WSF
Public Member Functions | Static Public Member Functions | Protected Attributes | List of all members
wsf::six_dof::KinematicState Class Reference

#include <WsfSixDOF_KinematicState.hpp>

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Public Member Functions

 KinematicState (const Environment *aEnvironmentPtr)
void SetTheLastValues ()
void UpdateAeroState (const int64_t aSimTime_nanosec)
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 ()
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_mps () const
double GetSpeed_fps () 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
double GetFlightPathAngle_rad () const
double GetFlightPathAngle_deg () const
double GetBearing_rad () const
double GetBearing_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 SetSpeed_fps (double aSpeed_fps, double aBearing_deg, double aFlightPathAngle_deg)
void SetSpeed_mps (double aSpeed_mps, double aBearing_deg, double aFlightPathAngle_deg)
void SetSpeed_mph (double aSpeed_mph, double aBearing_deg, double aFlightPathAngle_deg)
void SetSpeed_ktas (double aSpeed_ktas, double aBearing_deg, double aFlightPathAngle_deg)
void SetSpeed_kias (double aSpeed_kias, double aBearing_deg, double aFlightPathAngle_deg)
void SetSpeed_Mach (double aSpeed_Mach, double aBearing_deg, double aFlightPathAngle_deg)
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 CalculateSecondaryParameters ()
void CalcRangeSinceStart ()
double GetLastNx_g () const
double GetLastNy_g () const
double GetLastNz_g () const
UtVec3dX CalcNEDVecFromBodyVec (const UtVec3dX &aVecBody) const
UtVec3dX CalcNEDVecFromWCSVec (const UtVec3dX &aVecInertial) const
UtVec3dX CalcWCSVecFromBodyVec (const UtVec3dX &aVecBody) const
UtVec3dX CalcWCSVecFromNEDVec (const UtVec3dX &aVecNED) const
UtVec3dX CalcBodyVecFromNEDVec (const UtVec3dX &aVecNED) const
UtVec3dX CalcBodyVecFromWCSVec (const UtVec3dX &aVecInertial) const
UtVec3dX GetVelocityECI () const
UtVec3dX GetOmegaBody () const
void SetOmegaBody (const UtVec3dX &aOmega)
UtVec3dX GetOmegaBodyDot () const
void SetOmegaBodyDot (const UtVec3dX &aOmegaDot)
UtVec3dX GetLocationWCS () const
void SetLocationWCS (const UtVec3dX &aPosWCS)
UtVec3dX GetVelocityWCS () const
void SetVelocityWCS (const UtVec3dX &aVelWCS)
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 SetAccelerationWCS (const UtVec3dX &aAccelerationWCS)
UtVec3dX GetAccelerationWCS () const
UtEntity & GetUtEntity ()
UtVec3dX NormalizedGravitationalAccelVec () 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 (double aTerrainElevation_m, const KinematicState *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)

Protected Attributes

bool mUseSphericalEarth = false
bool mUseRotatingEarth = false
bool mIgnoreJettisonObjects = false
UtVec3dX mAccelerationWCS
UtDCM mDCM
UtEntity mUtEntity
UtVec3dX mOmega
UtVec3dX mOmegaDot
double mNx_g = 0.0
double mNy_g = 0.0
double mNz_g = 0.0
double mLift_lbs = 0.0
double mThrust_lbs = 0.0
double mDrag_lbs = 0.0
double mSideForce_lbs = 0.0
double mWgt_lbs = 0.0
UtVec3dX mMoment_ftlbs
double mRho_slugs_per_ft3 = 0.0
double mDynamicPressure_psf = 0.0
double mStaticPressure_psf = 0.0
double mRadarAlt_m = 0.0
double mAlpha_deg = 0.0
double mBeta_deg = 0.0
double mAlphaDot_dps = 0.0
double mBetaDot_dps = 0.0
double mYawRate_dps = 0.0
double mPitchRate_dps = 0.0
double mRollRate_dps = 0.0
double mApogee_km = 0.0
double mRangeSinceStart_km = 0.0
double mStartingLat = 0.0
double mStartingLon = 0.0
bool mStartingLocationInitialized = false
double mLastNx = 0.0
double mLastNy = 0.0
double mLastNz = 0.0
double mLastDynamicPressure_psf = 0.0
double mLastStaticPressure_psf = 0.0
double mLastAlt_m = 0.0
const Environment * mEnvironment = nullptr
double mDeltaYaw_rad = 0.0
double mDeltaPitch_rad = 0.0
double mDeltaRoll_rad = 0.0
int64_t mLastUpdate_nanosec = -1
double mLastAlpha_deg = 0.0
double mLastBeta_deg = 0.0

Constructor & Destructor Documentation

◆ KinematicState()

wsf::six_dof::KinematicState::KinematicState ( const Environment * aEnvironmentPtr)
explicit

References mEnvironment.

Referenced by CalculateLLAofRelativePoint().

Member Function Documentation

◆ CalcBodyVecFromNEDVec()

UtVec3dX wsf::six_dof::KinematicState::CalcBodyVecFromNEDVec ( const UtVec3dX & aVecNED) const

References mUtEntity.

◆ CalcBodyVecFromWCSVec()

UtVec3dX wsf::six_dof::KinematicState::CalcBodyVecFromWCSVec ( const UtVec3dX & aVecInertial) const

References mDCM.

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration(), and wsf::six_dof::RigidBodyIntegrator::CalculateFM().

◆ CalcNEDVecFromBodyVec()

UtVec3dX wsf::six_dof::KinematicState::CalcNEDVecFromBodyVec ( const UtVec3dX & aVecBody) const

References CalcNEDVecFromWCSVec(), and CalcWCSVecFromBodyVec().

Referenced by CalculateLLAofRelativePoint().

◆ CalcNEDVecFromWCSVec()

UtVec3dX wsf::six_dof::KinematicState::CalcNEDVecFromWCSVec ( const UtVec3dX & aVecInertial) const

References mUtEntity.

