OrbitGeometry.hpp

浏览该文件的文档.

 
 
#pragma once
 
#include "AstGlobal.h"
 
AST_NAMESPACE_BEGIN
 
AST_CORE_CAPI void aOrbitPlaneNormal(double inc, double raan, Vector3d& normal);
 
 
AST_CORE_CAPI double aOrbitRadius(double semiMajorAxis, double eccentricity, double trueAnomaly);
 
 
AST_CORE_CAPI void aOrbitPerifocalBasis(const OrbElem& e, Vector3d& p, Vector3d& q);
 
 
AST_CORE_CAPI errc_t aOrbitNodeLineDistances(const OrbElem& orb1, const OrbElem& orb2, double& distPlus, double& distMinus);
 
                                             
AST_CORE_CAPI errc_t aOrbitPathMinDistance(const OrbElem& orb1, const OrbElem& orb2, double& dist);
 
 
 
AST_CORE_CAPI errc_t aOrbitPlaneProximityIntervals(
     const TimePoint& epoch,     
     const OrbElem& orbit,       
     const OrbElem& other,       
     double gm,                  
     double threshold,           
     const TimeInterval& window,
     TimeIntervalList& result
);
 
AST_CORE_CAPI double aOrbitTrueAnomaly(
    const TimePoint& epoch,
    const OrbElem& orbit,
    double gm,
    const TimePoint& time
);
 
AST_CORE_CAPI void aOrbitPosition(
    const TimePoint& epoch,     
    const OrbElem& orbit,       
    double gm,                  
    const TimePoint& time,      
    Vector3d& position
);
AST_CORE_CAPI void aOrbitPosition2(
    const TimePoint& epoch,     
    const OrbElem& orbit,       
    double gm,                  
    const TimePoint& time,      
    Vector3d& position
);
AST_CORE_CAPI void aOrbitPosition3(
    const TimePoint& epoch,     
    const OrbElem& orbit,       
    double gm,                  
    const TimePoint& time,      
    Vector3d& position
);
 
AST_CORE_CAPI errc_t aOrbitPlaneDistance(
     const TimePoint& epoch,
     const OrbElem& orbit,
     const OrbElem& other,
     double gm,
     const TimePoint& time,
     double& dist
);
 
 
AST_CORE_API errc_t aSolveVerticalLandAscentPlane(
    const GeodeticPoint& site,
    const CelestialBody* body,
    const TimePoint&     tDescent,
    const TimePoint&     tAscent,
    bool                 prograde,
    double& outRaan, double& outInc, double& outU
);
 
 
AST_CORE_API errc_t aSolveVerticalLandAscentPlane(
    const LatLon& site, double duration, double angVel, bool prograde,
    double& outRaan, double& outInc, double& outU
);
 
 
AST_NAMESPACE_END