40AST_CORE_API
double aSOIRadius(
double gmPrimary,
double gmSatellite,
double orbitSemiMajorAxis);
58 CelestialBody& primaryBody,
59 CelestialBody& secondaryBody,
61 const TimePoint& initTime,
62 const CartState& initState,
78 const TimePoint& initTime,
79 const CartState& initState,
99 CelestialBody& primaryBody,
100 CelestialBody& secondaryBody,
102 const TimePoint& initTime,
103 const CartState& initState,
119 const TimePoint& initTime,
120 const CartState& initState,
errc_t aPatchedConicPropToPrimary(CelestialBody &primaryBody, CelestialBody &secondaryBody, double soiRadius, const TimePoint &initTime, const CartState &initState, TimePoint &outTime, CartState &outState)
双二体模型卫星到主天体预报(终端在主天体)
定义 PatchedConic.cpp:290
errc_t aPatchedConicPropMoonToEarth(double soiRadius, const TimePoint &initTime, const CartState &initState, TimePoint &outTime, CartState &outState)
地月转移双二体模型月球到地球预报
定义 PatchedConic.cpp:434
errc_t aPatchedConicPropEarthToMoon(double soiRadius, const TimePoint &initTime, const CartState &initState, TimePoint &outTime, CartState &outState)
地月转移双二体模型前推预报
定义 PatchedConic.cpp:270
double aSOIRadius(double gmPrimary, double gmSatellite, double orbitSemiMajorAxis)
计算卫星的影响球半径 (Laplace SOI)
定义 PatchedConic.cpp:77
errc_t aPatchedConicPropToSecondary(CelestialBody &primaryBody, CelestialBody &secondaryBody, double soiRadius, const TimePoint &initTime, const CartState &initState, TimePoint &outTime, CartState &outState)
双二体模型前推预报(终端在卫星)
定义 PatchedConic.cpp:84