Referenced by CalcNEDVecFromBodyVec(), and CalculateLLAofRelativePoint().

◆ CalcRangeSinceStart()

void wsf::six_dof::KinematicState::CalcRangeSinceStart ( )

References GetLat(), GetLon(), mRangeSinceStart_km, mStartingLat, mStartingLon, and mUtEntity.

Referenced by CalculateSecondaryParameters().

◆ CalculateLLAofRelativePoint()

bool wsf::six_dof::KinematicState::CalculateLLAofRelativePoint ( double aTerrainElevation_m,
const KinematicState * 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(), CalcNEDVecFromWCSVec(), GetLocationWCS(), GetVelocityWCS(), KinematicState(), mDCM, and mOmega.

Referenced by wsf::six_dof::RigidBodyGroundReactionPoint::CalcFrictionForceMoment(), wsf::six_dof::RigidBodyGroundReactionPoint::CalcGroundReactionForceMoment(), wsf::six_dof::RigidBodyGroundReactionPoint::CalcMaxFrictionForceMagnitude_lbs(), and wsf::six_dof::RigidBodyGroundReactionPoint::CalcNormalForceMoment().

◆ CalculateSecondaryParameters()

void wsf::six_dof::KinematicState::CalculateSecondaryParameters ( )

References wsf::six_dof::utils::AlphaBetaFromInertialVel(), CalcRangeSinceStart(), GetAlt_ft(), GetAlt_m(), GetSpeed_fps(), GetVelocityWCS(), mAlpha_deg, mApogee_km, mBeta_deg, mDCM, mDynamicPressure_psf, mEnvironment, mOmega, mPitchRate_dps, mRadarAlt_m, mRho_slugs_per_ft3, mRollRate_dps, mStaticPressure_psf, mUtEntity, and mYawRate_dps.

Referenced by RemoveAlphaForTesting(), wsf::six_dof::Mover::SeparateSubObject(), wsf::six_dof::PointMassIntegrator::Update(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ CalcWCSVecFromBodyVec()

UtVec3dX wsf::six_dof::KinematicState::CalcWCSVecFromBodyVec ( const UtVec3dX & aVecBody) const

References mDCM.

Referenced by CalcNEDVecFromBodyVec(), wsf::six_dof::RigidBodyIntegrator::CalculateFM(), and wsf::six_dof::Integrator::PropagateTranslation().

◆ CalcWCSVecFromNEDVec()

UtVec3dX wsf::six_dof::KinematicState::CalcWCSVecFromNEDVec ( const UtVec3dX & aVecNED) const

References mUtEntity.

◆ GetAccelerationWCS()

UtVec3dX wsf::six_dof::KinematicState::GetAccelerationWCS ( ) const
inline

References mAccelerationWCS.

Referenced by wsf::six_dof::Integrator::PropagateTranslation().

◆ GetAirDensity_slugs_per_ft3()

double wsf::six_dof::KinematicState::GetAirDensity_slugs_per_ft3 ( ) const
inline

References mRho_slugs_per_ft3.

◆ GetAlpha_deg()

double wsf::six_dof::KinematicState::GetAlpha_deg ( ) const

References mAlpha_deg.

Referenced by wsf::six_dof::PointMassMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::RigidBodyMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::PointMassMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::PointMassMover::GetCurrentThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentThrust_lbs(), wsf::six_dof::PointMassMover::UpdatePropulsionFuelBurn(), and wsf::six_dof::RigidBodyMover::UpdatePropulsionFuelBurn().

◆ GetAlpha_rad()

double wsf::six_dof::KinematicState::GetAlpha_rad ( ) const

References mAlpha_deg.

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration(), and RemoveAlphaForTesting().

◆ GetAlphaDot_dps()

double wsf::six_dof::KinematicState::GetAlphaDot_dps ( ) const

References mAlphaDot_dps.

◆ GetAlphaDot_rps()

double wsf::six_dof::KinematicState::GetAlphaDot_rps ( ) const

References mAlphaDot_dps.

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration().

◆ GetAlt_ft()

double wsf::six_dof::KinematicState::GetAlt_ft ( ) const

References GetAlt_m().

Referenced by CalculateSecondaryParameters(), wsf::six_dof::PointMassMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::RigidBodyMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::PilotObject::CreateTempActionIfNeeded(), wsf::six_dof::PointMassMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::PointMassMover::GetCurrentThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentThrust_lbs(), wsf::six_dof::PilotObject::SetTempActionToHoldCurrentConditions(), UpdateAeroState(), wsf::six_dof::PointMassMover::UpdatePropulsionFuelBurn(), and wsf::six_dof::RigidBodyMover::UpdatePropulsionFuelBurn().

◆ GetAlt_m()

double wsf::six_dof::KinematicState::GetAlt_m ( ) const

References mUtEntity.

Referenced by CalculateSecondaryParameters(), wsf::six_dof::PilotObject::FlyAtPoint(), GetAlt_ft(), GetSpeed_kias(), GetSpeed_Mach(), NormalizedGravitationalAccelVec(), wsf::six_dof::Integrator::PropagateTranslation(), wsf::six_dof::PilotObject::ReturnToPlannedWaypoints(), wsf::six_dof::PilotObject::SetPlannedWaypointIndex(), SetSpeed_kias(), SetSpeed_Mach(), wsf::six_dof::PilotObject::SetTempWaypointIndex(), SetTheLastValues(), and UpdateAeroState().

◆ GetAngleDeltas()

void wsf::six_dof::KinematicState::GetAngleDeltas ( double & aDeltaYaw_rad,
double & aDeltaPitch_rad,
double & aDeltaRoll_rad ) const

References mDeltaPitch_rad, mDeltaRoll_rad, and mDeltaYaw_rad.

◆ GetApogee_km()

double wsf::six_dof::KinematicState::GetApogee_km ( ) const
inline

References mApogee_km.

