Attitude Performance of the Spacecraft Combined Energy and Attitude Control System

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Author - R. Varatharajoo et al

Co-Author(s) - R. Varatharajoo; M. N. F. Abdullah

JBIS Volume # - 57

Page # - 237-241

Year - 2004

Keywords - Onboard errors, attitude control, CEACS

JBIS Reference Code # - 2004.57.237

Number of Pages - 5

[edit] 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 configura- tion on a spacecraft is identified.


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