SimulationFramework/sccontrol/sc__orbit__mnvr_8h_source.html

/*

 * orbit_mnvr.h

 *

 * Programmers: Mike Paluszek, Stephanie Thomas

 *20141999-2006, Princeton Satellite Systems. All rights reserved.

 *

 * Orbit maneuver functions. Primarily orbit mechanics.

 */


#ifndef __SC_ORBIT_MNVR__

#define __SC_ORBIT_MNVR__


#ifdef AS_OS_WINDOWS

#include "matrixlib.h"

#else

#include <MatrixLib/MatrixLib.h>

#endif


#include "sc_constants.h"


extern "C++"

{


    typedef struct lambert_out {

        ml_matrix vT;

        double a;

        double p;

        double tol;

    } lambert_out;


    lambert_out lambert_tof( const ml_matrix& r1,const ml_matrix& r2, double dT, int orbitType = 1, double mu = 3.98600436e5, double tol = 1e-10, int maxIter = 20 );


}


#endif

lambert_tof
lambert_out lambert_tof(const ml_matrix &r1, const ml_matrix &r2, double dT, int orbitType=1, double mu=3.98600436e5, double tol=1e-10, int maxIter=20)
Solves the Lambert time of flight problem using Battin's method.
Definition: sc_orbit_mnvr.cc:58

lambert_out
struct lambert_out lambert_out
Structure for storing the data output the Lambert TOF solver.

sc_constants.h
Physical and mathematical constants.

lambert_out
Structure for storing the data output the Lambert TOF solver.
Definition: sc_orbit_mnvr.h:33

lambert_out::vT
ml_matrix vT
Transfer velocity.
Definition: sc_orbit_mnvr.h:34

lambert_out::a
double a
Semi-major axis of the trajectory.
Definition: sc_orbit_mnvr.h:35

lambert_out::p
double p
The parameter for the orbit.
Definition: sc_orbit_mnvr.h:36

lambert_out::tol
double tol
Achieved tolerance.
Definition: sc_orbit_mnvr.h:37