

UtVec3dX P6DofKinematicState::CalcInertialVecFromNEDVec ( const UtVec3dX & aVecNED ) const

References CalcBodyVecFromNEDVec(), CalcInertialVecFromBodyVec(), and mUseSphericalEarth.

Referenced by P6DofIntegrator::PropagateTranslationSphericalEarth(), and P6DofIntegrator::PropagateTranslationWGSEarth().

◆ CalcNEDVecFromBodyVec()

UtVec3dX P6DofKinematicState::CalcNEDVecFromBodyVec ( const UtVec3dX & aVecBody ) const

References CalcInertialVecFromBodyVec(), CalcNEDVecFromInertialVec(), and mUseSphericalEarth.

Referenced by CalculateLLAofRelativePoint().

◆ CalcNEDVecFromInertialVec()

UtVec3dX P6DofKinematicState::CalcNEDVecFromInertialVec ( const UtVec3dX & aVecInertial ) const

References P6DofUtils::CalcSphericalVecToNED(), P6DofUtils::CalcWGS84VecToNED(), mSpherical_pos, mUseSphericalEarth, and mWGS84_pos.

Referenced by CalcNEDVecFromBodyVec(), CalculateLLAofRelativePoint(), P6DofIntegrator::PropagateTranslationSphericalEarth(), and P6DofIntegrator::PropagateTranslationWGSEarth().

◆ CalcRangeSinceStart()

void P6DofKinematicState::CalcRangeSinceStart ( )

References mLat, mLon, mRangeSinceStart_km, mRefEarthRadius_m, mStartingLat, mStartingLon, and P6DofUtils::SphericalGreatCircleHeadingAndDistance().

Referenced by CalculateSecondaryParameters().

◆ CalculateLLAofRelativePoint()

bool P6DofKinematicState::CalculateLLAofRelativePoint	(	const P6DofTerrain *	aTerrainPtr,
		const P6DofKinematicState &	aKinematicState,
		const UtVec3dX &	aBodyRelPos_m,
		const UtVec3dX &	aBodyRelCompressionVector,
		const UtVec3dX &	aBodyRelRollingVector,
		UtVec3dX &	aGearVelNED_mps,
		double &	aLat,
		double &	aLon,
		double &	aAlt_m,
		double &	aHeightAboveTerrain_m,
		UtVec3dX &	aCompressionVectorNED,
		UtVec3dX &	aRollingVectorInSurfaceNED,
		UtVec3dX &	aNormalVectorNED,
		UtVec3dX &	aSurfaceSpeedVectorNED_mps,
		double &	aFrictionMultiplier,
		double &	aCompression_m )

static

References CalcNEDVecFromBodyVec(), CalcNEDVecFromInertialVec(), P6DofUtils::CalcSphericalLatLonAlt(), P6DofTerrain::HeightOfTerrain_m(), mDCM, mOmega, mSpherical_pos, mSpherical_vel, mWGS84_pos, mWGS84_vel, P6DofKinematicState(), and UseSphericalEarth().

Referenced by P6DofGroundReactionPoint::CalcFrictionForceMoment(), P6DofGroundReactionPoint::CalcGroundReactionForceMoment(), P6DofGroundReactionPoint::CalcMaxFrictionForceMagnitude_lbs(), and P6DofGroundReactionPoint::CalcNormalForceMoment().

◆ CalculateRates()

void P6DofKinematicState::CalculateRates ( int64_t aSimTime_nanosec )

References mAlpha_deg, mAlphaDot_dps, mBeta_deg, mBetaDot_dps, mLastAlpha_deg, mLastBeta_deg, mLastUpdate_nanosec, and P6DofUtils::TimeToTime().

Referenced by P6DofIntegrator::Update().

◆ CalculateSecondaryParameters()

void P6DofKinematicState::CalculateSecondaryParameters ( const P6DofAtmosphere * aAtmospherePtr )

References P6DofUtils::AlphaBetaFromInertialVel(), P6DofAtmosphere::CalcKcasFromFps(), P6DofAtmosphere::CalcKtasFromFps(), P6DofUtils::CalcLocalAngles(), P6DofUtils::CalcLocalNEDVectors(), CalcRangeSinceStart(), P6DofUtils::CalcSphericalLatLonAlt(), P6DofUtils::CalcSphericalVecToNED(), P6DofUtils::CalcSphericalWCSAngles(), P6DofUtils::CalcUnitVectors(), P6DofAtmosphere::GetAeroParametersAtAltitude(), GetAlt_ft(), mAlpha_deg, mAlt_m, mApogee_km, mAtmospherePtr, mBeta_deg, mDCM, mDynamicPressure_psf, mFlightPathAngle_rad, mLat, mLocalHeading_deg, mLocalPitch_deg, mLocalRoll_deg, mLon, mOmega, mPitchRate_dps, mRadarAlt_m, mRho_slugs_per_ft3, mRollRate_dps, mSpeed_fps, mSpeed_kias, mSpeed_ktas, mSpeed_Mach, mSpherical_pos, mSpherical_vel, mStaticPressure_psf, mUtEntity, mVelDown_mps, mVelEast_mps, mVelNorth_mps, mVertSpeed_fpm, mWcsPitch_rad, mWcsRoll_rad, mWcsYaw_rad, mWGS84_pos, mWGS84_vel, mYawRate_dps, and UseSphericalEarth().

Referenced by RemoveAlphaForTesting(), P6DofVehicle::SeparateSubObject(), and P6DofIntegrator::Update().

◆ GetAirDensity_slugs_per_ft3()

double P6DofKinematicState::GetAirDensity_slugs_per_ft3 ( ) const

inline

References mRho_slugs_per_ft3.

◆ GetAlpha_deg()

double P6DofKinematicState::GetAlpha_deg ( ) const

References mAlpha_deg.

Referenced by P6DofVehicle::CalculateThrustVectorAndMomentUpdatePropulsion(), P6DofVehicle::GetCurrentForwardThrust_lbs(), P6DofVehicle::GetCurrentThrust_lbs(), and P6DofVehicle::UpdatePropulsionFuelBurn().

◆ GetAlpha_rad()

double P6DofKinematicState::GetAlpha_rad ( ) const

References mAlpha_deg.

Referenced by RemoveAlphaForTesting().

◆ GetAlphaDot_dps()

double P6DofKinematicState::GetAlphaDot_dps ( ) const

References mAlphaDot_dps.

◆ GetAlphaDot_rps()

double P6DofKinematicState::GetAlphaDot_rps ( ) const

References mAlphaDot_dps.

◆ GetAlt_ft()

double P6DofKinematicState::GetAlt_ft ( ) const

References mAlt_m.

