Abstract:<p>Robust control is essential to the flapping wing micro aerial vehicle (FWMAV) due to model uncertainties, environmental or self changes during flight, such as the change of drag coefficient caused by airflow and the asymmetric effect caused by wing damage. This paper proposes a robust H∞ controller synthesis scheme for parameter-varying FWMAV systems with sampling measurement and control input saturation. A linear parameter varying (LPV) model is established to characterize the nonlinear FWMAV model w… Show more
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