Design and control of novel tri-rotor UAV
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Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx5/6327840/6334591/06334647.pdf?arnumber=6334647
Cited by 36 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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2. Neural network-based robust adaptive super-twisting sliding mode fault-tolerant control for a class of tilt tri-rotor UAVs with unmodeled dynamics;The Aeronautical Journal;2024-04-08
3. An adaptive trajectory tracking control scheme for a novel fully actuated multirotor unmanned aerial vehicle without using velocity signals;International Journal of Adaptive Control and Signal Processing;2024-01-22
4. Investigation on the Airworthiness of a Novel Tri-Rotor Configuration for a Fixed Wing VTOL Aircraft;Volume 04 Issue 02;2023-12-30
5. Conceptual Design, Development, Test and System Identification of a Novel Tri-Rotor Configuration for a VTOL Fixed Wing Aircraft;Novel Techniques in Maintenance, Repair, and Overhaul;2023-11-23
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