testAttitudeIntegration.cpp File Reference


Detailed Description

Sample of an attitude integration using components of the SSF.

Author:
Author
nilspace
Version:
Revision
1.5
Date:
Date
2003/05/22 14:48:11

Definition in file testAttitudeIntegration.cpp.

#include "Matrix.h"
#include "RungeKuttaIntegrator.h"
#include "LinearInterpolator.h"
#include "Plot.h"
#include "Attitude.h"
#include "AttitudeState.h"
#include <vector.h>

Go to the source code of this file.

Functions

Vector NullFunctor (const ssfTime &_pSSFTime, const OrbitState &_pOrbitState, const AttitudeState &_pAttitudeState)
Vector AttituteDynamics (const ssfTime &_time, const Vector &_integratingState, Orbit *_pOrbit, Attitude *_pAttitude, const Matrix &_parameters, const Functor &_forceFunctorPtr)
 Dynamic and Kinematic attitude equations using quaternion and angular velocities.

int main ()


Function Documentation

Vector NullFunctor const ssfTime &  _pSSFTime,
const OrbitState &  _pOrbitState,
const AttitudeState &  _pAttitudeState
 

Definition at line 23 of file testAttitudeIntegration.cpp.

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

Dynamic and Kinematic attitude equations using quaternion and angular velocities.

Definition at line 56 of file testAttitudeIntegration.cpp.

int main  ) 
 

Definition at line 90 of file testAttitudeIntegration.cpp.


Generated on Wed Aug 6 12:58:58 2003 for Open-Sessame Framework by doxygen1.3