类 ast::CriticallyInclinedSunSyncOrbitDesigner 继承关系图:

Public 成员函数
	CriticallyInclinedSunSyncOrbitDesigner (CelestialBody *body)

errc_t	getOrbitState (ModOrbElem &orbElem) const override

double	getPerigeeAltitude () const

double	getRAAN () const

void	setPerigeeAltitude (double perigeeAltitude)

void	setRAAN (double raan)

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	perigeeAltitude_ {0}

double	raan_ {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

太阳同步临界倾角轨道/太阳同步冻结轨道设计器

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::CriticallyInclinedSunSyncOrbitDesigner::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

该类的文档由以下文件生成: