A New structural configuration of tilting rotor unmanned aerial vehicle modeling-Reference-Cited by-同舟云学术

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A New structural configuration of tilting rotor unmanned aerial vehicle modeling

Published:2016-07 Issue: Volume: Page:
ISSN:
Container-title:2016 35th Chinese Control Conference (CCC)
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Author:

An Chen,Zhang DaiBing,Zhang JiYang,Li TengXiang

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/7547213/7553055/07553680.pdf?arnumber=7553680

Cited by 6 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. Dual-axis tilting rotor quad-plane design, simulation, flight and performance comparison with a conventional quad-plane design;2022 International Conference on Unmanned Aircraft Systems (ICUAS);2022-06-21

2. Conversion control of a tilt tri-rotor unmanned aerial vehicle with modeling uncertainty;International Journal of Advanced Robotic Systems;2021-07-01

3. Plan for the Tilt Angles of the Tilt Rotor Unmanned Aerial Vehicle Based on Gauss Pseudospectral Method;2020 13th International Symposium on Computational Intelligence and Design (ISCID);2020-12

4. A Nonlinear Robust Sliding Mode Controller with Auxiliary Dynamic System for the Hovering Flight of a Tilt Tri-Rotor UAV;Applied Sciences;2020-09-19

5. Design of Flight Control System for a Novel Tilt-Rotor UAV;Complexity;2020-03-13

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