L1 adaptive dynamic inversion attitude control for unmanned aerial vehicle with actuator failures
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DOI: 10.1177/0954410018814602
Abstract: This paper presents a hybrid attitude control scheme of L1 adaptive and dynamic inversion for unmanned aerial vehicle with actuator faults, where both gain fault and bias fault are considered. Firstly, dynamic inversion is employed… read more here.
Keywords: dynamic inversion; unmanned aerial; adaptive dynamic; aerial vehicle ... See more keywords