OrbitParam.hpp 文件参考

#include "AstGlobal.h"

浏览该文件的源代码.

命名空间
namespace	ast

函数
double	ast::aApoAltToApoRad (double apogeeAlt, double bodyRadius)
double	ast::aApoAltToMeanMotion (double apogeeAlt, double eccentricity, double bodyRadius, double gm)
double	ast::aApoAltToPeriAlt (double apogeeAlt, double eccentricity, double bodyRadius)
double	ast::aApoAltToPeriRad (double apogeeAlt, double eccentricity, double bodyRadius)
double	ast::aApoAltToPeriod (double apogeeAlt, double eccentricity, double bodyRadius, double gm)
double	ast::aApoAltToSMA (double apogeeAlt, double eccentricity, double bodyRadius)
double	ast::aApoRadToApoAlt (double apogeeRad, double bodyRadius)
double	ast::aApoRadToMeanMotion (double apogeeRad, double eccentricity, double gm)
double	ast::aApoRadToPeriAlt (double apogeeRad, double eccentricity, double bodyRadius)
double	ast::aApoRadToPeriod (double apogeeRad, double eccentricity, double gm)
double	ast::aApoRadToPeriRad (double apogeeRad, double eccentricity)
double	ast::aApoRadToEcc (double apogeeRad, double semiMajorAxis)
double	ast::aApoRadToSMA (double apogeeRad, double eccentricity)
double	ast::aEccToMean (double eccAnomaly, double eccentricity)
double	ast::aEccToTrue (double eccAnomaly, double eccentricity)
double	ast::aEccToTimePastAscNode (double eccAnomaly, double argPeri, double semiMajorAxis, double eccentricity, double gm)
double	ast::aEccToTimePastPeri (double eccAnomaly, double semiMajorAxis, double eccentricity, double gm)
double	ast::aMeanMotionToApoAlt (double meanMotion, double eccentricity, double bodyRadius, double gm)
double	ast::aMeanMotionToApoRad (double meanMotion, double eccentricity, double gm)
double	ast::aMeanMotionToPeriAlt (double meanMotion, double eccentricity, double bodyRadius, double gm)
double	ast::aMeanMotionToPeriRad (double meanMotion, double eccentricity, double gm)
double	ast::aMeanMotionToPeriod (double meanMotn)
double	ast::aMeanMotionToSMA (double meanMotn, double gm)
double	ast::aMeanToEcc (double meanAnomaly, double eccentricity, double eps=1e-14, int maxIter=100)
double	ast::aMeanToTimePastAscNode (double meanAnomaly, double argPeri, double semiMajorAxis, double eccentricity, double gm)
double	ast::aMeanToTimePastPeri (double meanAnomaly, double semiMajorAxis, double gm)
double	ast::aMeanToTrue (double meanAnomaly, double eccentricity, double eps=1e-14, int maxIter=100)
double	ast::aPeriAltToApoAlt (double perigeeAlt, double eccentricity, double bodyRadius)
double	ast::aPeriAltToApoRad (double perigeeAlt, double eccentricity, double bodyRadius)
double	ast::aPeriAltToMeanMotion (double perigeeAlt, double eccentricity, double bodyRadius, double gm)
double	ast::aPeriAltToPeriRad (double perigeeAlt, double bodyRadius)
double	ast::aPeriAltToPeriod (double perigeeAlt, double eccentricity, double bodyRadius, double gm)
double	ast::aPeriAltToSMA (double perigeeAlt, double eccentricity, double bodyRadius)
double	ast::aPeriRadToApoAlt (double perigeeRad, double eccentricity, double bodyRadius)
double	ast::aPeriRadToApoRad (double perigeeRad, double eccentricity)
double	ast::aPeriRadToMeanMotion (double perigeeRad, double eccentricity, double gm)
double	ast::aPeriRadToPeriAlt (double perigeeRad, double bodyRadius)
double	ast::aPeriRadToPeriod (double perigeeRad, double eccentricity, double gm)
double	ast::aPeriRadToSMA (double perigeeRad, double eccentricity)
double	ast::aPeriRadToEcc (double perigeeRad, double semiMajorAxis)
double	ast::aPeriodToApoAlt (double period, double eccentricity, double bodyRadius, double gm)
