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WSF
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#include <P6DofAeroCoreObject.hpp>
Public Member Functions | |
| P6DofAeroCoreObject () | |
| ~P6DofAeroCoreObject ()=default | |
| P6DofAeroCoreObject & | operator= (const P6DofAeroCoreObject &other)=delete |
| P6DofAeroCoreObject * | Clone () const |
| bool | ProcessInput (UtInput &aInput) |
| bool | Initialize () |
| void | SetModeName (const std::string &aName) |
| std::string | GetModeName () const |
| const std::list< UtCloneablePtr< P6DofAeroCoreObject > > * | GetSubModesList () const |
| P6DofAeroCoreObject * | GetSubModeByName (const std::string &aName) const |
| void | CalculateCoreAeroFM (double aDynPress_lbsqft, double aMach, double aSpeed_fps, double aAlpha_rad, double aBeta_rad, double aAlphaDot_rps, double aBetaDot_rps, const UtVec3dX &aAngularRates_rps, UtVec3dX &aMoment_ftlbs, double &aLift_lbs, double &aDrag_lbs, double &aSideForce_lbs, double aRadiusSizeFactor=1.0) |
| double | CalculateLiftAtSpecifiedAlpha_lbs (double aDynPress_lbsqft, double aMach, double aAlpha_deg, double aRadiusSizeFactor=1.0) |
| void | CalculateAeroCoefficientVectors (double aMach, double aAlpha_rad, double &aCLArea, double &aCdArea, double &aCmArea, double aRadiusSizeFactor=1.0) |
| UtVec3dX | GetAeroCenter_ft () const |
| double | GetWingChord_ft () const |
| double | GetWingSpan_ft () const |
| double | GetWingArea_sqft () const |
| double | GetRefArea_sqft () const |
| double | CL_AlphaMach (double aMach, double aAlpha_rad) |
| double | CL_AlphaBetaMach (double aMach, double aAlpha_rad, double aBeta_rad) |
| double | CLq_AlphaMach (double aMach, double aAlpha_rad) |
| double | CL_AlphaDotAlphaMach (double aMach, double aAlpha_rad) |
| double | Cd_AlphaMach (double aMach, double aAlpha_rad) |
| double | Cd_BetaMach (double aMach, double aBeta_rad) |
| double | Cd_AlphaBetaMach (double aMach, double aAlpha_rad, double aBeta_rad) |
| double | CY_BetaMach (double aMach, double aBeta_rad) |
| double | CY_AlphaBetaMach (double aMach, double aAlpha_rad, double aBeta_rad) |
| double | CYr_BetaMach (double aMach, double aBeta_rad) |
| double | CY_BetaDotBetaMach (double aMach, double aBeta_rad) |
| double | Cm_AlphaMach (double aMach, double aAlpha_rad) |
| double | Cm_AlphaBetaMach (double aMach, double aAlpha_rad, double aBeta_rad) |
| double | Cmq_Mach (double aMach) |
| double | Cmp_Mach (double aMach) |
| double | CmAlphaDotMach (double aMach) |
| double | Cn_BetaMach (double aMach, double aBeta_rad) |
| double | Cn_AlphaBetaMach (double aMach, double aAlpha_rad, double aBeta_rad) |
| double | CnBetaDotMach (double aMach) |
| double | Cnr_Mach (double aMach) |
| double | Cnp_Mach (double aMach) |
| double | Cl_BetaMach (double aMach, double aBeta_rad) |
| double | Cl_AlphaBetaMach (double aMach, double aAlpha_rad, double aBeta_rad) |
| double | Clp_Mach (double aMach) |
| double | Cl_AlphaDotMach (double aMach) |
| double | Cl_BetaDotMach (double aMach) |
| double | Clr_Mach (double aMach) |
| double | Clq_Mach (double aMach) |
| double | CalculateAeroCmArea (double aMach, double aAlpha_rad) |
| double | CalculateAeroCLArea (double aMach, double aAlpha_rad) |
| double | CalculateAeroCdArea (double aMach, double aAlpha_rad) |
| bool | UsesRefArea () const |
| bool | UseLegacyAero () const |
Protected Member Functions | |
| P6DofAeroCoreObject (const P6DofAeroCoreObject &aSrc)=default | |
Static Protected Member Functions | |
| static bool | ProcessCommonInput (UtInput &aInput, const std::string &aCommand, P6DofAeroCoreObject *aObject) |
Protected Attributes | |
| std::string | mModeName = "DEFAULT" |
| std::list< UtCloneablePtr< P6DofAeroCoreObject > > | mSubModesList |
| double | mWingChord_ft = 0.0 |
| double | mWingSpan_ft = 0.0 |
| double | mWingArea_sqft = 0.0 |
| double | mRefArea_sqft = 0.0 |
| double | mRefLength_ft = 0.0 |
| bool | mUseRefArea = false |
| UtVec3dX | mAeroCenter_ft |
| bool | mUseLegacy = false |
| bool | mUseLegacySet = false |
| bool | mUseReducedFrequency = true |
| bool | mUseReducedFrequencySet = false |