◆ GetBearing_deg()

double wsf::six_dof::KinematicState::GetBearing_deg ( ) const
inline

References GetBearing_rad().

Referenced by wsf::six_dof::PilotObject::SetPlannedRoute().

◆ GetBearing_rad()

double wsf::six_dof::KinematicState::GetBearing_rad ( ) const

References mUtEntity.

Referenced by GetBearing_deg().

◆ GetBeta_deg()

double wsf::six_dof::KinematicState::GetBeta_deg ( ) const

References mBeta_deg.

Referenced by wsf::six_dof::PointMassMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::RigidBodyMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::PointMassMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::PointMassMover::GetCurrentThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentThrust_lbs(), wsf::six_dof::PointMassMover::UpdatePropulsionFuelBurn(), and wsf::six_dof::RigidBodyMover::UpdatePropulsionFuelBurn().

◆ GetBeta_rad()

double wsf::six_dof::KinematicState::GetBeta_rad ( ) const

References mBeta_deg.

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration(), and wsf::six_dof::RigidBodyIntegrator::PropagateRotation().

◆ GetBetaDot_dps()

double wsf::six_dof::KinematicState::GetBetaDot_dps ( ) const

References mBetaDot_dps.

◆ GetBetaDot_rps()

double wsf::six_dof::KinematicState::GetBetaDot_rps ( ) const

References mBetaDot_dps.

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration().

◆ GetBodyAeroVectors()

void wsf::six_dof::KinematicState::GetBodyAeroVectors ( const UtDCM & aDCM,
const UtVec3dX & aInertialVelVector,
UtVec3dX & aLiftBodyVector,
UtVec3dX & aDragBodyVector,
UtVec3dX & aSideForceBodyVector ) const

◆ GetCurrentPositionLLA()

UtLLAPos wsf::six_dof::KinematicState::GetCurrentPositionLLA ( ) const

References mUtEntity.

Referenced by wsf::six_dof::RigidBodyCommonController::GetAimHeadingAndTurnRateForTaxiWaypointNav_deg(), wsf::six_dof::CommonController::GetAimHeadingForWaypointNav_deg(), and wsf::six_dof::Integrator::PropagateTranslation().

◆ GetDCM()

UtDCM wsf::six_dof::KinematicState::GetDCM ( ) const
inline

References mDCM.

Referenced by wsf::six_dof::Integrator::PropagateRotation().

◆ GetDrag()

double wsf::six_dof::KinematicState::GetDrag ( ) const
inline

References mDrag_lbs.

Referenced by wsf::six_dof::PointMassIntegrator::Update(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ GetDynamicPressure_psf()

double wsf::six_dof::KinematicState::GetDynamicPressure_psf ( ) const
inline

References mDynamicPressure_psf.

Referenced by wsf::six_dof::PointMassMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::RigidBodyMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::PointMassMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::PointMassMover::GetCurrentThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentThrust_lbs(), wsf::six_dof::PointMassMover::UpdatePropulsionFuelBurn(), and wsf::six_dof::RigidBodyMover::UpdatePropulsionFuelBurn().

◆ GetFlightPathAngle_deg()

double wsf::six_dof::KinematicState::GetFlightPathAngle_deg ( ) const
inline

References GetFlightPathAngle_rad().

Referenced by wsf::six_dof::PilotObject::SetPlannedRoute().

◆ GetFlightPathAngle_rad()

double wsf::six_dof::KinematicState::GetFlightPathAngle_rad ( ) const

References mUtEntity.

Referenced by GetFlightPathAngle_deg().

◆ GetLastAltitudeMSL_ft()

double wsf::six_dof::KinematicState::GetLastAltitudeMSL_ft ( ) const

References mLastAlt_m.

◆ GetLastDynamicPressure_psf()

double wsf::six_dof::KinematicState::GetLastDynamicPressure_psf ( ) const

References mLastDynamicPressure_psf.

◆ GetLastNx_g()

double wsf::six_dof::KinematicState::GetLastNx_g ( ) const

References mLastNx.

◆ GetLastNy_g()

double wsf::six_dof::KinematicState::GetLastNy_g ( ) const

References mLastNy.

◆ GetLastNz_g()

double wsf::six_dof::KinematicState::GetLastNz_g ( ) const

References mLastNz.

◆ GetLastStaticPressure_psf()

double wsf::six_dof::KinematicState::GetLastStaticPressure_psf ( ) const

References mLastStaticPressure_psf.

◆ GetLat()

double wsf::six_dof::KinematicState::GetLat ( ) const

References mUtEntity.

Referenced by CalcRangeSinceStart(), wsf::six_dof::PilotObject::FlyAtPoint(), wsf::six_dof::PilotObject::ReturnToPlannedWaypoints(), SetAlt(), wsf::six_dof::PilotObject::SetPlannedWaypointIndex(), wsf::six_dof::PilotObject::SetTempWaypointIndex(), and UpdateAeroState().

◆ GetLift()

double wsf::six_dof::KinematicState::GetLift ( ) const
inline

References mLift_lbs.

Referenced by wsf::six_dof::PointMassIntegrator::Update(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ GetLocalHeading_deg()

double wsf::six_dof::KinematicState::GetLocalHeading_deg ( ) const
inline

References GetLocalHeading_rad().

Referenced by wsf::six_dof::CommonController::CalcLateralNavMode_RollHeadingCore().

◆ GetLocalHeading_rad()

double wsf::six_dof::KinematicState::GetLocalHeading_rad ( ) const

References mUtEntity.

Referenced by wsf::six_dof::PilotObject::CreateTempActionIfNeeded(), wsf::six_dof::RigidBodyCommonController::GetAimHeadingAndTurnRateForTaxiWaypointNav_deg(), wsf::six_dof::CommonController::GetAimHeadingForWaypointNav_deg(), GetLocalHeading_deg(), and wsf::six_dof::PilotObject::SetTempActionToHoldCurrentConditions().

