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Chan, W.L. (author), Nguyen, Q.V. (author), Debiasi, M. (author)
Study was conducted on the effect of wing root angle deflection to pave the way for the implementation of tailless flight control on a hovering flapping wing platform. Hypotheses of how the wing root deflection in the sagittal direction could help generate pitching and yawing moments are presented and investigated. The investigation was...
conference paper 2014