Attitude Performance of the Spacecraft Combined Energy and Attitude Control System

R. Varatharajoo; M. N. F. Abdullah (2004), JBIS, 57, 237-241

Refcode: 2004.57.237
Keywords: Onboard errors, attitude control, CEACS

Abstract:
An attitude control architecture is proposed for the combined energy and attitude control system (CEACS), which operates in a speed control mode. The non-ideal CEACS attitude performance is deeply investigated herein. In this regard, numerical treatments are performed profoundly, and the most critical CEACS configuration on a spacecraft is identified.