◆ GetLocalPitch_deg()

double wsf::six_dof::KinematicState::GetLocalPitch_deg ( ) const
inline

References GetLocalPitch_rad().

Referenced by wsf::six_dof::CommonController::CalcLateralNavMode_RollHeadingCore().

◆ GetLocalPitch_rad()

double wsf::six_dof::KinematicState::GetLocalPitch_rad ( ) const

References mUtEntity.

Referenced by GetLocalPitch_deg().

◆ GetLocalRoll_deg()

double wsf::six_dof::KinematicState::GetLocalRoll_deg ( ) const
inline

References GetLocalRoll_rad().

◆ GetLocalRoll_rad()

double wsf::six_dof::KinematicState::GetLocalRoll_rad ( ) const

References mUtEntity.

Referenced by GetLocalRoll_deg().

◆ GetLocationWCS()

UtVec3dX wsf::six_dof::KinematicState::GetLocationWCS ( ) const
inline

References mUtEntity, and pos.

Referenced by CalculateLLAofRelativePoint(), NormalizedGravitationalAccelVec(), and wsf::six_dof::Integrator::PropagateTranslation().

◆ GetLon()

double wsf::six_dof::KinematicState::GetLon ( ) const

References mUtEntity.

Referenced by CalcRangeSinceStart(), wsf::six_dof::PilotObject::FlyAtPoint(), wsf::six_dof::PilotObject::ReturnToPlannedWaypoints(), SetAlt(), wsf::six_dof::PilotObject::SetPlannedWaypointIndex(), wsf::six_dof::PilotObject::SetTempWaypointIndex(), and UpdateAeroState().

◆ GetMoment()

UtVec3dX wsf::six_dof::KinematicState::GetMoment ( ) const
inline

References mMoment_ftlbs.

Referenced by wsf::six_dof::RigidBodyIntegrator::Update().

◆ GetNx_g()

double wsf::six_dof::KinematicState::GetNx_g ( ) const

References mNx_g.

◆ GetNy_g()

double wsf::six_dof::KinematicState::GetNy_g ( ) const

References mNy_g.

◆ GetNz_g()

double wsf::six_dof::KinematicState::GetNz_g ( ) const

References mNz_g.

◆ GetOmegaBody()

UtVec3dX wsf::six_dof::KinematicState::GetOmegaBody ( ) const
inline

References mOmega.

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration(), wsf::six_dof::Integrator::PropagateRotation(), and wsf::six_dof::RigidBodyIntegrator::PropagateRotation().

◆ GetOmegaBodyDot()

UtVec3dX wsf::six_dof::KinematicState::GetOmegaBodyDot ( ) const
inline

References mOmegaDot.

Referenced by wsf::six_dof::utils::CanFlyAt(), wsf::six_dof::utils::CanFlyAt(), and wsf::six_dof::Integrator::PropagateRotation().

◆ GetOmegaBodyDPS()

UtVec3dX wsf::six_dof::KinematicState::GetOmegaBodyDPS ( ) const

References mOmega.

◆ GetPitchMoment()

double wsf::six_dof::KinematicState::GetPitchMoment ( ) const
inline

References mMoment_ftlbs.

◆ GetPitchRate_dps()

double wsf::six_dof::KinematicState::GetPitchRate_dps ( ) const

References mOmega.

◆ GetPitchRate_rps()

double wsf::six_dof::KinematicState::GetPitchRate_rps ( ) const

References mOmega.

◆ GetPitchWCS()

double wsf::six_dof::KinematicState::GetPitchWCS ( ) const
inline

References mUtEntity.

◆ GetRangeSinceStart_km()

double wsf::six_dof::KinematicState::GetRangeSinceStart_km ( ) const
inline

References mRangeSinceStart_km.

◆ GetRollMoment()

double wsf::six_dof::KinematicState::GetRollMoment ( ) const
inline

References mMoment_ftlbs.

◆ GetRollRate_dps()

double wsf::six_dof::KinematicState::GetRollRate_dps ( ) const

References mOmega.

◆ GetRollRate_rps()

double wsf::six_dof::KinematicState::GetRollRate_rps ( ) const

References mOmega.

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration().

◆ GetRollWCS()

double wsf::six_dof::KinematicState::GetRollWCS ( ) const
inline

References mUtEntity.

◆ GetSideForce()

double wsf::six_dof::KinematicState::GetSideForce ( ) const
inline

References mSideForce_lbs.

Referenced by wsf::six_dof::PointMassIntegrator::Update(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ GetSpeed_fps()

double wsf::six_dof::KinematicState::GetSpeed_fps ( ) const

References GetSpeed_mps().

Referenced by wsf::six_dof::CommonController::CalcLateralNavMode_RollHeadingCore(), CalculateSecondaryParameters(), wsf::six_dof::PointMassMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::RigidBodyMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::CommonController::GetAimHeadingForWaypointNav_deg(), wsf::six_dof::PointMassMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::PointMassMover::GetCurrentThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentThrust_lbs(), GetSpeed_kias(), GetSpeed_ktas(), GetSpeed_Mach(), wsf::six_dof::RigidBodyCommonController::ProcessStandardLateralNavMode_TaxiYawRate(), wsf::six_dof::PointMassMover::UpdatePropulsionFuelBurn(), and wsf::six_dof::RigidBodyMover::UpdatePropulsionFuelBurn().

◆ GetSpeed_kias()

double wsf::six_dof::KinematicState::GetSpeed_kias ( ) const

References GetAlt_m(), GetSpeed_fps(), and mEnvironment.

◆ GetSpeed_ktas()

double wsf::six_dof::KinematicState::GetSpeed_ktas ( ) const

References GetSpeed_fps(), and mEnvironment.

