Orbit Equations of Motion
[Orbit Toolkit]


Functions

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.

Function Documentation

Vector TwoBodyDynamics (  const ssfTime &  _time,
const Vector &  _integratingState,
Orbit *  _pOrbit,
Attitude *  _pAttitude,
const Matrix &  _parameters,
const Functor &  _forceFunctorPtr
)  [static]
 

Orbit equation of motion using position and velocity.

Calculate the new time rate of change of state (position & velocity) using two-body dynamics with disturbance forces

The returned state vector is:

Parameters:
_time current time (in seconds)
_state vector of states, (kilometers, kilometers/second)
_pOrbit pointer to the current Orbit instance
_pAttitude pointer to the current Attitude instance
_parameters additional parameters for integration
_forceFuncPtr pointer to the force calculating function
Returns:
6x1 vector of time derivatives of state

Definition at line 71 of file TwoBodyDynamics.h.

Generated on Wed Aug 6 12:59:11 2003 for Open-Sessame Framework by doxygen1.3