double	ast::aPeriodToApoRad (double period, double eccentricity, double gm)
double	ast::aPeriodToMeanMotion (double period)
double	ast::aPeriodToPeriAlt (double period, double eccentricity, double bodyRadius, double gm)
double	ast::aPeriodToPeriRad (double period, double eccentricity, double gm)
double	ast::aPeriodToSMA (double period, double gm)
double	ast::aPeriRadApoRadToEcc (double perigeeRad, double apogeeRad)
double	ast::aPeriAltApoAltToEcc (double perigeeAlt, double apogeeAlt, double bodyRadius)
double	ast::aSMAToApoAlt (double semiMajorAxis, double eccentricity, double bodyRadius)
double	ast::aSMAToApoRad (double semiMajorAxis, double eccentricity)
double	ast::aSMAToMeanMotion (double semiMajorAxis, double gm)
double	ast::aSMAToPeriAlt (double semiMajorAxis, double eccentricity, double bodyRadius)
double	ast::aSMAToPeriRad (double semiMajorAxis, double eccentricity)
double	ast::aSMAToPeriod (double semiMajorAxis, double gm)
double	ast::aSMAToSMinAx (double semiMajorAxis, double eccentricity)
double	ast::aSMAToSParam (double semiMajorAxis, double eccentricity)
double	ast::aSMinAxToSMA (double semiminorAxis, double eccentricity)
double	ast::aTimePastAscNodeToEcc (double TimePastAscNode, double argPeri, double semiMajorAxis, double eccentricity, double gm, double eps=1e-14, int maxIter=100)
double	ast::aTimePastAscNodeToMean (double TimePastAscNode, double argPeri, double semiMajorAxis, double eccentricity, double gm)
double	ast::aTimePastAscNodeToTimePastPeri (double TimePastAscNode, double argPeri, double semiMajorAxis, double eccentricity, double gm)
double	ast::aTimePastAscNodeToTrue (double TimePastAscNode, double argPeri, double semiMajorAxis, double eccentricity, double gm, double eps=1e-14, int maxIter=100)
double	ast::aTimePastPeriToEcc (double TimePastPeri, double semiMajorAxis, double eccentricity, double gm, double eps=1e-14, int maxIter=100)
double	ast::aTimePastPeriToMean (double TimePastPeri, double semiMajorAxis, double gm)
double	ast::aTimePastPeriToTrue (double TimePastPeri, double semiMajorAxis, double eccentricity, double gm, double eps=1e-14, int maxIter=100)
double	ast::aTimePastPeriToTimePastAscNode (double TimePastPeri, double argPeri, double semiMajorAxis, double eccentricity, double gm)
double	ast::aTrueToEcc (double trueAnomaly, double eccentricity)
double	ast::aTrueToMean (double trueAnomaly, double eccentricity)
double	ast::aTrueToTimePastAscNode (double trueAnomaly, double argPeri, double semiMajorAxis, double eccentricity, double gm)
double	ast::aTrueToTimePastPeri (double trueAnomaly, double semiMajorAxis, double eccentricity, double gm)
double	ast::aTrueToArgLat (double trueAnomaly, double argPeri)
double	ast::aArgLatToTrue (double argLat, double argPeri)
double	ast::aTrueToTrueLong (double trueAnomaly, double argPeri, double raan)
double	ast::aArgPeriToLongPeri (double argPeri, double raan)
double	ast::aRAANToLAN (double raan, Axes *inertialAxes, const TimePoint &timeOfAscNodePassage, Axes *bodyFixedAxes)
double	ast::aLANToRAAN (double lan, Axes *bodyFixedAxes, const TimePoint &timeOfAscNodePassage, Axes *inertialAxes)
double	ast::aRepeatGroundTrackSMA (int daysToRepeat, int revsToRepeat, double gm, double bodyRotRate)
double	ast::aEccToFlat (double eccentricity)
double	ast::aFlatToEcc (double flatFactor)

详细描述

轨道参数转换与计算接口

提供各种轨道参数之间的转换函数，包括近地点/远地点高度/半径、周期、平均角速度、偏心率等参数的相互转换。

作者

axel

日期

19.11.2025

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