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🛰️航天仿真算法库 SpaceAST 0.3.1
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#include "PatchedConic.hpp"#include "AstCore/TwoBody.hpp"#include "AstCore/CelestialBody.hpp"#include "AstCore/Frame.hpp"#include "AstCore/OrbitElement.hpp"#include "AstCore/OrbitParam.hpp"#include "AstCore/RunTimeSolarSystem.hpp"#include "AstCore/RunTimeJplDe.hpp"#include "AstCore/TimeInterval.hpp"#include "AstCore/TimePoint.hpp"#include "AstUtil/Constants.h"#include "AstUtil/Logger.hpp"#include "AstUtil/I18n.hpp"#include "AstMath/BrentSolver.hpp"#include "AstMath/BisectionSolver.hpp"#include "AstMath/KinematicTransform.hpp"#include <cmath>命名空间 | |
| namespace | ast |
函数 | |
| double | ast::aSOIRadius (double gmPrimary, double gmSatellite, double orbitSemiMajorAxis) |
| errc_t | ast::aPatchedConicPropToSecondary (CelestialBody &primaryBody, CelestialBody &secondaryBody, double soiRadius, const TimePoint &initTime, const CartState &initState, TimePoint &outTime, CartState &outState) |
| errc_t | ast::aPatchedConicPropEarthToMoon (double soiRadius, const TimePoint &initTime, const CartState &initState, TimePoint &outTime, CartState &outState) |
| errc_t | ast::aPatchedConicPropToPrimary (CelestialBody &primaryBody, CelestialBody &secondaryBody, double soiRadius, const TimePoint &initTime, const CartState &initState, TimePoint &outTime, CartState &outState) |
| errc_t | ast::aPatchedConicPropMoonToEarth (double soiRadius, const TimePoint &initTime, const CartState &initState, TimePoint &outTime, CartState &outState) |
圆锥曲线拼接(双二体)预报
以卫星影响球为拼接面的圆锥曲线拼接预报。
SpaceAST项目(https://github.com/space-ast/ast) 本软件基于 Apache 2.0 开源许可证分发。 您可在遵守许可证条款的前提下使用、修改和分发本软件。 许可证全文请见:
http://www.apache.org/licenses/LICENSE-2.0
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