Attitude Performance of the Spacecraft Combined Energy and Attitude Control System

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

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

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 configura- tion on a spacecraft is identified.

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