Referenced by CalculateSecondaryParameters(), P6DofVehicle::CalculateThrustVectorAndMomentUpdatePropulsion(), P6DofVehicle::GetCurrentForwardThrust_lbs(), P6DofVehicle::GetCurrentThrust_lbs(), SetSpeed_fps(), SetSpeed_kias(), SetSpeed_ktas(), SetSpeed_Mach(), UpdateAeroState(), and P6DofVehicle::UpdatePropulsionFuelBurn().

◆ GetAlt_m()

double P6DofKinematicState::GetAlt_m ( ) const

References mAlt_m.

Referenced by P6DofIntegrator::CalculateFM(), P6DofIntegrator::PropagateTranslationSphericalEarth(), and P6DofIntegrator::PropagateTranslationWGSEarth().

◆ GetAngleDeltas()

void P6DofKinematicState::GetAngleDeltas	(	double &	aDeltaYaw_rad,
		double &	aDeltaPitch_rad,
		double &	aDeltaRoll_rad ) const

References mDeltaPitch_rad, mDeltaRoll_rad, and mDeltaYaw_rad.

◆ GetApogee_km()

double P6DofKinematicState::GetApogee_km ( ) const

inline

References mApogee_km.

◆ GetAtmospherePtr()

const P6DofAtmosphere * P6DofKinematicState::GetAtmospherePtr ( ) const

inline

References mAtmospherePtr.

◆ GetBeta_deg()

double P6DofKinematicState::GetBeta_deg ( ) const

References mBeta_deg.

Referenced by P6DofVehicle::CalculateThrustVectorAndMomentUpdatePropulsion(), P6DofVehicle::GetCurrentForwardThrust_lbs(), P6DofVehicle::GetCurrentThrust_lbs(), and P6DofVehicle::UpdatePropulsionFuelBurn().

◆ GetBeta_rad()

double P6DofKinematicState::GetBeta_rad ( ) const

References mBeta_deg.

Referenced by P6DofIntegrator::PropagateRotation().

◆ GetBetaDot_dps()

double P6DofKinematicState::GetBetaDot_dps ( ) const

References mBetaDot_dps.

◆ GetBetaDot_rps()

double P6DofKinematicState::GetBetaDot_rps ( ) const

References mBetaDot_dps.

◆ GetBodyAeroVectors()

void P6DofKinematicState::GetBodyAeroVectors	(	const UtDCM &	aDCM,
		const UtVec3dX &	aInertialVelVector,
		UtVec3dX &	aLiftBodyVector,
		UtVec3dX &	aDragBodyVector,
		UtVec3dX &	aSideForceBodyVector ) const

◆ GetCurrentPositionLLA()

UtLLAPos P6DofKinematicState::GetCurrentPositionLLA ( ) const

References mAlt_m, mLat, and mLon.

◆ GetDCM()

UtDCM P6DofKinematicState::GetDCM ( ) const

inline

References mDCM.

Referenced by P6DofIntegrator::PropagateRotation().

◆ GetDrag()

double P6DofKinematicState::GetDrag ( ) const

inline

References mDrag_lbs.

Referenced by P6DofIntegrator::Update().

◆ GetDynamicPressure_psf()

double P6DofKinematicState::GetDynamicPressure_psf ( ) const

inline

References mDynamicPressure_psf.

Referenced by P6DofVehicle::CalculateThrustVectorAndMomentUpdatePropulsion(), P6DofVehicle::GetCurrentForwardThrust_lbs(), P6DofVehicle::GetCurrentThrust_lbs(), and P6DofVehicle::UpdatePropulsionFuelBurn().

◆ GetFlightPathAngle_deg()

double P6DofKinematicState::GetFlightPathAngle_deg ( ) const

References mFlightPathAngle_rad.

◆ GetFlightPathAngle_rad()

double P6DofKinematicState::GetFlightPathAngle_rad ( ) const

inline

References mFlightPathAngle_rad.

◆ GetInertialAccel()

UtVec3dX P6DofKinematicState::GetInertialAccel ( ) const

inline

References mInertialAccel.

Referenced by P6DofIntegrator::PropagateTranslationSphericalEarth(), and P6DofIntegrator::PropagateTranslationWGSEarth().

◆ GetInertialVelocity()

UtVec3dX P6DofKinematicState::GetInertialVelocity ( ) const

References mSpherical_vel, mWGS84_vel, and UseSphericalEarth().

◆ GetLastAltitudeMSL_ft()

double P6DofKinematicState::GetLastAltitudeMSL_ft ( ) const

References mLastAlt_m.

◆ GetLastDynamicPressure_psf()

double P6DofKinematicState::GetLastDynamicPressure_psf ( ) const

References mLastDynamicPressure_psf.

◆ GetLastNx_g()

double P6DofKinematicState::GetLastNx_g ( ) const

References mLastNx.

◆ GetLastNy_g()

double P6DofKinematicState::GetLastNy_g ( ) const

References mLastNy.

◆ GetLastNz_g()

double P6DofKinematicState::GetLastNz_g ( ) const

References mLastNz.

◆ GetLastStaticPressure_psf()

double P6DofKinematicState::GetLastStaticPressure_psf ( ) const

References mLastStaticPressure_psf.

◆ GetLat()

double P6DofKinematicState::GetLat ( ) const

References mLat.

Referenced by P6DofIntegrator::CalculateFM(), P6DofIntegrator::PropagateTranslationSphericalEarth(), and P6DofIntegrator::PropagateTranslationWGSEarth().

◆ GetLift()

double P6DofKinematicState::GetLift ( ) const

inline

References mLift_lbs.

Referenced by P6DofIntegrator::Update().

◆ GetLocalHeading_deg()

double P6DofKinematicState::GetLocalHeading_deg ( ) const

inline

References mLocalHeading_deg.

◆ GetLocalHeading_rad()

double P6DofKinematicState::GetLocalHeading_rad ( ) const

References mLocalHeading_deg.

◆ GetLocalPitch_deg()

double P6DofKinematicState::GetLocalPitch_deg ( ) const

inline

References mLocalPitch_deg.

◆ GetLocalPitch_rad()

double P6DofKinematicState::GetLocalPitch_rad ( ) const

References mLocalPitch_deg.

◆ GetLocalRoll_deg()

double P6DofKinematicState::GetLocalRoll_deg ( ) const

inline

References mLocalRoll_deg.

◆ GetLocalRoll_rad()

double P6DofKinematicState::GetLocalRoll_rad ( ) const

References mLocalRoll_deg.