Referenced by wsf::six_dof::PilotObject::CreateTempActionIfNeeded(), wsf::six_dof::PilotObject::FlyAtPoint(), wsf::six_dof::PilotObject::SetPlannedRoute(), and wsf::six_dof::PilotObject::SetTempActionToHoldCurrentConditions().

◆ GetSpeed_Mach()

double wsf::six_dof::KinematicState::GetSpeed_Mach ( ) const

References GetAlt_m(), GetSpeed_fps(), and mEnvironment.

Referenced by wsf::six_dof::PointMassMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::RigidBodyMover::CalculateThrustVectorAndMomentUpdatePropulsion(), wsf::six_dof::PointMassMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentForwardThrust_lbs(), wsf::six_dof::PointMassMover::GetCurrentThrust_lbs(), wsf::six_dof::RigidBodyMover::GetCurrentThrust_lbs(), wsf::six_dof::PointMassMover::UpdatePropulsionFuelBurn(), and wsf::six_dof::RigidBodyMover::UpdatePropulsionFuelBurn().

◆ GetSpeed_mps()

double wsf::six_dof::KinematicState::GetSpeed_mps ( ) const

References GetVelocityWCS().

Referenced by wsf::six_dof::RigidBodyCommonController::GetAimHeadingAndTurnRateForTaxiWaypointNav_deg(), wsf::six_dof::CommonController::GetAimHeadingForWaypointNav_deg(), and GetSpeed_fps().

◆ GetStartingLatLon()

void wsf::six_dof::KinematicState::GetStartingLatLon ( double & aLat,
double & aLon ) const

References mStartingLat, and mStartingLon.

◆ GetStaticPressure_psf()

double wsf::six_dof::KinematicState::GetStaticPressure_psf ( ) const
inline

References mStaticPressure_psf.

◆ GetThrust()

double wsf::six_dof::KinematicState::GetThrust ( ) const
inline

References mThrust_lbs.

Referenced by wsf::six_dof::PointMassIntegrator::Update(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ GetUtEntity()

UtEntity & wsf::six_dof::KinematicState::GetUtEntity ( )
inline

References mUtEntity.

Referenced by wsf::six_dof::Integrator::PropagateTranslation().

◆ GetVelocityECI()

UtVec3dX wsf::six_dof::KinematicState::GetVelocityECI ( ) const
inline

References mUtEntity, and vel.

◆ GetVelocityNED_mps()

UtVec3dX wsf::six_dof::KinematicState::GetVelocityNED_mps ( ) const

References mUtEntity.

Referenced by wsf::six_dof::Integrator::PropagateTranslation().

◆ GetVelocityWCS()

UtVec3dX wsf::six_dof::KinematicState::GetVelocityWCS ( ) const
inline

References mUtEntity, and vel.

Referenced by CalculateLLAofRelativePoint(), and wsf::six_dof::Integrator::PropagateTranslation().

◆ GetVerticalSpeed_fpm()

double wsf::six_dof::KinematicState::GetVerticalSpeed_fpm ( ) const
inline

References mUtEntity.

◆ GetWeight()

double wsf::six_dof::KinematicState::GetWeight ( ) const
inline

References mWgt_lbs.

Referenced by wsf::six_dof::PointMassIntegrator::Update(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ GetYawMoment()

double wsf::six_dof::KinematicState::GetYawMoment ( ) const
inline

References mMoment_ftlbs.

◆ GetYawRate_dps()

double wsf::six_dof::KinematicState::GetYawRate_dps ( ) const

References mOmega.

Referenced by wsf::six_dof::RigidBodyCommonController::ProcessStandardLateralNavMode_TaxiYawRate().

◆ GetYawRate_rps()

double wsf::six_dof::KinematicState::GetYawRate_rps ( ) const

References mOmega.

◆ GetYawWCS()

double wsf::six_dof::KinematicState::GetYawWCS ( ) const
inline

References mUtEntity.

◆ IgnoreJettisonObjects()

bool wsf::six_dof::KinematicState::IgnoreJettisonObjects ( ) const
inline

References mIgnoreJettisonObjects.

◆ NormalizedGravitationalAccelVec()

UtVec3dX wsf::six_dof::KinematicState::NormalizedGravitationalAccelVec ( ) const

References GetAlt_m(), GetLocationWCS(), and mUtEntity.

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration(), and wsf::six_dof::RigidBodyIntegrator::CalculateFM().

◆ RemoveAlphaForTesting()

void wsf::six_dof::KinematicState::RemoveAlphaForTesting ( )

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

Referenced by wsf::six_dof::PointMassIntegrator::Update(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ SetAccelerationWCS()

void wsf::six_dof::KinematicState::SetAccelerationWCS ( const UtVec3dX & aAccelerationWCS)
inline

References mAccelerationWCS.

Referenced by wsf::six_dof::Integrator::PropagateTranslation().

◆ SetAlphaBetaDotToZero()

void wsf::six_dof::KinematicState::SetAlphaBetaDotToZero ( )

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

◆ SetAlt()

void wsf::six_dof::KinematicState::SetAlt ( double aAlt_m)
inline

References GetLat(), GetLon(), and mUtEntity.

Referenced by wsf::six_dof::Integrator::PropagateTranslation().

◆ SetAngleDeltas()

void wsf::six_dof::KinematicState::SetAngleDeltas ( double aDeltaYaw_rad,
double aDeltaPitch_rad,
double aDeltaRoll_rad )

References mDeltaPitch_rad, mDeltaRoll_rad, and mDeltaYaw_rad.

Referenced by wsf::six_dof::Integrator::PropagateRotation().

◆ SetAttitude_rad()

void wsf::six_dof::KinematicState::SetAttitude_rad ( double aHeading_rad,
double aPitch_rad,
double aRoll_rad )

References mUtEntity.

Referenced by wsf::six_dof::PilotObject::SetPlannedRoute().

◆ SetBodyAccel()

void wsf::six_dof::KinematicState::SetBodyAccel ( double aNx_g,
double aNy_g,
double aNz_g )

References mNx_g, mNy_g, and mNz_g.

