Propagate an orbit. More...

#include <ons_orbit_propagation.h>

Public Member Functions
	orbit_propagation ()
	Constructor. More...

	~orbit_propagation ()
	Destructor. More...

void	set_integrator_time_info (ml_matrix t, double jd_start)
	Sets the integrator times and julian date. More...

void	set_observation_time_info (ml_matrix tObs)
	Sets the observation times. More...

void	set_acceleration_info (ml_matrix tAcc, ml_matrix accel)
	Sets the acceleration history and times. More...

void	merge_integrator_time (ml_matrix tNew)
	Merges a new time vector with the existing integrator times. More...

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)
	Sets the gravity model. More...

void	set_solar_pressure_info (double area)
	Sets the solar pressure model. More...

void	set_initial_values (const ml_matrix &x0)
	Sets the initial state. More...

void	set_ephemeris_info (const ml_matrix &mu, const ml_matrix &planet_index, char *frame, int observer)
	Sets the ephemeris. More...

ml_matrix	propagate ()
	Updates the current estimate. More...

void	print ()
	Updates the current estimate. More...

ml_matrix	right_hand_side (ml_matrix x, double t, ml_matrix appAcc)
	Dynamical equations right hand side. More...

Detailed Description

Propagate an orbit.

Constructor & Destructor Documentation

◆ orbit_propagation()

orbit_propagation::orbit_propagation ( )

Constructor.

◆ ~orbit_propagation()

orbit_propagation::~orbit_propagation ( )

Destructor.

Member Function Documentation

◆ merge_integrator_time()

void orbit_propagation::merge_integrator_time ( ml_matrix tNew )

Merges a new time vector with the existing integrator times.

◆ print()

void orbit_propagation::print ( )

Updates the current estimate.

◆ propagate()

ml_matrix orbit_propagation::propagate ( )

Updates the current estimate.

◆ right_hand_side()

ml_matrix orbit_propagation::right_hand_side	(	ml_matrix	x,
		double	t,
		ml_matrix	appAcc
	)

Dynamical equations right hand side.

◆ set_acceleration_info()

void orbit_propagation::set_acceleration_info	(	ml_matrix	tAcc,
		ml_matrix	accel
	)

Sets the acceleration history and times.

◆ set_ephemeris_info()

void orbit_propagation::set_ephemeris_info	(	const ml_matrix &	mu,
		const ml_matrix &	planet_index,
		char *	frame,
		int	observer
	)

Sets the ephemeris.

◆ set_initial_values()

void orbit_propagation::set_initial_values ( const ml_matrix & x0 )

Sets the initial state.

◆ set_integrator_time_info()

void orbit_propagation::set_integrator_time_info	(	ml_matrix	t,
		double	jd_start
	)

Sets the integrator times and julian date.

◆ set_observation_time_info()

void orbit_propagation::set_observation_time_info ( ml_matrix tObs )

Sets the observation times.

◆ set_solar_pressure_info()

void orbit_propagation::set_solar_pressure_info ( double area )

Sets the solar pressure model.

◆ set_spherical_harmonic_info()

void orbit_propagation::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
	)

Sets the gravity model.

The documentation for this class was generated from the following file:

ons_orbit_propagation.h

Public Member Functions