Effect of Asymmetric Control Constraints on Fixed-Wing UAV Trajectories
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DOI: 10.1109/taes.2018.2871435
Abstract: Reference trajectories, for the longitudinal states of a fixed-wing unmanned aerial vehicle subjected to asymmetric control constraints, are distinguished using the characteristics of regions of asymptotic stability calculated as ellipsoidal domains by solving linear matrix… read more here.
Keywords: effect asymmetric; fixed wing; control constraints; constraints fixed ... See more keywords