OrbitDesign.hpp

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#pragma once
 
#include "AstGlobal.h"
 
AST_NAMESPACE_BEGIN
 
errc_t aSunSynchronousInclination(double gm, double j2, double rb, double bodyMeanMotion, double a, double ecc, double& inc);
 
errc_t aSunSynchronousSemiMajorAxis(double gm, double j2, double rb, double bodyMeanMotion, double inc, double ecc, double& semiMajorAxis);
 
 
A_ALWAYS_INLINE double aSunSynchronousInclination(double gm, double j2, double rb, double bodyMeanMotion, double a, double ecc)
{
    double inc;
    aSunSynchronousInclination(gm, j2, rb, bodyMeanMotion, a, ecc, inc);
    return inc;
}
 
A_ALWAYS_INLINE double aSunSynchronousSemiMajorAxis(double gm, double j2, double rb, double bodyMeanMotion, double inc, double ecc)
{
    double semiMajorAxis;
    aSunSynchronousSemiMajorAxis(gm, j2, rb, bodyMeanMotion, inc, ecc, semiMajorAxis);
    return semiMajorAxis;
}
 
AST_NAMESPACE_END