类 ast::SimpleOrbitDesigner 继承关系图:

Public 成员函数
	SimpleOrbitDesigner (CelestialBody *body)

errc_t	getOrbitState (ModOrbElem &orbElem) const override

double	getSemimajorAxis () const

double	getEccentricity () const

double	getInclination () const

double	getRightAscensionOfAscendingNode () const

double	getArgumentOfPeriapsis () const

double	getTrueAnomaly () const

void	setSemimajorAxis (double semimajorAxis)

void	setEccentricity (double eccentricity)

void	setInclination (double inclination)

void	setRightAscensionOfAscendingNode (double rightAscensionOfAscendingNode)

void	setArgumentOfPeriapsis (double argumentOfPeriapsis)

void	setTrueAnomaly (double trueAnomaly)

errc_t	getOrbitState (CartState &cartState) const

errc_t	getOrbitState (OrbElem &orbElem) const

Public 成员函数继承自 ast::BaseOrbitDesigner
	BaseOrbitDesigner (CelestialBody *body)

CelestialBody *	getCelestialBody () const

double	getGM () const

double	getJ2 () const

double	getBodyRadius () const

errc_t	getOrbitEpoch (TimePoint &orbitEpoch) const final

errc_t	getOrbitState (CartState &cartState) const

errc_t	getOrbitState (OrbElem &orbElem) const

errc_t	getCoordFrame (bool &useCoordEpoch, TimePoint &coordEpoch, SharedPtr< Frame > &coordFrame) const override

Public 成员函数继承自 ast::IOrbitDesigner

Protected 属性
double	semimajorAxis_ {0.0}

double	eccentricity_ {0.0}

double	inclination_ {0.0}

double	rightAscensionOfAscendingNode_ {0.0}

double	argumentOfPeriapsis_ {0.0}

double	trueAnomaly_ {0.0}

Protected 属性继承自 ast::BaseOrbitDesigner
SharedPtr< CelestialBody >	celestialBody_

TimePoint	orbitEpoch_ {}

额外继承的成员函数
静态 Public 成员函数继承自 ast::BaseOrbitDesigner
static CelestialBody *	getDefaultCelestialBody ()

详细描述

基础轨道设计器

成员函数说明

errc_t ast::BaseOrbitDesigner::getOrbitState ( CartState & cartState ) const

获取轨道状态

参数

cartState 笛卡尔状态

errc_t ast::SimpleOrbitDesigner::getOrbitState ( ModOrbElem & orbElem ) const

overridevirtual

获取轨道状态

参数

orbitEpoch	轨道历元（可选）
orbElem	轨道根数

errc_t ast::BaseOrbitDesigner::getOrbitState ( OrbElem & orbElem ) const

获取轨道状态

参数

orbElem 轨道根数

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