◆ GetLocationSpherical()

UtVec3dX P6DofKinematicState::GetLocationSpherical ( ) const

inline

References mSpherical_pos.

Referenced by P6DofIntegrator::PropagateTranslationSphericalEarth().

◆ GetLocationWGS()

UtVec3dX P6DofKinematicState::GetLocationWGS ( ) const

inline

References mWGS84_pos.

Referenced by P6DofIntegrator::PropagateTranslationWGSEarth().

◆ GetLon()

double P6DofKinematicState::GetLon ( ) const

References mLon.

Referenced by P6DofIntegrator::CalculateFM(), P6DofIntegrator::PropagateTranslationSphericalEarth(), and P6DofIntegrator::PropagateTranslationWGSEarth().

◆ GetMoment()

UtVec3dX P6DofKinematicState::GetMoment ( ) const

inline

References mMoment_ftlbs.

Referenced by P6DofIntegrator::Update().

◆ GetNx_g()

double P6DofKinematicState::GetNx_g ( ) const

References mNx_g.

◆ GetNy_g()

double P6DofKinematicState::GetNy_g ( ) const

References mNy_g.

◆ GetNz_g()

double P6DofKinematicState::GetNz_g ( ) const

References mNz_g.

◆ GetOmegaBody()

UtVec3dX P6DofKinematicState::GetOmegaBody ( ) const

inline

References mOmega.

Referenced by P6DofIntegrator::PropagateRotation().

◆ GetOmegaBodyDot()

UtVec3dX P6DofKinematicState::GetOmegaBodyDot ( ) const

inline

References mOmegaDot.

Referenced by P6DofIntegrator::PropagateRotation().

◆ GetOmegaBodyDPS()

UtVec3dX P6DofKinematicState::GetOmegaBodyDPS ( ) const

References mOmega.

◆ GetPitchMoment()

double P6DofKinematicState::GetPitchMoment ( ) const

inline

References mMoment_ftlbs.

◆ GetPitchRate_dps()

double P6DofKinematicState::GetPitchRate_dps ( ) const

References mOmega.

◆ GetPitchRate_rps()

double P6DofKinematicState::GetPitchRate_rps ( ) const

References mOmega.

◆ GetPitchWCS()

double P6DofKinematicState::GetPitchWCS ( ) const

inline

References mWcsPitch_rad.

◆ GetRangeSinceStart_km()

double P6DofKinematicState::GetRangeSinceStart_km ( ) const

inline

References mRangeSinceStart_km.

◆ GetRollMoment()

double P6DofKinematicState::GetRollMoment ( ) const

inline

References mMoment_ftlbs.

◆ GetRollRate_dps()

double P6DofKinematicState::GetRollRate_dps ( ) const

References mOmega.

◆ GetRollRate_rps()

double P6DofKinematicState::GetRollRate_rps ( ) const

References mOmega.

◆ GetRollWCS()

double P6DofKinematicState::GetRollWCS ( ) const

inline

References mWcsRoll_rad.

◆ GetSideForce()

double P6DofKinematicState::GetSideForce ( ) const

inline

References mSideForce_lbs.

Referenced by P6DofIntegrator::Update().

◆ GetSpeed_fps()

double P6DofKinematicState::GetSpeed_fps ( ) const

inline

References mSpeed_fps.

Referenced by P6DofVehicle::CalculateThrustVectorAndMomentUpdatePropulsion(), P6DofVehicle::GetCurrentForwardThrust_lbs(), P6DofVehicle::GetCurrentThrust_lbs(), and P6DofVehicle::UpdatePropulsionFuelBurn().

◆ GetSpeed_kias()

double P6DofKinematicState::GetSpeed_kias ( ) const

inline

References mSpeed_kias.

◆ GetSpeed_ktas()

double P6DofKinematicState::GetSpeed_ktas ( ) const

inline

References mSpeed_ktas.

◆ GetSpeed_Mach()

double P6DofKinematicState::GetSpeed_Mach ( ) const

inline

References mSpeed_Mach.

Referenced by P6DofVehicle::CalculateThrustVectorAndMomentUpdatePropulsion(), P6DofVehicle::GetCurrentForwardThrust_lbs(), P6DofVehicle::GetCurrentThrust_lbs(), and P6DofVehicle::UpdatePropulsionFuelBurn().

◆ GetSpeed_mps()

double P6DofKinematicState::GetSpeed_mps ( ) const

References mSpeed_fps.

◆ GetStartingLatLon()

void P6DofKinematicState::GetStartingLatLon	(	double &	aLat,
		double &	aLon ) const

References mStartingLat, and mStartingLon.

◆ GetStaticPressure_psf()

double P6DofKinematicState::GetStaticPressure_psf ( ) const

inline

References mStaticPressure_psf.

◆ GetThrust()

double P6DofKinematicState::GetThrust ( ) const

inline

References mThrust_lbs.

Referenced by P6DofIntegrator::Update().

◆ GetUtEntity()

UtEntity & P6DofKinematicState::GetUtEntity ( )

inline

References mUtEntity.

◆ GetVelocityNED_mps()

UtVec3dX P6DofKinematicState::GetVelocityNED_mps ( ) const

References P6DofUtils::CalcSphericalVecToNED(), mSpherical_pos, mSpherical_vel, mUseSphericalEarth, mWGS84_pos, and mWGS84_vel.

Referenced by P6DofIntegrator::PropagateRotation().

◆ GetVelocitySpherical()

UtVec3dX P6DofKinematicState::GetVelocitySpherical ( ) const

inline

References mSpherical_vel.

Referenced by P6DofIntegrator::PropagateTranslationSphericalEarth().

◆ GetVelocityWGS()

UtVec3dX P6DofKinematicState::GetVelocityWGS ( ) const

inline

References mWGS84_vel.

Referenced by P6DofIntegrator::PropagateTranslationWGSEarth().

◆ GetVerticalSpeed_fpm()

double P6DofKinematicState::GetVerticalSpeed_fpm ( ) const

inline

References mVertSpeed_fpm.

◆ GetWeight()

double P6DofKinematicState::GetWeight ( ) const

inline

References mWgt_lbs.

Referenced by P6DofIntegrator::Update().

◆ GetYawMoment()

double P6DofKinematicState::GetYawMoment ( ) const

inline

References mMoment_ftlbs.

◆ GetYawRate_dps()

double P6DofKinematicState::GetYawRate_dps ( ) const

References mOmega.

◆ GetYawRate_rps()

double P6DofKinematicState::GetYawRate_rps ( ) const

References mOmega.

◆ GetYawWCS()

double P6DofKinematicState::GetYawWCS ( ) const

inline

References mWcsYaw_rad.

