Modeling and vibration control of the flapping-wing robotic aircraft with output constraint
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DOI: 10.1016/j.jsv.2017.12.027
Abstract: Abstract In this paper, we propose the boundary control for undesired vibrations suppression with output constraint of the flapping-wing robotic aircraft (FWRA). We also present the dynamics of the flexible wing of FWRA with governing… read more here.
Keywords: wing robotic; output constraint; flapping wing; output ... See more keywords