06.2 - Flight Dynamics and Control (UAV related)
DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE
L. Wang¹, X. Yang¹, Y. Luo¹, H. Chen¹, J. Li¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
The anticipated outcome of this research is to establish an efficient attitude control strategy specifically for a dragonfly-inspired prototype, complete the corresponding hardware and software design of the control system, and verify its robustness through ground experiments, ultimately achieving stable control of the prototype's attitude under high-frequency flapping.