◆ IgnoreJettisonObjects()

bool P6DofKinematicState::IgnoreJettisonObjects ( ) const

inline

References mIgnoreJettisonObjects.

◆ NormalizedGravitationalAccelVec()

UtVec3dX P6DofKinematicState::NormalizedGravitationalAccelVec	(	const P6DofGravity *	aGravityPtr,
		const double	aLat,
		const double	aLon,
		const double	aAlt_m,
		const bool	aUseSphericalEarth )

static

References P6DofGravity::NormalizedGravitationalAccel().

Referenced by P6DofIntegrator::CalculateFM().

◆ RemoveAlphaForTesting()

void P6DofKinematicState::RemoveAlphaForTesting ( P6DofAtmosphere * aAtmospherePtr )

References CalculateSecondaryParameters(), GetAlpha_rad(), and mDCM.

Referenced by P6DofIntegrator::Update().

◆ SetAlphaBetaDotToZero()

void P6DofKinematicState::SetAlphaBetaDotToZero ( )

References mAlpha_deg, mAlphaDot_dps, mBeta_deg, mBetaDot_dps, mLastAlpha_deg, and mLastBeta_deg.

◆ SetAlt()

void P6DofKinematicState::SetAlt ( double aAlt_m )

inline

References mAlt_m.

◆ SetAngleDeltas()

void P6DofKinematicState::SetAngleDeltas	(	double	aDeltaYaw_rad,
		double	aDeltaPitch_rad,
		double	aDeltaRoll_rad )

References mDeltaPitch_rad, mDeltaRoll_rad, and mDeltaYaw_rad.

Referenced by P6DofIntegrator::PropagateRotation().

◆ SetAttitude_rad()

void P6DofKinematicState::SetAttitude_rad	(	double	aHeading_rad,
		double	aPitch_rad,
		double	aRoll_rad )

References mLocalHeading_deg, mLocalPitch_deg, and mLocalRoll_deg.

◆ SetBodyAccel()

void P6DofKinematicState::SetBodyAccel	(	double	aNx_g,
		double	aNy_g,
		double	aNz_g )

References mNx_g, mNy_g, and mNz_g.

Referenced by P6DofIntegrator::PropagateUsingFM().

◆ SetDCM()

void P6DofKinematicState::SetDCM ( const UtDCM & aDCM )

inline

References mDCM.

Referenced by P6DofIntegrator::PropagateRotation().

◆ SetIgnoreJettisonObjects()

void P6DofKinematicState::SetIgnoreJettisonObjects ( bool aValue )

inline

References mIgnoreJettisonObjects.

◆ SetInertialAccel()

void P6DofKinematicState::SetInertialAccel ( const UtVec3dX & aInertialAccel )

inline

References mInertialAccel.

Referenced by P6DofIntegrator::PropagateTranslationSphericalEarth(), and P6DofIntegrator::PropagateTranslationWGSEarth().

◆ SetLastUpdateTime()

void P6DofKinematicState::SetLastUpdateTime ( int64_t aLastUpdate_nanosec )

inline

References mLastUpdate_nanosec.

◆ SetLiftDragSideForceThrustWeight()

void P6DofKinematicState::SetLiftDragSideForceThrustWeight	(	double	aLift_lbs,
		double	aDrag_lbs,
		double	aSideForce_lbs,
		double	aThrust_lbs,
		double	aWgt_lbs )

References mDrag_lbs, mLift_lbs, mSideForce_lbs, mThrust_lbs, and mWgt_lbs.

Referenced by P6DofIntegrator::CalculateFM(), and P6DofIntegrator::Update().

◆ SetLocalHeading_deg()

void P6DofKinematicState::SetLocalHeading_deg ( double aHeading )

inline

References mLocalHeading_deg.

◆ SetLocalPitch_deg()

void P6DofKinematicState::SetLocalPitch_deg ( double aPitch )

inline

References mLocalPitch_deg.

◆ SetLocalRoll_deg()

void P6DofKinematicState::SetLocalRoll_deg ( double aRoll )

inline

References mLocalRoll_deg.

◆ SetLocationSpherical()

void P6DofKinematicState::SetLocationSpherical ( const UtVec3dX & aSpherical_pos )

inline

References mSpherical_pos.

Referenced by P6DofIntegrator::PropagateTranslationSphericalEarth().

◆ SetLocationWGS()

void P6DofKinematicState::SetLocationWGS ( const UtVec3dX & aWGS84_pos )

inline

References mWGS84_pos.

Referenced by P6DofIntegrator::PropagateTranslationWGSEarth().

◆ SetMomentAtCG()

void P6DofKinematicState::SetMomentAtCG ( UtVec3dX aMoment_ftlbs )

References mMoment_ftlbs.

Referenced by P6DofIntegrator::CalculateFM(), and P6DofIntegrator::Update().

◆ SetOmegaBody()

void P6DofKinematicState::SetOmegaBody ( const UtVec3dX & aOmega )

inline

References mOmega.

Referenced by P6DofIntegrator::PropagateRotation().

◆ SetOmegaBodyDot()

void P6DofKinematicState::SetOmegaBodyDot ( const UtVec3dX & aOmegaDot )

inline

References mOmegaDot.

Referenced by P6DofIntegrator::PropagateRotation().

◆ SetOrientationWCS()

void P6DofKinematicState::SetOrientationWCS	(	double	aYaw_rad,
		double	aPitch_rad,
		double	aRoll_rad )

References mWcsPitch_rad, mWcsRoll_rad, and mWcsYaw_rad.

◆ SetPitchRate()

void P6DofKinematicState::SetPitchRate ( double aPitchRate_dps )

References mOmega.

◆ SetPositionLLA()

void P6DofKinematicState::SetPositionLLA	(	double	aLat,
		double	aLon,
		double	aAlt_m )

References mAlt_m, mLat, and mLon.

◆ SetRefEarthRadius()

void P6DofKinematicState::SetRefEarthRadius ( )

References gSphericalEarthRadius_m, mRefEarthRadius_m, mStartingLat, mStartingLon, and UseSphericalEarth().

◆ SetRollRate()

void P6DofKinematicState::SetRollRate ( double aRollRate_dps )

References mOmega.

◆ SetSpeed_fps()

void P6DofKinematicState::SetSpeed_fps ( double aSpeed_fps )

References GetAlt_ft(), mAtmospherePtr, mSpeed_fps, mSpeed_kias, mSpeed_ktas, and mSpeed_Mach.

Referenced by SetSpeed_mph(), SetSpeed_mps(), and ZeroKinematicsDuringTesting().

