🛰️航天仿真算法库 SpaceAST 0.0.1
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OrbitalPrecession.hpp
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21#pragma once
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23#include "AstGlobal.h"
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25AST_NAMESPACE_BEGIN
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41AST_CORE_CAPI double aRAANRate(double gm, double j2, double rb, double a, double ecc, double inc);
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51AST_CORE_CAPI double aArgPeriRate(double gm, double j2, double rb, double a, double ecc, double inc);
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62AST_CORE_CAPI double aMeanAnomalyRate(double gm, double j2, double rb, double a, double ecc, double inc);
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74AST_CORE_CAPI double aMeanArgLatRate(double gm, double j2, double rb, double a, double ecc, double inc);
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85AST_CORE_CAPI double aJ2Period(double gm, double j2, double rb, double a, double ecc, double inc);
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90AST_NAMESPACE_END
double aMeanAnomalyRate(double gm, double j2, double rb, double a, double ecc, double inc)
计算轨道平近点角变化率
定义 OrbitalPrecession.cpp:43
double aArgPeriRate(double gm, double j2, double rb, double a, double ecc, double inc)
计算轨道近点幅角变化率
定义 OrbitalPrecession.cpp:36
double aMeanArgLatRate(double gm, double j2, double rb, double a, double ecc, double inc)
计算维度幅角平均变化率(平近点角变化率 + 近点幅角变化率)
定义 OrbitalPrecession.cpp:49
double aRAANRate(double gm, double j2, double rb, double a, double ecc, double inc)
计算轨道升交点赤经漂移速率
定义 OrbitalPrecession.cpp:29
double aJ2Period(double gm, double j2, double rb, double a, double ecc, double inc)
计算轨道在J2长期项影响下的轨道周期/交点周期
定义 OrbitalPrecession.cpp:54