Aerodynamic Design and Experiment for Flapping-Wing Micro Air Vehicle Using a Six-Bar Linkage

flapping-wing;MAV;six-bar linkage;wing trajectory;multi-bodi dynamics;621

공과대학 기계항공공학부 ;

University:서울대학교 대학원

关键词: flapping-wing;    MAV;    six-bar linkage;    wing trajectory;    multi-bodi dynamics;    621;   

Others  :  http://s-space.snu.ac.kr/bitstream/10371/123890/1/000000133517.pdf

美国|英语

来源: Seoul National University Open Repository

【 摘 要 】

a multibody dynamics software. Upon research of the wing trajectory, the concept of fully controlling the FWMAV was solidified. 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 and generated sufficient vertical force to carry out guided flight test.