◆ SetSpeed_kias()

void P6DofKinematicState::SetSpeed_kias ( double aSpeed_kias )

References GetAlt_ft(), mAtmospherePtr, mSpeed_fps, mSpeed_kias, mSpeed_ktas, and mSpeed_Mach.

◆ SetSpeed_ktas()

void P6DofKinematicState::SetSpeed_ktas ( double aSpeed_ktas )

References GetAlt_ft(), mAtmospherePtr, mSpeed_fps, mSpeed_kias, mSpeed_ktas, and mSpeed_Mach.

◆ SetSpeed_Mach()

void P6DofKinematicState::SetSpeed_Mach ( double aSpeed_Mach )

References GetAlt_ft(), mAtmospherePtr, mSpeed_fps, mSpeed_kias, mSpeed_ktas, and mSpeed_Mach.

◆ SetSpeed_mph()

void P6DofKinematicState::SetSpeed_mph ( double aSpeed_mph )

References SetSpeed_fps().

◆ SetSpeed_mps()

void P6DofKinematicState::SetSpeed_mps ( double aSpeed_mps )

References SetSpeed_fps().

◆ SetStartingLatLon()

void P6DofKinematicState::SetStartingLatLon	(	double	aLat,
		double	aLon )

References mStartingLat, mStartingLocationInitialized, and mStartingLon.

◆ SetTheLastValues()

void P6DofKinematicState::SetTheLastValues ( )

References mAlt_m, mDynamicPressure_psf, mLastAlt_m, mLastDynamicPressure_psf, mLastNx, mLastNy, mLastNz, mLastStaticPressure_psf, mNx_g, mNy_g, mNz_g, and mStaticPressure_psf.

◆ SetUseRotatingEarth()

void P6DofKinematicState::SetUseRotatingEarth ( bool aValue )

inline

References mUseRotatingEarth.

◆ SetUseSphericalEarth()

void P6DofKinematicState::SetUseSphericalEarth ( bool aValue )

inline

References mUseSphericalEarth.

◆ SetVelocityNED()

void P6DofKinematicState::SetVelocityNED	(	double	aVelNorth_mps,
		double	aVelEast_mps,
		double	aVelDown_mps )

References P6DofUtils::CalcSphericalNEDVelToSphericalVel(), mSpherical_pos, mSpherical_vel, mUseSphericalEarth, mVelDown_mps, mVelEast_mps, mVelNorth_mps, mWGS84_pos, and mWGS84_vel.

Referenced by P6DofIntegrator::PropagateRotation().

◆ SetVelocitySpherical()

void P6DofKinematicState::SetVelocitySpherical ( const UtVec3dX & aSpherical_vel )

inline

References mSpherical_vel.

Referenced by P6DofIntegrator::PropagateTranslationSphericalEarth().

◆ SetVelocityWGS()

void P6DofKinematicState::SetVelocityWGS ( const UtVec3dX & aWGS84_vel )

inline

References mWGS84_vel.

Referenced by P6DofIntegrator::PropagateTranslationWGSEarth().

◆ SetVerticalSpeed_fpm()

void P6DofKinematicState::SetVerticalSpeed_fpm ( double aVertSpeed_fpm )

References mVertSpeed_fpm.

◆ SetYawRate()

void P6DofKinematicState::SetYawRate ( double aYawRate_dps )

References mOmega.

◆ StartingLocationInitialized()

bool P6DofKinematicState::StartingLocationInitialized ( ) const

inline

References mStartingLocationInitialized.

◆ UpdateAeroState()

void P6DofKinematicState::UpdateAeroState	(	const P6DofAtmosphere *	aAtmosphere,
		const P6DofWind *	aWind,
		const int64_t	aSimTime_nanosec,
		const double	aDeltaT_sec )

◆ UseRotatingEarth()

bool P6DofKinematicState::UseRotatingEarth ( ) const

inline

References mUseRotatingEarth.

◆ UseSphericalEarth()

bool P6DofKinematicState::UseSphericalEarth ( ) const

inline

References mUseSphericalEarth.

Referenced by P6DofIntegrator::CalculateFM(), CalculateLLAofRelativePoint(), CalculateSecondaryParameters(), GetInertialVelocity(), P6DofIntegrator::PropagateTranslation(), SetRefEarthRadius(), and ZeroVelocity().

◆ ZeroKinematicsDuringTesting()

void P6DofKinematicState::ZeroKinematicsDuringTesting ( )

◆ ZeroVelocity()

void P6DofKinematicState::ZeroVelocity ( )

References mSpherical_vel, mWGS84_vel, UseSphericalEarth(), and vel.

Referenced by ZeroKinematicsDuringTesting().

Member Data Documentation

◆ gSphericalEarthRadius_m

const double P6DofKinematicState::gSphericalEarthRadius_m = 6371000.0

staticprotected

Referenced by SetRefEarthRadius().

◆ mAlpha_deg

double P6DofKinematicState::mAlpha_deg

protected

Referenced by CalculateRates(), CalculateSecondaryParameters(), GetAlpha_deg(), GetAlpha_rad(), P6DofKinematicState(), SetAlphaBetaDotToZero(), UpdateAeroState(), and ZeroKinematicsDuringTesting().

◆ mAlphaDot_dps

double P6DofKinematicState::mAlphaDot_dps

protected

Referenced by CalculateRates(), GetAlphaDot_dps(), GetAlphaDot_rps(), P6DofKinematicState(), SetAlphaBetaDotToZero(), UpdateAeroState(), and ZeroKinematicsDuringTesting().

◆ mAlt_m

double P6DofKinematicState::mAlt_m

protected

Referenced by CalculateSecondaryParameters(), GetAlt_ft(), GetAlt_m(), GetCurrentPositionLLA(), P6DofKinematicState(), SetAlt(), SetPositionLLA(), and SetTheLastValues().

◆ mApogee_km

double P6DofKinematicState::mApogee_km

protected

Referenced by CalculateSecondaryParameters(), GetApogee_km(), and P6DofKinematicState().

◆ mAtmospherePtr

const P6DofAtmosphere* P6DofKinematicState::mAtmospherePtr

protected

Referenced by CalculateSecondaryParameters(), GetAtmospherePtr(), P6DofKinematicState(), SetSpeed_fps(), SetSpeed_kias(), SetSpeed_ktas(), SetSpeed_Mach(), and UpdateAeroState().

◆ mBeta_deg

double P6DofKinematicState::mBeta_deg

protected

Referenced by CalculateRates(), CalculateSecondaryParameters(), GetBeta_deg(), GetBeta_rad(), P6DofKinematicState(), SetAlphaBetaDotToZero(), UpdateAeroState(), and ZeroKinematicsDuringTesting().