Referenced by wsf::six_dof::PointMassIntegrator::PropagateUsingAcceleration(), and wsf::six_dof::RigidBodyIntegrator::PropagateUsingFM().

◆ SetDCM()

void wsf::six_dof::KinematicState::SetDCM ( const UtDCM & aDCM)
inline

References mDCM.

Referenced by wsf::six_dof::Integrator::PropagateRotation().

◆ SetIgnoreJettisonObjects()

void wsf::six_dof::KinematicState::SetIgnoreJettisonObjects ( bool aValue)
inline

References mIgnoreJettisonObjects.

◆ SetLastUpdateTime()

void wsf::six_dof::KinematicState::SetLastUpdateTime ( int64_t aLastUpdate_nanosec)
inline

References mLastUpdate_nanosec.

◆ SetLiftDragSideForceThrustWeight()

void wsf::six_dof::KinematicState::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 wsf::six_dof::PointMassIntegrator::CalculateAcceleration(), wsf::six_dof::RigidBodyIntegrator::CalculateFM(), wsf::six_dof::PointMassIntegrator::Update(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ SetLocationWCS()

void wsf::six_dof::KinematicState::SetLocationWCS ( const UtVec3dX & aPosWCS)
inline

References mUtEntity.

Referenced by wsf::six_dof::Integrator::PropagateTranslation().

◆ SetMomentAtCG()

void wsf::six_dof::KinematicState::SetMomentAtCG ( UtVec3dX aMoment_ftlbs)

References mMoment_ftlbs.

Referenced by wsf::six_dof::RigidBodyIntegrator::CalculateFM(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ SetOmegaBody()

void wsf::six_dof::KinematicState::SetOmegaBody ( const UtVec3dX & aOmega)
inline

References mOmega.

Referenced by wsf::six_dof::Integrator::PropagateRotation(), and wsf::six_dof::RigidBodyIntegrator::PropagateRotation().

◆ SetOmegaBodyDot()

void wsf::six_dof::KinematicState::SetOmegaBodyDot ( const UtVec3dX & aOmegaDot)
inline

References mOmegaDot.

Referenced by wsf::six_dof::Integrator::PropagateRotation().

◆ SetOrientationWCS()

void wsf::six_dof::KinematicState::SetOrientationWCS ( double aYaw_rad,
double aPitch_rad,
double aRoll_rad )

References mUtEntity.

◆ SetPitchRate()

void wsf::six_dof::KinematicState::SetPitchRate ( double aPitchRate_dps)

References mOmega.

Referenced by wsf::six_dof::Integrator::PropagateRotation().

◆ SetPositionLLA()

void wsf::six_dof::KinematicState::SetPositionLLA ( double aLat,
double aLon,
double aAlt_m )

References mUtEntity.

Referenced by wsf::six_dof::Integrator::PropagateTranslation(), and wsf::six_dof::PilotObject::SetPlannedRoute().

◆ SetRollRate()

void wsf::six_dof::KinematicState::SetRollRate ( double aRollRate_dps)

References mOmega.

Referenced by wsf::six_dof::Integrator::PropagateRotation().

◆ SetSpeed_fps()

void wsf::six_dof::KinematicState::SetSpeed_fps ( double aSpeed_fps,
double aBearing_deg,
double aFlightPathAngle_deg )

References SetSpeed_mps().

Referenced by wsf::six_dof::PilotObject::SetPlannedRoute(), SetSpeed_kias(), SetSpeed_ktas(), and SetSpeed_Mach().

◆ SetSpeed_kias()

void wsf::six_dof::KinematicState::SetSpeed_kias ( double aSpeed_kias,
double aBearing_deg,
double aFlightPathAngle_deg )

References GetAlt_m(), mEnvironment, and SetSpeed_fps().

Referenced by wsf::six_dof::PilotObject::SetPlannedRoute().

◆ SetSpeed_ktas()

void wsf::six_dof::KinematicState::SetSpeed_ktas ( double aSpeed_ktas,
double aBearing_deg,
double aFlightPathAngle_deg )

References mEnvironment, and SetSpeed_fps().

Referenced by wsf::six_dof::PilotObject::SetPlannedRoute().

◆ SetSpeed_Mach()

void wsf::six_dof::KinematicState::SetSpeed_Mach ( double aSpeed_Mach,
double aBearing_deg,
double aFlightPathAngle_deg )

References GetAlt_m(), mEnvironment, and SetSpeed_fps().

Referenced by wsf::six_dof::PilotObject::SetPlannedRoute().

◆ SetSpeed_mph()

void wsf::six_dof::KinematicState::SetSpeed_mph ( double aSpeed_mph,
double aBearing_deg,
double aFlightPathAngle_deg )

References SetSpeed_mps().

Referenced by wsf::six_dof::PilotObject::SetPlannedRoute().

◆ SetSpeed_mps()

void wsf::six_dof::KinematicState::SetSpeed_mps ( double aSpeed_mps,
double aBearing_deg,
double aFlightPathAngle_deg )

References mUtEntity.

Referenced by wsf::six_dof::PilotObject::SetPlannedRoute(), SetSpeed_fps(), and SetSpeed_mph().

◆ SetStartingLatLon()

void wsf::six_dof::KinematicState::SetStartingLatLon ( double aLat,
double aLon )

References mStartingLat, mStartingLocationInitialized, and mStartingLon.

◆ SetTheLastValues()

void wsf::six_dof::KinematicState::SetTheLastValues ( )

References GetAlt_m(), mDynamicPressure_psf, mLastAlt_m, mLastDynamicPressure_psf, mLastNx, mLastNy, mLastNz, mLastStaticPressure_psf, mNx_g, mNy_g, mNz_g, and mStaticPressure_psf.

◆ SetUseRotatingEarth()

void wsf::six_dof::KinematicState::SetUseRotatingEarth ( bool aValue)
inline

References mUseRotatingEarth.