| UtCloneablePtr< UtTable::Table > | mCL_AlphaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCL_AlphaBetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCLq_AlphaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCL_AlphaDotAlphaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCd_AlphaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCd_BetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCd_AlphaBetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCY_BetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCY_AlphaBetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCYr_BetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCY_BetaDotBetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCm_AlphaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCm_AlphaBetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mCmq_MachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mCmp_MachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mCm_AlphaDotMachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCn_BetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCn_AlphaBetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mCn_BetaDotMachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mCnr_MachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mCnp_MachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCl_BetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Table > | mCl_AlphaBetaMachTablePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mClp_MachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mCl_AlphaDotMachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mCl_BetaDotMachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mClr_MachCurvePtr {nullptr} |
| UtCloneablePtr< UtTable::Curve > | mClq_MachCurvePtr {nullptr} |
| P6DofAeroCoreObject::P6DofAeroCoreObject | ( | ) |
References mAeroCenter_ft.
Referenced by Clone(), GetSubModeByName(), operator=(), P6DofAeroCoreObject(), and ProcessCommonInput().
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References P6DofAeroCoreObject().
| double P6DofAeroCoreObject::CalculateAeroCdArea | ( | double | aMach, |
| double | aAlpha_rad ) |
References Cd_AlphaBetaMach(), Cd_AlphaMach(), mRefArea_sqft, mUseLegacy, mUseRefArea, and mWingArea_sqft.
Referenced by operator=().
| double P6DofAeroCoreObject::CalculateAeroCLArea | ( | double | aMach, |
| double | aAlpha_rad ) |
References CL_AlphaBetaMach(), CL_AlphaMach(), mRefArea_sqft, mUseLegacy, mUseRefArea, and mWingArea_sqft.
Referenced by operator=().
| double P6DofAeroCoreObject::CalculateAeroCmArea | ( | double | aMach, |
| double | aAlpha_rad ) |
References Cm_AlphaBetaMach(), Cm_AlphaMach(), mRefArea_sqft, mUseLegacy, mUseRefArea, mWingArea_sqft, and mWingChord_ft.
Referenced by operator=().
| void P6DofAeroCoreObject::CalculateAeroCoefficientVectors | ( | double | aMach, |
| double | aAlpha_rad, | ||
| double & | aCLArea, | ||
| double & | aCdArea, | ||
| double & | aCmArea, | ||
| double | aRadiusSizeFactor = 1.0 ) |
References Cd_AlphaBetaMach(), Cd_AlphaMach(), CL_AlphaBetaMach(), CL_AlphaMach(), Cm_AlphaBetaMach(), Cm_AlphaMach(), mRefArea_sqft, mUseLegacy, mUseRefArea, mWingArea_sqft, and mWingChord_ft.
Referenced by operator=().
| void P6DofAeroCoreObject::CalculateCoreAeroFM | ( | double | aDynPress_lbsqft, |
| double | aMach, | ||
| double | aSpeed_fps, | ||
| double | aAlpha_rad, | ||
| double | aBeta_rad, | ||
| double | aAlphaDot_rps, | ||
| double | aBetaDot_rps, | ||
| const UtVec3dX & | aAngularRates_rps, | ||
| UtVec3dX & | aMoment_ftlbs, | ||
| double & | aLift_lbs, | ||
| double & | aDrag_lbs, | ||
| double & | aSideForce_lbs, | ||
| double | aRadiusSizeFactor = 1.0 ) |
References Cd_AlphaBetaMach(), Cd_AlphaMach(), Cd_BetaMach(), CL_AlphaBetaMach(), Cl_AlphaBetaMach(), CL_AlphaDotAlphaMach(), Cl_AlphaDotMach(), CL_AlphaMach(), Cl_BetaDotMach(), Cl_BetaMach(), Clp_Mach(), CLq_AlphaMach(), Clq_Mach(), Clr_Mach(), Cm_AlphaBetaMach(), Cm_AlphaMach(), CmAlphaDotMach(), Cmp_Mach(), Cmq_Mach(), Cn_AlphaBetaMach(), Cn_BetaMach(), CnBetaDotMach(), Cnp_Mach(), Cnr_Mach(), CY_AlphaBetaMach(), CY_BetaDotBetaMach(), CY_BetaMach(), CYr_BetaMach(), mRefArea_sqft, mRefLength_ft, mUseLegacy, mUseReducedFrequency, mUseRefArea, mWingArea_sqft, mWingChord_ft, and mWingSpan_ft.