◆ mBetaDot_dps

double P6DofKinematicState::mBetaDot_dps

protected

Referenced by CalculateRates(), GetBetaDot_dps(), GetBetaDot_rps(), P6DofKinematicState(), SetAlphaBetaDotToZero(), UpdateAeroState(), and ZeroKinematicsDuringTesting().

◆ mDCM

UtDCM P6DofKinematicState::mDCM

protected

Referenced by CalcBodyVecFromInertialVec(), CalcBodyVecFromNEDVec(), CalcInertialVecFromBodyVec(), CalculateLLAofRelativePoint(), CalculateSecondaryParameters(), GetDCM(), P6DofKinematicState(), RemoveAlphaForTesting(), SetDCM(), and UpdateAeroState().

◆ mDeltaPitch_rad

double P6DofKinematicState::mDeltaPitch_rad

protected

Referenced by GetAngleDeltas(), P6DofKinematicState(), SetAngleDeltas(), and ZeroKinematicsDuringTesting().

◆ mDeltaRoll_rad

double P6DofKinematicState::mDeltaRoll_rad

protected

Referenced by GetAngleDeltas(), P6DofKinematicState(), SetAngleDeltas(), and ZeroKinematicsDuringTesting().

◆ mDeltaYaw_rad

double P6DofKinematicState::mDeltaYaw_rad

protected

Referenced by GetAngleDeltas(), P6DofKinematicState(), SetAngleDeltas(), and ZeroKinematicsDuringTesting().

◆ mDrag_lbs

double P6DofKinematicState::mDrag_lbs

protected

Referenced by GetDrag(), P6DofKinematicState(), SetLiftDragSideForceThrustWeight(), and ZeroKinematicsDuringTesting().

◆ mDynamicPressure_psf

double P6DofKinematicState::mDynamicPressure_psf

protected

Referenced by CalculateSecondaryParameters(), GetDynamicPressure_psf(), P6DofKinematicState(), SetTheLastValues(), and UpdateAeroState().

◆ mFlightPathAngle_rad

double P6DofKinematicState::mFlightPathAngle_rad

protected

Referenced by CalculateSecondaryParameters(), GetFlightPathAngle_deg(), GetFlightPathAngle_rad(), P6DofKinematicState(), and ZeroKinematicsDuringTesting().

◆ mIgnoreJettisonObjects

bool P6DofKinematicState::mIgnoreJettisonObjects

protected

Referenced by IgnoreJettisonObjects(), P6DofKinematicState(), and SetIgnoreJettisonObjects().

◆ mInertialAccel

UtVec3dX P6DofKinematicState::mInertialAccel

protected

Referenced by GetInertialAccel(), P6DofKinematicState(), SetInertialAccel(), and ZeroKinematicsDuringTesting().

◆ mLastAlpha_deg

double P6DofKinematicState::mLastAlpha_deg = 0.0

protected

Referenced by CalculateRates(), SetAlphaBetaDotToZero(), and ZeroKinematicsDuringTesting().

◆ mLastAlt_m

double P6DofKinematicState::mLastAlt_m

protected

Referenced by GetLastAltitudeMSL_ft(), P6DofKinematicState(), and SetTheLastValues().

◆ mLastBeta_deg

double P6DofKinematicState::mLastBeta_deg = 0.0

protected

Referenced by CalculateRates(), SetAlphaBetaDotToZero(), and ZeroKinematicsDuringTesting().

◆ mLastDynamicPressure_psf

double P6DofKinematicState::mLastDynamicPressure_psf

protected

Referenced by GetLastDynamicPressure_psf(), P6DofKinematicState(), and SetTheLastValues().

◆ mLastNx

double P6DofKinematicState::mLastNx

protected

Referenced by GetLastNx_g(), P6DofKinematicState(), SetTheLastValues(), and ZeroKinematicsDuringTesting().

◆ mLastNy

double P6DofKinematicState::mLastNy

protected

Referenced by GetLastNy_g(), P6DofKinematicState(), SetTheLastValues(), and ZeroKinematicsDuringTesting().

◆ mLastNz

double P6DofKinematicState::mLastNz

protected

Referenced by GetLastNz_g(), P6DofKinematicState(), SetTheLastValues(), and ZeroKinematicsDuringTesting().

◆ mLastStaticPressure_psf

double P6DofKinematicState::mLastStaticPressure_psf

protected

Referenced by GetLastStaticPressure_psf(), P6DofKinematicState(), and SetTheLastValues().

◆ mLastUpdate_nanosec

int64_t P6DofKinematicState::mLastUpdate_nanosec = -1

protected

Referenced by CalculateRates(), and SetLastUpdateTime().

◆ mLat

double P6DofKinematicState::mLat

protected

Referenced by CalcRangeSinceStart(), CalculateSecondaryParameters(), GetCurrentPositionLLA(), GetLat(), P6DofKinematicState(), and SetPositionLLA().

◆ mLift_lbs

double P6DofKinematicState::mLift_lbs

protected

Referenced by GetLift(), P6DofKinematicState(), SetLiftDragSideForceThrustWeight(), and ZeroKinematicsDuringTesting().

◆ mLocalHeading_deg

double P6DofKinematicState::mLocalHeading_deg

protected

Referenced by CalcBodyVecFromNEDVec(), CalculateSecondaryParameters(), GetLocalHeading_deg(), GetLocalHeading_rad(), P6DofKinematicState(), SetAttitude_rad(), SetLocalHeading_deg(), and ZeroKinematicsDuringTesting().

◆ mLocalPitch_deg

double P6DofKinematicState::mLocalPitch_deg

protected

Referenced by CalcBodyVecFromNEDVec(), CalculateSecondaryParameters(), GetLocalPitch_deg(), GetLocalPitch_rad(), P6DofKinematicState(), SetAttitude_rad(), SetLocalPitch_deg(), and ZeroKinematicsDuringTesting().

◆ mLocalRoll_deg

double P6DofKinematicState::mLocalRoll_deg

protected

Referenced by CalcBodyVecFromNEDVec(), CalculateSecondaryParameters(), GetLocalRoll_deg(), GetLocalRoll_rad(), P6DofKinematicState(), SetAttitude_rad(), SetLocalRoll_deg(), and ZeroKinematicsDuringTesting().

◆ mLon

double P6DofKinematicState::mLon

protected

Referenced by CalcRangeSinceStart(), CalculateSecondaryParameters(), GetCurrentPositionLLA(), GetLon(), P6DofKinematicState(), and SetPositionLLA().

