Hybrid control and steering logic for the CMG-based spacecraft attitude control system

Abstract

Considering the momentum singularity characteristics, an integrated control strategy for the control moment gyros based attitude control systems is proposed, in which the angular momentum conservation between the spacecraft and the CMG is utilized to improved the system performance both in the closed loop responsiveness and the singularity controllability… (More)
DOI: 10.1109/CCA.2015.7320712

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