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김영환(Y. H. Kim),이준희(J. H. Lee),전재혁(J. H. Jeon),김종암(C. Kim),신상준(S. J. Sh),김상용(S. Y. Kim) 대한기계학회 2015 대한기계학회 춘추학술대회 Vol.2015 No.11
This paper presents the design and experimental results of the insect-mimicking Flapping-Wing Micro Air Vehicle (FWMAV) mechanism utilizing a six-bar linkage. The designed mechanism enables to radically change the wing trajectory in limited fuselage spaces through a small alteration in the location of the joint. We mapped this wing trajectory in order to implement the concept of fully-controlled the FWMAV by using RecurDyn; a multi-body dynamics analysis software. The multi-body dynamic analysis allowed us to predict the amount of stress existing in each link prior to fabrication, enabling the construction of a more reliable component. As a result, possible operational errors during the production process were minimized. A test-bed was constructed to validate the assembled FWMAV’s performance, where the FWMAV’s aerodynamic forces and moments were confirmed through the experiment.