Referenced by operator=().
| double P6DofAeroCoreObject::CalculateLiftAtSpecifiedAlpha_lbs | ( | double | aDynPress_lbsqft, |
| double | aMach, | ||
| double | aAlpha_deg, | ||
| double | aRadiusSizeFactor = 1.0 ) |
References CL_AlphaBetaMach(), CL_AlphaMach(), mRefArea_sqft, mUseLegacy, mUseRefArea, and mWingArea_sqft.
Referenced by operator=().
| double P6DofAeroCoreObject::Cd_AlphaBetaMach | ( | double | aMach, |
| double | aAlpha_rad, | ||
| double | aBeta_rad ) |
| double P6DofAeroCoreObject::Cd_AlphaMach | ( | double | aMach, |
| double | aAlpha_rad ) |
| double P6DofAeroCoreObject::Cd_BetaMach | ( | double | aMach, |
| double | aBeta_rad ) |
References mCd_BetaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CL_AlphaBetaMach | ( | double | aMach, |
| double | aAlpha_rad, | ||
| double | aBeta_rad ) |
References mCL_AlphaBetaMachTablePtr.
Referenced by CalculateAeroCLArea(), CalculateAeroCoefficientVectors(), CalculateCoreAeroFM(), CalculateLiftAtSpecifiedAlpha_lbs(), WsfP6DOF_MoverTestObject::LimitAlphaByMaxGLoad(), WsfP6DOF_MoverTestObject::LimitAlphaByMaxGLoad(), operator=(), WsfP6DOF_MoverTestObject::TurnRateAt(), and WsfP6DOF_MoverTestObject::TurnRateWithConditions().
| double P6DofAeroCoreObject::Cl_AlphaBetaMach | ( | double | aMach, |
| double | aAlpha_rad, | ||
| double | aBeta_rad ) |
References mCl_AlphaBetaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CL_AlphaDotAlphaMach | ( | double | aMach, |
| double | aAlpha_rad ) |
References mCL_AlphaDotAlphaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cl_AlphaDotMach | ( | double | aMach | ) |
References mCl_AlphaDotMachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CL_AlphaMach | ( | double | aMach, |
| double | aAlpha_rad ) |
References mCL_AlphaMachTablePtr.
Referenced by CalculateAeroCLArea(), CalculateAeroCoefficientVectors(), CalculateCoreAeroFM(), CalculateLiftAtSpecifiedAlpha_lbs(), WsfP6DOF_MoverTestObject::LimitAlphaByMaxGLoad(), WsfP6DOF_MoverTestObject::LimitAlphaByMaxGLoad(), operator=(), WsfP6DOF_MoverTestObject::TurnRateAt(), and WsfP6DOF_MoverTestObject::TurnRateWithConditions().
| double P6DofAeroCoreObject::Cl_BetaDotMach | ( | double | aMach | ) |
References mCl_BetaDotMachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cl_BetaMach | ( | double | aMach, |
| double | aBeta_rad ) |
References mCl_BetaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| P6DofAeroCoreObject * P6DofAeroCoreObject::Clone | ( | ) | const |
References P6DofAeroCoreObject().
Referenced by P6DofVehicleType::DeriveFrom(), and operator=().
| double P6DofAeroCoreObject::Clp_Mach | ( | double | aMach | ) |
References mClp_MachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CLq_AlphaMach | ( | double | aMach, |
| double | aAlpha_rad ) |
References mCLq_AlphaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Clq_Mach | ( | double | aMach | ) |
References mClq_MachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Clr_Mach | ( | double | aMach | ) |
References mClr_MachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cm_AlphaBetaMach | ( | double | aMach, |
| double | aAlpha_rad, | ||
| double | aBeta_rad ) |
References mCm_AlphaBetaMachTablePtr.
Referenced by CalculateAeroCmArea(), CalculateAeroCoefficientVectors(), CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cm_AlphaMach | ( | double | aMach, |
| double | aAlpha_rad ) |
References mCm_AlphaMachTablePtr.
