The present study investigates a novel short-wing quadplane UAV, establishing its kinematic and dynamic models while considering corrections to the rotor model under various inflow conditions. Additionally, longitudinal trim is conducted for the UAV, and linearization is performed using small perturbation principles near the equilibrium state. Subsequently, modal analysis is carried out. Finally, numerical simulations are conducted to examine the operational status of the rotors during horizontal forward flight.
Modeling and Analysis of Short-Wing Quadplane UAVs
Lect. Notes Electrical Eng.
International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024
2025-03-02
15 pages
Article/Chapter (Book)
Electronic Resource
English
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