Hover flight control of X-shaped flapping wing aircraft considering wing–tail interactions
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DOI: 10.1016/j.ast.2021.106870
Abstract: Abstract The dynamic modelling and attitude controller design of a flapping wing aircraft, Beihawk, were investigated in this study. The aircraft features of an X-shaped flapping wing configuration, tail control surfaces installed downstream of the… read more here.
Keywords: flapping wing; control; wing tail; aircraft ... See more keywords