Referenced by CalculateAeroCmArea(), CalculateAeroCoefficientVectors(), CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CmAlphaDotMach | ( | double | aMach | ) |
References mCm_AlphaDotMachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cmp_Mach | ( | double | aMach | ) |
References mCmp_MachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cmq_Mach | ( | double | aMach | ) |
References mCmq_MachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cn_AlphaBetaMach | ( | double | aMach, |
| double | aAlpha_rad, | ||
| double | aBeta_rad ) |
References mCn_AlphaBetaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cn_BetaMach | ( | double | aMach, |
| double | aBeta_rad ) |
References mCn_BetaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CnBetaDotMach | ( | double | aMach | ) |
References mCn_BetaDotMachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cnp_Mach | ( | double | aMach | ) |
References mCnp_MachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::Cnr_Mach | ( | double | aMach | ) |
References mCnr_MachCurvePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CY_AlphaBetaMach | ( | double | aMach, |
| double | aAlpha_rad, | ||
| double | aBeta_rad ) |
References mCY_AlphaBetaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CY_BetaDotBetaMach | ( | double | aMach, |
| double | aBeta_rad ) |
References mCY_BetaDotBetaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CY_BetaMach | ( | double | aMach, |
| double | aBeta_rad ) |
References mCY_BetaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| double P6DofAeroCoreObject::CYr_BetaMach | ( | double | aMach, |
| double | aBeta_rad ) |
References mCYr_BetaMachTablePtr.
Referenced by CalculateCoreAeroFM(), and operator=().
| UtVec3dX P6DofAeroCoreObject::GetAeroCenter_ft | ( | ) | const |
References mAeroCenter_ft.
Referenced by P6DofIntegrator::CalculateFM(), and operator=().
| std::string P6DofAeroCoreObject::GetModeName | ( | ) | const |
References mModeName.
Referenced by operator=().
| double P6DofAeroCoreObject::GetRefArea_sqft | ( | ) | const |
| P6DofAeroCoreObject * P6DofAeroCoreObject::GetSubModeByName | ( | const std::string & | aName | ) | const |
References mSubModesList, and P6DofAeroCoreObject().
Referenced by operator=().
| const std::list< UtCloneablePtr< P6DofAeroCoreObject > > * P6DofAeroCoreObject::GetSubModesList | ( | ) | const |
References mSubModesList.
Referenced by operator=().
| double P6DofAeroCoreObject::GetWingArea_sqft | ( | ) | const |
| double P6DofAeroCoreObject::GetWingChord_ft | ( | ) | const |
References mWingChord_ft.
Referenced by operator=().
| double P6DofAeroCoreObject::GetWingSpan_ft | ( | ) | const |
References mWingSpan_ft.
Referenced by operator=().
| bool P6DofAeroCoreObject::Initialize | ( | ) |
References mSubModesList, mUseLegacy, and mUseReducedFrequency.
Referenced by operator=().
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References CalculateAeroCdArea(), CalculateAeroCLArea(), CalculateAeroCmArea(), CalculateAeroCoefficientVectors(), CalculateCoreAeroFM(), CalculateLiftAtSpecifiedAlpha_lbs(), Cd_AlphaBetaMach(), Cd_AlphaMach(), Cd_BetaMach(), CL_AlphaBetaMach(), Cl_AlphaBetaMach(), CL_AlphaDotAlphaMach(), Cl_AlphaDotMach(), CL_AlphaMach(), Cl_BetaDotMach(), Cl_BetaMach(), Clone(), Clp_Mach(), CLq_AlphaMach(), Clq_Mach(), Clr_Mach(), Cm_AlphaBetaMach(), Cm_AlphaMach(), CmAlphaDotMach(), Cmp_Mach(), Cmq_Mach(), Cn_AlphaBetaMach(), Cn_BetaMach(), CnBetaDotMach(), Cnp_Mach(), Cnr_Mach(), CY_AlphaBetaMach(), CY_BetaDotBetaMach(), CY_BetaMach(), CYr_BetaMach(), GetAeroCenter_ft(), GetModeName(), GetRefArea_sqft(), GetSubModeByName(), GetSubModesList(), GetWingArea_sqft(), GetWingChord_ft(), GetWingSpan_ft(), Initialize(), P6DofAeroCoreObject(), ProcessInput(), and SetModeName().
