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document
Nguyen, Q.-V. (author), Chan, W.L. (author), Debiasi, M. (author)
We present our insect-based hovering Flapping-Wing Micro Air Vehicle (FW-MAV) capable of sustained flight and control. The proposed design combines two fixed wings and two flapping wings to take advantage of the double clap-and-ling effects at the end of each half-stroke during one flapping cycle for high thrust production, and utilizes the...
conference paper 2014
document
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