Composite Attitude Tracking Control for Launch Vehicles Subject to Actuator Degradation Fault and Multiple Disturbances
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DOI: 10.1109/tii.2024.3359443
Abstract: The safety and high-precision attitude control of launch vehicles are threatened by degradation fault and multiple disturbances (such as model uncertainty, uncertain inertia, and external disturbance) during the reentry stage. To address these challenges, an… read more here.
Keywords: multiple disturbances; degradation fault; control; fault multiple ... See more keywords