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A simple velocity-free controller for attitude regulation of a spacecraft with delayed feedback
Authors:Ailon   A. Segev   R. Arogeti   S.
Affiliation:Dept. of Electr. & Comput. Eng., Ben Gurion Univ. of the Negev, Beer Sheva, Israel;
Abstract: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.
Keywords:
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