sgp4/SGP4.h

283 lines
6.7 KiB
C++

#ifndef SGDP4_H_
#define SGDP4_H_
#include "Tle.h"
#include "Eci.h"
class SGP4 {
public:
SGP4(void);
SGP4(const Tle& tle);
virtual ~SGP4(void);
void SetTle(const Tle& tle);
void FindPosition(Eci* eci, double tsince) const;
void FindPosition(Eci* eci, const Julian& date) const;
/*
* XMO
*/
double MeanAnomoly() const {
return mean_anomoly_;
}
/*
* XNODEO
*/
double AscendingNode() const {
return ascending_node_;
}
/*
* OMEGAO
*/
double ArgumentPerigee() const {
return argument_perigee_;
}
/*
* EO
*/
double Eccentricity() const {
return eccentricity_;
}
/*
* XINCL
*/
double Inclination() const {
return inclination_;
}
/*
* XNO
*/
double MeanMotion() const {
return mean_motion_;
}
/*
* BSTAR
*/
double BStar() const {
return bstar_;
}
/*
* AODP
*/
double RecoveredSemiMajorAxis() const {
return recovered_semi_major_axis_;
}
/*
* XNODP
*/
double RecoveredMeanMotion() const {
return recovered_mean_motion_;
}
/*
* PERIGE
*/
double Perigee() const {
return perigee_;
}
double Period() const {
return period_;
}
/*
* EPOCH
*/
Julian Epoch() const {
return epoch_;
}
struct CommonConstants {
double cosio;
double sinio;
double eta;
double t2cof;
double a3ovk2;
double x1mth2;
double x3thm1;
double x7thm1;
double aycof;
double xlcof;
double xnodcf;
double c1;
double c4;
double omgdot; // secular rate of omega (radians/sec)
double xnodot; // secular rate of xnode (radians/sec)
double xmdot; // secular rate of xmo (radians/sec)
};
struct NearSpaceConstants {
double c5;
double omgcof;
double xmcof;
double delmo;
double sinmo;
double d2;
double d3;
double d4;
double t3cof;
double t4cof;
double t5cof;
};
struct DeepSpaceConstants {
double gsto;
double zmol;
double zmos;
/*
* whether the deep space orbit is
* geopotential resonance for 12 hour orbits
*/
bool resonance_flag;
/*
* whether the deep space orbit is
* 24h synchronous resonance
*/
bool synchronous_flag;
/*
* lunar / solar constants for epoch
* applied during DeepSpaceSecular()
*/
double sse;
double ssi;
double ssl;
double ssg;
double ssh;
/*
* lunar / solar constants
* used during DeepSpaceCalculateLunarSolarTerms()
*/
double se2;
double si2;
double sl2;
double sgh2;
double sh2;
double se3;
double si3;
double sl3;
double sgh3;
double sh3;
double sl4;
double sgh4;
double ee2;
double e3;
double xi2;
double xi3;
double xl2;
double xl3;
double xl4;
double xgh2;
double xgh3;
double xgh4;
double xh2;
double xh3;
/*
* used during DeepSpaceCalcDotTerms()
*/
double d2201;
double d2211;
double d3210;
double d3222;
double d4410;
double d4422;
double d5220;
double d5232;
double d5421;
double d5433;
double del1;
double del2;
double del3;
};
struct IntegratorConstants {
/*
* integrator constants
*/
double xfact;
double xlamo;
/*
* integrator values for epoch
*/
double xndot_0;
double xnddt_0;
double xldot_0;
};
struct IntegratorParams {
/*
* integrator values
*/
double xli;
double xni;
double atime;
/*
* itegrator values for current d_atime_
*/
double xndot_t;
double xnddt_t;
double xldot_t;
};
private:
void Initialize();
void DeepSpaceInitialize(const double& eosq, const double& sinio, const double& cosio, const double& betao,
const double& theta2, const double& betao2,
const double& xmdot, const double& omgdot, const double& xnodot);
void DeepSpaceCalculateLunarSolarTerms(const double t, double* pe, double* pinc,
double* pl, double* pgh, double* ph) const;
void DeepSpacePeriodics(const double& t, double* em, double* xinc,
double* omgasm, double* xnodes, double* xll) const;
void DeepSpaceSecular(const double& t, double* xll, double* omgasm,
double* xnodes, double* em, double* xinc, double* xn) const;
void FindPositionSDP4(Eci* eci, double tsince) const;
void FindPositionSGP4(Eci* eci, double tsince) const;
void CalculateFinalPositionVelocity(Eci* eci, const double& tsince, const double& e,
const double& a, const double& omega, const double& xl, const double& xnode,
const double& xincl, const double& xlcof, const double& aycof,
const double& x3thm1, const double& x1mth2, const double& x7thm1,
const double& cosio, const double& sinio) const;
void DeepSpaceCalcDotTerms(double* xndot, double* xnddt, double* xldot) const;
void DeepSpaceIntegrator(const double delt, const double step2,
const double xndot, const double xnddt, const double xldot)const;
void Reset();
bool first_run_;
bool use_simple_model_;
bool use_deep_space_;
struct CommonConstants common_consts_;
struct NearSpaceConstants nearspace_consts_;
struct DeepSpaceConstants deepspace_consts_;
struct IntegratorConstants integrator_consts_;
mutable struct IntegratorParams integrator_params_;
/*
* these variables are set at the very start
* and should not be changed after that
*/
double mean_anomoly_;
double ascending_node_;
double argument_perigee_;
double eccentricity_;
double inclination_;
double mean_motion_;
double bstar_;
double recovered_semi_major_axis_;
double recovered_mean_motion_;
double perigee_;
double period_;
Julian epoch_;
};
#endif