SimulateAccelerometer

This program simulate accelerometer data. The orientation of the accelerometer is given by inputfileStarCamera otherwise the celestial reference frame (CRF) is used. For computation of non-conservative forces a satelliteModel is needed.

Name	Type	Annotation
outputfileAccelerometer	filename
inputfileSatelliteModel	filename	satellite macro model
inputfileOrbit	filename
inputfileStarCamera	filename
earthRotation	earthRotation
ephemerides	ephemerides
forces	forces

This program is parallelized.