ons_orbit_propagation.h

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/*
 * sc_orbit_propagation.h 
 *
 * Copyright 2008, Princeton Satellite Systems. All rights reserved.
 *
 * Orbit propagation class.
 *
 */
 
#ifdef AS_OS_WINDOWS
#include "matrixlib.h"
#else
#include <MatrixLib/MatrixLib.h>
#endif
#include <SCControl/SCControl.h>
 
 
#ifndef __ORBIT_PROPAGATION__
#define __ORBIT_PROPAGATION__
 
class orbit_propagation {
public:
        orbit_propagation();
        ~orbit_propagation();
        void set_integrator_time_info (ml_matrix t, double jd_start );
        void set_observation_time_info (ml_matrix tObs );
        void set_acceleration_info (ml_matrix tAcc, ml_matrix accel );
        void merge_integrator_time (ml_matrix tNew );
        void set_spherical_harmonic_info  (double radius, ml_matrix s, ml_matrix c, ml_matrix j, double mu, int z_harm, int t_harm, int spherical );
        void set_solar_pressure_info ( double area );
        void set_initial_values (const ml_matrix &x0);
        void set_ephemeris_info ( const ml_matrix& mu, const ml_matrix &planet_index, char* frame, int observer );
        ml_matrix propagate ();
        void print ();
        
        ml_matrix right_hand_side( ml_matrix x, double t, ml_matrix appAcc );
        
private:
        ml_matrix t;
        double jd;
        ml_matrix tObs;
        ml_matrix tAcc;
        ml_matrix acc;
        ml_matrix x;
        int order;
        int spherical_harmonic_on;
        int solar_pressure_on;
        double area;
        ml_matrix mu;
        ml_matrix planet_index;
        gravity_t *gravity_model;
        char* frame;
        int observer;
        int center;
    
    
    galilean_moons g;
    
    int n_galilean_moons;
 
 
};
 
#endif