◆ mMoment_ftlbs

UtVec3dX P6DofKinematicState::mMoment_ftlbs

protected

Referenced by GetMoment(), GetPitchMoment(), GetRollMoment(), GetYawMoment(), P6DofKinematicState(), SetMomentAtCG(), and ZeroKinematicsDuringTesting().

◆ mNx_g

double P6DofKinematicState::mNx_g

protected

Referenced by GetNx_g(), P6DofKinematicState(), SetBodyAccel(), SetTheLastValues(), and ZeroKinematicsDuringTesting().

◆ mNy_g

double P6DofKinematicState::mNy_g

protected

Referenced by GetNy_g(), P6DofKinematicState(), SetBodyAccel(), SetTheLastValues(), and ZeroKinematicsDuringTesting().

◆ mNz_g

double P6DofKinematicState::mNz_g

protected

Referenced by GetNz_g(), P6DofKinematicState(), SetBodyAccel(), SetTheLastValues(), and ZeroKinematicsDuringTesting().

◆ mOmega

UtVec3dX P6DofKinematicState::mOmega

protected

Referenced by CalculateLLAofRelativePoint(), CalculateSecondaryParameters(), GetOmegaBody(), GetOmegaBodyDPS(), GetPitchRate_dps(), GetPitchRate_rps(), GetRollRate_dps(), GetRollRate_rps(), GetYawRate_dps(), GetYawRate_rps(), P6DofKinematicState(), SetOmegaBody(), SetPitchRate(), SetRollRate(), SetYawRate(), and ZeroKinematicsDuringTesting().

◆ mOmegaDot

UtVec3dX P6DofKinematicState::mOmegaDot

protected

Referenced by GetOmegaBodyDot(), P6DofKinematicState(), SetOmegaBodyDot(), and ZeroKinematicsDuringTesting().

◆ mPitchRate_dps

double P6DofKinematicState::mPitchRate_dps

protected

Referenced by CalculateSecondaryParameters(), P6DofKinematicState(), and ZeroKinematicsDuringTesting().

◆ mRadarAlt_m

double P6DofKinematicState::mRadarAlt_m

protected

Referenced by CalculateSecondaryParameters(), and P6DofKinematicState().

◆ mRangeSinceStart_km

double P6DofKinematicState::mRangeSinceStart_km

protected

Referenced by CalcRangeSinceStart(), GetRangeSinceStart_km(), and P6DofKinematicState().

◆ mRefEarthRadius_m

double P6DofKinematicState::mRefEarthRadius_m

protected

Referenced by CalcRangeSinceStart(), P6DofKinematicState(), and SetRefEarthRadius().

◆ mRho_slugs_per_ft3

double P6DofKinematicState::mRho_slugs_per_ft3

protected

Referenced by CalculateSecondaryParameters(), GetAirDensity_slugs_per_ft3(), P6DofKinematicState(), and UpdateAeroState().

◆ mRollRate_dps

double P6DofKinematicState::mRollRate_dps

protected

Referenced by CalculateSecondaryParameters(), P6DofKinematicState(), and ZeroKinematicsDuringTesting().

◆ mSideForce_lbs

double P6DofKinematicState::mSideForce_lbs

protected

Referenced by GetSideForce(), P6DofKinematicState(), SetLiftDragSideForceThrustWeight(), and ZeroKinematicsDuringTesting().

◆ mSpeed_fps

double P6DofKinematicState::mSpeed_fps

protected

Referenced by CalculateSecondaryParameters(), GetSpeed_fps(), GetSpeed_mps(), P6DofKinematicState(), SetSpeed_fps(), SetSpeed_kias(), SetSpeed_ktas(), SetSpeed_Mach(), and UpdateAeroState().

◆ mSpeed_kias

double P6DofKinematicState::mSpeed_kias

protected

Referenced by CalculateSecondaryParameters(), GetSpeed_kias(), P6DofKinematicState(), SetSpeed_fps(), SetSpeed_kias(), SetSpeed_ktas(), SetSpeed_Mach(), and UpdateAeroState().

◆ mSpeed_ktas

double P6DofKinematicState::mSpeed_ktas

protected

Referenced by CalculateSecondaryParameters(), GetSpeed_ktas(), P6DofKinematicState(), SetSpeed_fps(), SetSpeed_kias(), SetSpeed_ktas(), SetSpeed_Mach(), and UpdateAeroState().

◆ mSpeed_Mach

double P6DofKinematicState::mSpeed_Mach

protected

Referenced by CalculateSecondaryParameters(), GetSpeed_Mach(), P6DofKinematicState(), SetSpeed_fps(), SetSpeed_kias(), SetSpeed_ktas(), SetSpeed_Mach(), and UpdateAeroState().

◆ mSpherical_pos

UtVec3dX P6DofKinematicState::mSpherical_pos

protected

Referenced by CalcBodyVecFromNEDVec(), CalcNEDVecFromInertialVec(), CalculateLLAofRelativePoint(), CalculateSecondaryParameters(), GetLocationSpherical(), GetVelocityNED_mps(), P6DofKinematicState(), SetLocationSpherical(), and SetVelocityNED().

◆ mSpherical_vel

UtVec3dX P6DofKinematicState::mSpherical_vel

protected

Referenced by CalculateLLAofRelativePoint(), CalculateSecondaryParameters(), GetInertialVelocity(), GetVelocityNED_mps(), GetVelocitySpherical(), P6DofKinematicState(), SetVelocityNED(), SetVelocitySpherical(), UpdateAeroState(), and ZeroVelocity().

◆ mStartingLat

double P6DofKinematicState::mStartingLat

protected

Referenced by CalcRangeSinceStart(), GetStartingLatLon(), P6DofKinematicState(), SetRefEarthRadius(), and SetStartingLatLon().

◆ mStartingLocationInitialized

bool P6DofKinematicState::mStartingLocationInitialized

protected

Referenced by P6DofKinematicState(), SetStartingLatLon(), and StartingLocationInitialized().

◆ mStartingLon

double P6DofKinematicState::mStartingLon

protected

Referenced by CalcRangeSinceStart(), GetStartingLatLon(), P6DofKinematicState(), SetRefEarthRadius(), and SetStartingLatLon().

◆ mStaticPressure_psf

double P6DofKinematicState::mStaticPressure_psf

protected

Referenced by CalculateSecondaryParameters(), GetStaticPressure_psf(), P6DofKinematicState(), SetTheLastValues(), and UpdateAeroState().

◆ mThrust_lbs

double P6DofKinematicState::mThrust_lbs

protected

Referenced by GetThrust(), P6DofKinematicState(), SetLiftDragSideForceThrustWeight(), and ZeroKinematicsDuringTesting().

