What is it about?
An adaptive moment distribution control logic is derived for a micro-satellite with reaction-wheel-assembly jitter disturbances. Specifically, an adjustment in the allocation of the attitude control torques is made according to the current speed of each reaction wheel.
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This page is a summary of: Adaptive Momentum Distribution Jitter Control for Microsatellite, Journal of Guidance Control and Dynamics, March 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g003909.
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