🛰️航天仿真算法库 SpaceAST 0.0.1
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OrbitGeometry.cpp 文件参考
#include "OrbitGeometry.hpp"
#include "AstCore/OrbitElement.hpp"
#include "AstCore/TwoBody.hpp"
#include "AstCore/Vector.hpp"
#include "AstCore/TimeIntervalList.hpp"
#include "AstMath/BrentOptimizer.hpp"
#include "AstUtil/Constants.h"
#include <algorithm>
#include <cmath>
#include <limits>
#include <utility>
#include <vector>

命名空间

namespace  ast
 

函数

void ast::aOrbitPlaneNormal (double inc, double raan, Vector3d &normal)
 
double ast::aOrbitRadius (double semiMajorAxis, double eccentricity, double trueAnomaly)
 
void ast::aOrbitPerifocalBasis (const OrbElem &e, Vector3d &p, Vector3d &q)
 
errc_t ast::aOrbitNodeLineDistances (const OrbElem &orb1, const OrbElem &orb2, double &distPlus, double &distMinus)
 
errc_t ast::aOrbitPathMinDistance (const OrbElem &orb1, const OrbElem &orb2, double &dist)
 
errc_t ast::aOrbitPlaneProximityIntervals (const TimePoint &epoch, const OrbElem &orbit, const OrbElem &other, double gm, double threshold, const TimeInterval &window, TimeIntervalList &result)
 
double ast::aOrbitTrueAnomaly (const TimePoint &epoch, const OrbElem &orbit, double gm, const TimePoint &time)
 
void ast::aOrbitPosition (const TimePoint &epoch, const OrbElem &orbit, double gm, const TimePoint &time, Vector3d &position)
 
void ast::aOrbitPosition2 (const TimePoint &epoch, const OrbElem &orbit, double gm, const TimePoint &time, Vector3d &position)
 
void ast::aOrbitPosition3 (const TimePoint &epoch, const OrbElem &orbit, double gm, const TimePoint &time, Vector3d &position)
 
errc_t ast::aOrbitPlaneDistance (const TimePoint &epoch, const OrbElem &orbit, const OrbElem &other, double gm, const TimePoint &time, double &dist)
 

详细描述



作者
axel
日期
2026-08-19

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

重要须知: 软件按"现有状态"提供,无任何明示或暗示的担保条件。 除非法律要求或书面同意,作者与贡献者不承担任何责任。 使用本软件所产生的风险,需由您自行承担。