This attribute defines the orientation method for the manuever from the reference axes to the body frame. It is valid for use with AttitudeControl: Attitude
Astrogator <Satellite Object Path> SetValue <Astrogator Object Path>.AttitudeRep <Value>
Available attitude types are:
Astrogator */Satellite/Satellite1 SetValue MainSequence.SegmentList.Maneuver.ImpulsiveMnvr.AttitudeRep EulerAngles
Astrogator */Satellite/Satellite1 SetValue MainSequence.SegmentList. Maneuver.FiniteMnvr.AttitudeRep EulerAngles
STK Programming Interface 11.0.1