35th Congress of the International Council of the Aeronautical Sciences

06.2 - Flight Dynamics and Control (UAV related)

RESEARCH ON FLIGHT DYNAMICS AND CONTROL CHARACTERISTICS OF MULTI-UAV WINGTIP-LINKED FLIGHT

R. Wang¹, Y. Wu¹, Z. Zhou¹, S. Yao¹, Z. Zhang¹; ¹Northwestern Polytechnical University, China

Focusing on the flight dynamics and control of wingtip-linked multi-UAVs, this study systematically investigates dynamic modeling, aerodynamic analysis, modal characteristics, behavioral evolution, and flight control. A universal theoretical framework applicable to arbitrary unit numbers, hinge stiffness, and flight configurations is established and validated through flight tests.


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