Robust Flight Control Law Development for Tiltrotor Conversion
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx5/5335880/5335881/05335887.pdf?arnumber=5335887
Cited by 4 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
1. Numerical Simulation on Aerodynamic Characteristics of Transition Section of Tilt-Wing Aircraft;Aerospace;2024-04-06
2. Development of Multimode Flight Transition Strategy for Tilt-Rotor VTOL UAVs;Drones;2023-09-14
3. Review of designs and flight control techniques of hybrid and convertible VTOL UAVs;Aerospace Science and Technology;2021-11
4. Trajectory tracking controller design using neural networks for a tiltrotor unmanned aerial vehicle;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2010-08-01
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