◆ SetUseSphericalEarth()

void wsf::six_dof::KinematicState::SetUseSphericalEarth ( bool aValue)

References mUseSphericalEarth, and mUtEntity.

◆ SetVelocityNED()

void wsf::six_dof::KinematicState::SetVelocityNED ( double aVelNorth_mps,
double aVelEast_mps,
double aVelDown_mps )

References mUtEntity.

Referenced by wsf::six_dof::Integrator::PropagateTranslation().

◆ SetVelocityWCS()

void wsf::six_dof::KinematicState::SetVelocityWCS ( const UtVec3dX & aVelWCS)
inline

References mUtEntity.

Referenced by wsf::six_dof::Integrator::PropagateTranslation(), and ZeroVelocity().

◆ SetYawRate()

void wsf::six_dof::KinematicState::SetYawRate ( double aYawRate_dps)

References mOmega.

Referenced by wsf::six_dof::Integrator::PropagateRotation().

◆ StartingLocationInitialized()

bool wsf::six_dof::KinematicState::StartingLocationInitialized ( ) const
inline

References mStartingLocationInitialized.

◆ UpdateAeroState()

void wsf::six_dof::KinematicState::UpdateAeroState ( const int64_t aSimTime_nanosec)

References wsf::six_dof::utils::AlphaBetaFromInertialVel(), wsf::six_dof::utils::cEPSILON_SIMTIME_NANOSEC, GetAlt_ft(), GetAlt_m(), GetLat(), GetLon(), GetVelocityWCS(), mAlpha_deg, mAlphaDot_dps, mBeta_deg, mBetaDot_dps, mDCM, mDynamicPressure_psf, mEnvironment, mLastAlpha_deg, mLastBeta_deg, mLastUpdate_nanosec, mRho_slugs_per_ft3, mStaticPressure_psf, mUtEntity, and wsf::six_dof::utils::TimeToTime().

Referenced by wsf::six_dof::PointMassIntegrator::CalculateAcceleration(), wsf::six_dof::RigidBodyIntegrator::CalculateFM(), wsf::six_dof::PointMassIntegrator::Update(), and wsf::six_dof::RigidBodyIntegrator::Update().

◆ UseRotatingEarth()

bool wsf::six_dof::KinematicState::UseRotatingEarth ( ) const
inline

References mUseRotatingEarth.

Referenced by wsf::six_dof::Integrator::PropagateTranslation().

◆ UseSphericalEarth()

bool wsf::six_dof::KinematicState::UseSphericalEarth ( ) const
inline

References mUseSphericalEarth.

◆ ZeroKinematicsDuringTesting()

void wsf::six_dof::KinematicState::ZeroKinematicsDuringTesting ( )

References mAccelerationWCS, mAlpha_deg, mAlphaDot_dps, mBeta_deg, mBetaDot_dps, mDeltaPitch_rad, mDeltaRoll_rad, mDeltaYaw_rad, mDrag_lbs, mLastAlpha_deg, mLastBeta_deg, mLastNx, mLastNy, mLastNz, mLift_lbs, mMoment_ftlbs, mNx_g, mNy_g, mNz_g, mOmega, mOmegaDot, mPitchRate_dps, mRollRate_dps, mSideForce_lbs, mThrust_lbs, mYawRate_dps, and ZeroVelocity().

◆ ZeroVelocity()

void wsf::six_dof::KinematicState::ZeroVelocity ( )

References SetVelocityWCS().

Referenced by ZeroKinematicsDuringTesting().

Member Data Documentation

◆ mAccelerationWCS

UtVec3dX wsf::six_dof::KinematicState::mAccelerationWCS
protected

Referenced by GetAccelerationWCS(), SetAccelerationWCS(), and ZeroKinematicsDuringTesting().

◆ mAlpha_deg

double wsf::six_dof::KinematicState::mAlpha_deg = 0.0
protected

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

◆ mAlphaDot_dps

double wsf::six_dof::KinematicState::mAlphaDot_dps = 0.0
protected

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

◆ mApogee_km

double wsf::six_dof::KinematicState::mApogee_km = 0.0
protected

Referenced by CalculateSecondaryParameters(), and GetApogee_km().

◆ mBeta_deg

double wsf::six_dof::KinematicState::mBeta_deg = 0.0
protected

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

◆ mBetaDot_dps

double wsf::six_dof::KinematicState::mBetaDot_dps = 0.0
protected

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

◆ mDCM

UtDCM wsf::six_dof::KinematicState::mDCM
protected

Referenced by CalcBodyVecFromWCSVec(), CalculateLLAofRelativePoint(), CalculateSecondaryParameters(), CalcWCSVecFromBodyVec(), GetDCM(), RemoveAlphaForTesting(), SetDCM(), and UpdateAeroState().

◆ mDeltaPitch_rad

double wsf::six_dof::KinematicState::mDeltaPitch_rad = 0.0
protected

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

◆ mDeltaRoll_rad

double wsf::six_dof::KinematicState::mDeltaRoll_rad = 0.0
protected

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

◆ mDeltaYaw_rad

double wsf::six_dof::KinematicState::mDeltaYaw_rad = 0.0
protected

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

◆ mDrag_lbs

double wsf::six_dof::KinematicState::mDrag_lbs = 0.0
protected

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

◆ mDynamicPressure_psf

double wsf::six_dof::KinematicState::mDynamicPressure_psf = 0.0
protected

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

◆ mEnvironment

const Environment* wsf::six_dof::KinematicState::mEnvironment = nullptr
protected

Referenced by CalculateSecondaryParameters(), GetSpeed_kias(), GetSpeed_ktas(), GetSpeed_Mach(), KinematicState(), SetSpeed_kias(), SetSpeed_ktas(), SetSpeed_Mach(), and UpdateAeroState().

