Flight Control of Tilt Rotor UAV During Transition Mode Based on Finite-Time Control Theory-Reference-Cited by-同舟云学术

Flight Control of Tilt Rotor UAV During Transition Mode Based on Finite-Time Control Theory

Published:2018-12-25 Issue: Volume: Page:65-77
ISSN:2194-5357
Container-title:Proceedings of the Fifth Euro-China Conference on Intelligent Data Analysis and Applications
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Author:

Yang Hang,Lin Huangxing,Wang Jingyao,Zeng Jianping

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-030-03766-6_8

Reference15 articles.

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3. Ahn, O., Kim, J.M., Lim, C.H.: Smart UAV research program status update: achievement of tilt-rotor technology development and vision ahead. In: ICAS 2010, 27th Congress of International Council of the Aeronautical Sciences (2010)

4. Fu, R., Sun, H.F., Zeng, J.P.: Exponential stabilisation of nonlinear parameter-varying systems with applications to conversion flight control of a tilt rotor aircraft. Int. J. Control, 1–11 (2018)

5. Sato, M., Muraoka, K.: Flight controller design and demonstration of quad-tilt-wing unmanned aerial vehicle. J. Guid. Control Dyn. 38(6), 1071–1082 (2014)

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