类 ast::SunSynchronousOrbitDesigner 继承关系图:

Public 类型
enum	EGeometryDefinition { eAltitude = 0 , eInclination = 1 }

enum	ENodeDefinition { eAscendingNode = 0 , eDescendingNode = 1 }

Public 成员函数
	SunSynchronousOrbitDesigner (CelestialBody *body)

errc_t	getOrbitState (ModOrbElem &orbElem) const override

EGeometryDefinition	getGeometryDefinition () const

void	setGeometryDefinition (EGeometryDefinition def)

ENodeDefinition	getNodeDefinition () const

void	setNodeDefinition (ENodeDefinition def)

double	calcInclination (double alt) const

double	calcInclination () const

double	calcAltitude (double inc) const

double	calcAltitude () const

double	getInclination () const

void	setInclination (double inc)

double	getAltitude () const

void	setAltitude (double alt)

double	getLocalTimeOfAscendingNode () const

void	setLocalTimeOfAscendingNode (double t)

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

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

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

TimePoint	orbitEpoch_ {}

详细描述

太阳同步轨道设计器

成员函数说明

errc_t ast::SunSynchronousOrbitDesigner::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

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