TwoBodyDynamics.h File Reference

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Detailed Description

Dynamic equations and forces of two-body motion.

Author:

Author

nilspace

Version:

Revision

1.7

Date:

Date

2003/06/12 18:02:37

Definition in file TwoBodyDynamics.h.

#include "matrix/Matrix.h"
#include "Integrator.h"
#include "Time.h"
#include "Orbit.h"
#include "OrbitState.h"
#include "Attitude.h"
#include <vector.h>

Go to the source code of this file.

Functions
void	PositionVelocityConvFunc (const Matrix &_meshPoint, OrbitState &_convertedOrbitState)
	Orbit state conversion function from Position and Velocity state vector. TwoBodyDynamics.
Vector	TwoBodyDynamics (const ssfTime &_time, const Vector &_integratingState, Orbit *_pOrbit, Attitude *_pAttitude, const Matrix &_parameters, const Functor &_forceFunctorPtr)
	Orbit equation of motion using position and velocity.

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Function Documentation

void PositionVelocityConvFunc (  const Matrix &  _meshPoint, OrbitState &  _convertedOrbitState )  [static]

Orbit state conversion function from Position and Velocity state vector. TwoBodyDynamics. This function converts a matrix of states from the TwoBodyDynamics right-hand side function into an OrbitState object. This conversion function is necessary for propagators to store to an OrbitHistory object regardless of the equations of motion state vector being used. Parameters: _meshPoint  State vector from integration mesh point, [Position (3), Velocity (3)]. _convertedOrbitState  OrbitState object that is converted from the mesh point vector. This function just sets the position and velocity state representation and requires the user to set the corresponding reference frame. Definition at line 36 of file TwoBodyDynamics.h.

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