InstrumentAccelerometerApplyEstimatedParameters

This program evaluates estimated satellite parameters and writes the result to an accelerometer file.

Name	Type	Annotation
outputfileAccelerometer	filename
inputfileSatelliteModel	filename	satellite macro model
inputfileOrbit	filename
inputfileStarCamera	filename
inputfileAccelerometer	filename	add non-gravitational forces in satellite reference frame
earthRotation	earthRotation
ephemerides	ephemerides	may be needed by parametrizationAcceleration
parametrizationAcceleration	parametrizationAcceleration	orbit force parameters
inputfileParameter	filename	estimated orbit force parameters
indexStart	int	position in the solution vector
rightSide	int	if solution contains several right hand sides, select one
factor	double	the result is multiplied by this factor

This program is parallelized.