◆ mUseRotatingEarth

bool P6DofKinematicState::mUseRotatingEarth

protected

Referenced by P6DofKinematicState(), SetUseRotatingEarth(), and UseRotatingEarth().

◆ mUseSphericalEarth

bool P6DofKinematicState::mUseSphericalEarth

protected

Referenced by CalcBodyVecFromInertialVec(), CalcBodyVecFromNEDVec(), CalcInertialVecFromBodyVec(), CalcInertialVecFromNEDVec(), CalcNEDVecFromBodyVec(), CalcNEDVecFromInertialVec(), GetVelocityNED_mps(), P6DofKinematicState(), SetUseSphericalEarth(), SetVelocityNED(), UpdateAeroState(), and UseSphericalEarth().

◆ mUtEntity

UtEntity P6DofKinematicState::mUtEntity

protected

Referenced by CalculateSecondaryParameters(), and GetUtEntity().

◆ mVelDown_mps

double P6DofKinematicState::mVelDown_mps

protected

Referenced by CalculateSecondaryParameters(), P6DofKinematicState(), and SetVelocityNED().

◆ mVelEast_mps

double P6DofKinematicState::mVelEast_mps

protected

Referenced by CalculateSecondaryParameters(), P6DofKinematicState(), and SetVelocityNED().

◆ mVelNorth_mps

double P6DofKinematicState::mVelNorth_mps

protected

Referenced by CalculateSecondaryParameters(), P6DofKinematicState(), and SetVelocityNED().

◆ mVertSpeed_fpm

double P6DofKinematicState::mVertSpeed_fpm

protected

Referenced by CalculateSecondaryParameters(), GetVerticalSpeed_fpm(), P6DofKinematicState(), SetVerticalSpeed_fpm(), and ZeroKinematicsDuringTesting().

◆ mWcsPitch_rad

double P6DofKinematicState::mWcsPitch_rad

protected

Referenced by CalculateSecondaryParameters(), GetPitchWCS(), P6DofKinematicState(), and SetOrientationWCS().

◆ mWcsRoll_rad

double P6DofKinematicState::mWcsRoll_rad

protected

Referenced by CalculateSecondaryParameters(), GetRollWCS(), P6DofKinematicState(), and SetOrientationWCS().

◆ mWcsYaw_rad

double P6DofKinematicState::mWcsYaw_rad

protected

Referenced by CalculateSecondaryParameters(), GetYawWCS(), P6DofKinematicState(), and SetOrientationWCS().

◆ mWGS84_pos

UtVec3dX P6DofKinematicState::mWGS84_pos

protected

Referenced by CalcBodyVecFromNEDVec(), CalcNEDVecFromInertialVec(), CalculateLLAofRelativePoint(), CalculateSecondaryParameters(), GetLocationWGS(), GetVelocityNED_mps(), P6DofKinematicState(), SetLocationWGS(), and SetVelocityNED().

◆ mWGS84_vel

UtVec3dX P6DofKinematicState::mWGS84_vel

protected

Referenced by CalculateLLAofRelativePoint(), CalculateSecondaryParameters(), GetInertialVelocity(), GetVelocityNED_mps(), GetVelocityWGS(), P6DofKinematicState(), SetVelocityNED(), SetVelocityWGS(), UpdateAeroState(), and ZeroVelocity().

◆ mWgt_lbs

double P6DofKinematicState::mWgt_lbs

protected

Referenced by GetWeight(), P6DofKinematicState(), and SetLiftDragSideForceThrustWeight().

◆ mYawRate_dps

double P6DofKinematicState::mYawRate_dps

protected

Referenced by CalculateSecondaryParameters(), P6DofKinematicState(), and ZeroKinematicsDuringTesting().

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

Public Member Functions

Static Public Member Functions

Protected Attributes

Static Protected Attributes

Constructor & Destructor Documentation

◆ P6DofKinematicState()

Member Function Documentation

◆ CalcBodyVecFromInertialVec()

◆ CalcBodyVecFromNEDVec()

◆ CalcInertialVecFromBodyVec()

◆ CalcInertialVecFromNEDVec()

◆ CalcNEDVecFromBodyVec()

◆ CalcNEDVecFromInertialVec()

◆ CalcRangeSinceStart()

◆ CalculateLLAofRelativePoint()

◆ CalculateRates()

◆ CalculateSecondaryParameters()

◆ GetAirDensity_slugs_per_ft3()

◆ GetAlpha_deg()

◆ GetAlpha_rad()

◆ GetAlphaDot_dps()

◆ GetAlphaDot_rps()

◆ GetAlt_ft()

◆ GetAlt_m()

◆ GetAngleDeltas()

◆ GetApogee_km()

◆ GetAtmospherePtr()

◆ GetBeta_deg()

◆ GetBeta_rad()

◆ GetBetaDot_dps()

◆ GetBetaDot_rps()

◆ GetBodyAeroVectors()

◆ GetCurrentPositionLLA()

◆ GetDCM()

◆ GetDrag()

◆ GetDynamicPressure_psf()

◆ GetFlightPathAngle_deg()

◆ GetFlightPathAngle_rad()

◆ GetInertialAccel()

◆ GetInertialVelocity()

◆ GetLastAltitudeMSL_ft()

◆ GetLastDynamicPressure_psf()

◆ GetLastNx_g()

◆ GetLastNy_g()

◆ GetLastNz_g()

◆ GetLastStaticPressure_psf()

◆ GetLat()

◆ GetLift()

◆ GetLocalHeading_deg()

◆ GetLocalHeading_rad()

◆ GetLocalPitch_deg()

◆ GetLocalPitch_rad()

◆ GetLocalRoll_deg()

◆ GetLocalRoll_rad()

◆ GetLocationSpherical()

◆ GetLocationWGS()

◆ GetLon()

◆ GetMoment()

◆ GetNx_g()

◆ GetNy_g()

◆ GetNz_g()

◆ GetOmegaBody()

◆ GetOmegaBodyDot()

◆ GetOmegaBodyDPS()

◆ GetPitchMoment()

◆ GetPitchRate_dps()

◆ GetPitchRate_rps()

◆ GetPitchWCS()

◆ GetRangeSinceStart_km()

◆ GetRollMoment()

◆ GetRollRate_dps()

◆ GetRollRate_rps()

◆ GetRollWCS()

◆ GetSideForce()

◆ GetSpeed_fps()

◆ GetSpeed_kias()

◆ GetSpeed_ktas()

◆ GetSpeed_Mach()

◆ GetSpeed_mps()

◆ GetStartingLatLon()