Uncertainty and Disturbance Estimator-Based Control of a Flapping-Wing Aerial Vehicle With Unknown Backlash-Like Hysteresis
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DOI: 10.1109/tie.2019.2926055
Abstract: Robust and accurate control of a flapping-wing aerial vehicle (FWAV) system is a challenging problem due to the existence of backlash-like hysteresis nonlinearity. This paper proposes uncertainty and disturbance estimator (UDE)-based control with output feedback… read more here.
Keywords: flapping wing; control; control flapping; backlash like ... See more keywords
A simulation-based approach to modeling component interactions during design of flapping wing aerial vehicles
Sign Up to like & getrecommendations! Published in 2019 at "International Journal of Micro Air Vehicles"
DOI: 10.1177/1756829318822325
Abstract: A new flapping wing aerial vehicle (FWAV) simulation methodology is presented that combines models of the key subsystems: (1) the actuator, (2) the battery, and (3) the wings. This approach captures component interactions that are… read more here.
Keywords: system; flapping wing; wing aerial; model ... See more keywords