◆ mIgnoreJettisonObjects

bool wsf::six_dof::KinematicState::mIgnoreJettisonObjects = false
protected

Referenced by IgnoreJettisonObjects(), and SetIgnoreJettisonObjects().

◆ mLastAlpha_deg

double wsf::six_dof::KinematicState::mLastAlpha_deg = 0.0
protected

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

◆ mLastAlt_m

double wsf::six_dof::KinematicState::mLastAlt_m = 0.0
protected

Referenced by GetLastAltitudeMSL_ft(), and SetTheLastValues().

◆ mLastBeta_deg

double wsf::six_dof::KinematicState::mLastBeta_deg = 0.0
protected

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

◆ mLastDynamicPressure_psf

double wsf::six_dof::KinematicState::mLastDynamicPressure_psf = 0.0
protected

Referenced by GetLastDynamicPressure_psf(), and SetTheLastValues().

◆ mLastNx

double wsf::six_dof::KinematicState::mLastNx = 0.0
protected

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

◆ mLastNy

double wsf::six_dof::KinematicState::mLastNy = 0.0
protected

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

◆ mLastNz

double wsf::six_dof::KinematicState::mLastNz = 0.0
protected

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

◆ mLastStaticPressure_psf

double wsf::six_dof::KinematicState::mLastStaticPressure_psf = 0.0
protected

Referenced by GetLastStaticPressure_psf(), and SetTheLastValues().

◆ mLastUpdate_nanosec

int64_t wsf::six_dof::KinematicState::mLastUpdate_nanosec = -1
protected

Referenced by SetLastUpdateTime(), and UpdateAeroState().

◆ mLift_lbs

double wsf::six_dof::KinematicState::mLift_lbs = 0.0
protected

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

◆ mMoment_ftlbs

UtVec3dX wsf::six_dof::KinematicState::mMoment_ftlbs
protected

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

◆ mNx_g

double wsf::six_dof::KinematicState::mNx_g = 0.0
protected

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

◆ mNy_g

double wsf::six_dof::KinematicState::mNy_g = 0.0
protected

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

◆ mNz_g

double wsf::six_dof::KinematicState::mNz_g = 0.0
protected

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

◆ mOmega

UtVec3dX wsf::six_dof::KinematicState::mOmega
protected

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

◆ mOmegaDot

UtVec3dX wsf::six_dof::KinematicState::mOmegaDot
protected

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

◆ mPitchRate_dps

double wsf::six_dof::KinematicState::mPitchRate_dps = 0.0
protected

Referenced by CalculateSecondaryParameters(), and ZeroKinematicsDuringTesting().

◆ mRadarAlt_m

double wsf::six_dof::KinematicState::mRadarAlt_m = 0.0
protected

Referenced by CalculateSecondaryParameters().

◆ mRangeSinceStart_km

double wsf::six_dof::KinematicState::mRangeSinceStart_km = 0.0
protected

Referenced by CalcRangeSinceStart(), and GetRangeSinceStart_km().

◆ mRho_slugs_per_ft3

double wsf::six_dof::KinematicState::mRho_slugs_per_ft3 = 0.0
protected

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

◆ mRollRate_dps

double wsf::six_dof::KinematicState::mRollRate_dps = 0.0
protected

Referenced by CalculateSecondaryParameters(), and ZeroKinematicsDuringTesting().

◆ mSideForce_lbs

double wsf::six_dof::KinematicState::mSideForce_lbs = 0.0
protected

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

◆ mStartingLat

double wsf::six_dof::KinematicState::mStartingLat = 0.0
protected

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

◆ mStartingLocationInitialized

bool wsf::six_dof::KinematicState::mStartingLocationInitialized = false
protected

Referenced by SetStartingLatLon(), and StartingLocationInitialized().

◆ mStartingLon

double wsf::six_dof::KinematicState::mStartingLon = 0.0
protected

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

◆ mStaticPressure_psf

double wsf::six_dof::KinematicState::mStaticPressure_psf = 0.0
protected

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

◆ mThrust_lbs

double wsf::six_dof::KinematicState::mThrust_lbs = 0.0
protected

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

◆ mUseRotatingEarth

bool wsf::six_dof::KinematicState::mUseRotatingEarth = false
protected

Referenced by SetUseRotatingEarth(), and UseRotatingEarth().

◆ mUseSphericalEarth

bool wsf::six_dof::KinematicState::mUseSphericalEarth = false
protected

Referenced by SetUseSphericalEarth(), and UseSphericalEarth().

◆ mUtEntity

UtEntity wsf::six_dof::KinematicState::mUtEntity
protected

Referenced by CalcBodyVecFromNEDVec(), CalcNEDVecFromWCSVec(), CalcRangeSinceStart(), CalculateSecondaryParameters(), CalcWCSVecFromNEDVec(), GetAlt_m(), GetBearing_rad(), GetCurrentPositionLLA(), GetFlightPathAngle_rad(), GetLat(), GetLocalHeading_rad(), GetLocalPitch_rad(), GetLocalRoll_rad(), GetLocationWCS(), GetLon(), GetPitchWCS(), GetRollWCS(), GetUtEntity(), GetVelocityECI(), GetVelocityNED_mps(), GetVelocityWCS(), GetVerticalSpeed_fpm(), GetYawWCS(), NormalizedGravitationalAccelVec(), SetAlt(), SetAttitude_rad(), SetLocationWCS(), SetOrientationWCS(), SetPositionLLA(), SetSpeed_mps(), SetUseSphericalEarth(), SetVelocityNED(), SetVelocityWCS(), and UpdateAeroState().

◆ mWgt_lbs

double wsf::six_dof::KinematicState::mWgt_lbs = 0.0
protected

Referenced by GetWeight(), and SetLiftDragSideForceThrustWeight().

◆ mYawRate_dps

double wsf::six_dof::KinematicState::mYawRate_dps = 0.0
protected

Referenced by CalculateSecondaryParameters(), and ZeroKinematicsDuringTesting().

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