What is it about?
This paper proposes a nonlinear active fault-tolerant control law that can deal with control reversal, parametric model uncertainties, sensing errors, actuator faults, and structural damage.
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This page is a summary of: Active Fault-Tolerant Incremental Sliding-Mode Flight Control Against Control Reversal, Journal of Guidance Control and Dynamics, December 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g006690.
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