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References mAeroCenter_ft, mCd_AlphaBetaMachTablePtr, mCd_AlphaMachTablePtr, mCd_BetaMachTablePtr, mCL_AlphaBetaMachTablePtr, mCl_AlphaBetaMachTablePtr, mCL_AlphaDotAlphaMachTablePtr, mCl_AlphaDotMachCurvePtr, mCL_AlphaMachTablePtr, mCl_BetaDotMachCurvePtr, mCl_BetaMachTablePtr, mClp_MachCurvePtr, mCLq_AlphaMachTablePtr, mClq_MachCurvePtr, mClr_MachCurvePtr, mCm_AlphaBetaMachTablePtr, mCm_AlphaDotMachCurvePtr, mCm_AlphaMachTablePtr, mCmp_MachCurvePtr, mCmq_MachCurvePtr, mCn_AlphaBetaMachTablePtr, mCn_BetaDotMachCurvePtr, mCn_BetaMachTablePtr, mCnp_MachCurvePtr, mCnr_MachCurvePtr, mCY_AlphaBetaMachTablePtr, mCY_BetaDotBetaMachTablePtr, mCY_BetaMachTablePtr, mCYr_BetaMachTablePtr, mRefArea_sqft, mRefLength_ft, mUseLegacy, mUseLegacySet, mUseReducedFrequency, mUseReducedFrequencySet, mUseRefArea, mWingArea_sqft, mWingChord_ft, mWingSpan_ft, and P6DofAeroCoreObject().
Referenced by ProcessInput().
| bool P6DofAeroCoreObject::ProcessInput | ( | UtInput & | aInput | ) |
References mSubModesList, and ProcessCommonInput().
Referenced by operator=().
| void P6DofAeroCoreObject::SetModeName | ( | const std::string & | aName | ) |
References mModeName.
Referenced by operator=().
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References mUseLegacy.
Referenced by WsfP6DOF_MoverTestObject::AlphaAtDesiredDrag(), WsfP6DOF_MoverTestObject::AlphaAtDesiredDrag(), WsfP6DOF_MoverTestObject::LimitAlphaByMaxGLoad(), WsfP6DOF_MoverTestObject::LimitAlphaByMaxGLoad(), WsfP6DOF_MoverTestObject::TurnRateAt(), and WsfP6DOF_MoverTestObject::TurnRateWithConditions().
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Referenced by GetAeroCenter_ft(), P6DofAeroCoreObject(), and ProcessCommonInput().
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Referenced by Cd_AlphaBetaMach(), and ProcessCommonInput().
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Referenced by Cd_AlphaMach(), and ProcessCommonInput().
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Referenced by Cd_BetaMach(), and ProcessCommonInput().
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Referenced by CL_AlphaBetaMach(), and ProcessCommonInput().
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Referenced by Cl_AlphaBetaMach(), and ProcessCommonInput().
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Referenced by CL_AlphaDotAlphaMach(), and ProcessCommonInput().
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Referenced by Cl_AlphaDotMach(), and ProcessCommonInput().
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Referenced by CL_AlphaMach(), and ProcessCommonInput().
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Referenced by Cl_BetaDotMach(), and ProcessCommonInput().
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Referenced by Cl_BetaMach(), and ProcessCommonInput().
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Referenced by Clp_Mach(), and ProcessCommonInput().
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Referenced by CLq_AlphaMach(), and ProcessCommonInput().
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Referenced by Clq_Mach(), and ProcessCommonInput().
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Referenced by Clr_Mach(), and ProcessCommonInput().
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Referenced by Cm_AlphaBetaMach(), and ProcessCommonInput().
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Referenced by CmAlphaDotMach(), and ProcessCommonInput().
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Referenced by Cm_AlphaMach(), and ProcessCommonInput().
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Referenced by Cmp_Mach(), and ProcessCommonInput().
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Referenced by Cmq_Mach(), and ProcessCommonInput().
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Referenced by Cn_AlphaBetaMach(), and ProcessCommonInput().
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Referenced by CnBetaDotMach(), and ProcessCommonInput().
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Referenced by Cn_BetaMach(), and ProcessCommonInput().
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Referenced by Cnp_Mach(), and ProcessCommonInput().
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Referenced by Cnr_Mach(), and ProcessCommonInput().
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Referenced by CY_AlphaBetaMach(), and ProcessCommonInput().
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Referenced by CY_BetaDotBetaMach(), and ProcessCommonInput().
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Referenced by CY_BetaMach(), and ProcessCommonInput().
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Referenced by CYr_BetaMach(), and ProcessCommonInput().
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Referenced by GetModeName(), and SetModeName().
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Referenced by CalculateCoreAeroFM(), and ProcessCommonInput().
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Referenced by GetSubModeByName(), GetSubModesList(), Initialize(), and ProcessInput().
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Referenced by ProcessCommonInput().
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Referenced by CalculateCoreAeroFM(), Initialize(), and ProcessCommonInput().
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Referenced by ProcessCommonInput().
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Referenced by CalculateCoreAeroFM(), GetWingSpan_ft(), and ProcessCommonInput().