Control Method of Fly-Wing UAV Based on H∞ Robust Control and Control Allocation-Reference-Cited by-同舟云学术

Control Method of Fly-Wing UAV Based on H∞ Robust Control and Control Allocation

Published:2022 Issue: Volume: Page:2213-2225
ISSN:1876-1100
Container-title:Proceedings of 2021 International Conference on Autonomous Unmanned Systems (ICAUS 2021)
language:
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Author:

Liang Zhitao,Wang Peng,Wang Jiangfeng,Jia Gaowei,Guo Zheng

Publisher

Springer Singapore

Link

https://link.springer.com/content/pdf/10.1007/978-981-16-9492-9_219

Reference12 articles.

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2. Li, J., Chen, X., Li, Y., Zhang, R.: Nonlinear robust control method for maneuver flight of flying wing UAV. J. Beijing Univ. Aeronaut. Astronaut. 44(001), 89–98 (2018)

3. Movahhed, S.R., Hamed, M.A.: Output tracking of a 6-DOF flying wing UAV in longitudinal motion using LQR optimized sliding mode control with integral action. In: 2021 7th International Conference on Control, Instrumentation and Automation (ICCIA), pp. 1–5 (2021). https://doi.org/10.1109/ICCIA52082.2021.9403604

4. Meng, X.: Research on attitude control of flying-wing UAV based on dynamic inversion method with neural network compensation structure. Navig. Positioning Timing 5(4), 49–55 (2018)

5. Zhao, X., Chen, P., Yuan, M., et al.: Method of UAV height control based on H∞ /S-plane model. Mech. Sci. Technol. Aerosp. Eng. 37(7), 1143–1148 (2018)

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