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A simple velocity-free controller for attitude regulation of a spacecraft with delayed feedback

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3 Author(s)
A. Ailon ; Dept. of Electr. & Comput. Eng., Ben Gurion Univ. of the Negev, Beer Sheva, Israel ; R. Segev ; S. Arogeti

In this note, we consider the application of a velocity-free controller for attitude regulation of a rigid spacecraft with gas jet actuators when the effects of time-delays in the feedback loop are taken into consideration. Simple sufficient conditions for exponential stability are presented. Some structural properties of the resulting closed-loop system are studied, and relevant design tools are demonstrated.

Published in:

IEEE Transactions on Automatic Control  (Volume:49 ,  Issue: 1 )