Trajectory tracking control of unmanned helicopters by using adaptive dynamic surface approach

被引:1
|
作者
He, Yue-Bang [1 ]
Pei, Hai-Long [1 ]
Ye, Xiang [1 ]
Zhang, Qian [1 ]
机构
[1] Key Laboratory of Autonomous Systems and Networked Control of the Ministry of Education, South China University of Technology, Guangzhou 510640, Guangdong
来源
Huanan Ligong Daxue Xuebao/Journal of South China University of Technology (Natural Science) | 2013年 / 41卷 / 05期
关键词
Adaptive dynamic surface control; Lyapunov stability; Trajectory tracking; Unmanned helicopter;
D O I
10.3969/j.issn.1000-565X.2013.05.001
中图分类号
学科分类号
摘要
As the existing unmanned helicopter models are of high order and great load change, a control method based on the adaptive dynamic surface approach is proposed. In this method, first, one-order linear filters are used to estimate the time derivatives of virtual control signals, thus significantly simplifying the design of the controller. Then, an on-line adaptive law is used to estimate the helicopter mass, thus guaranteeing the stability of the closed-loop system with variable load. Finally, the semi-global uniform bound of tracking errors is proved based on the Lyapunov stability theory. Simulated results indicate that the proposed method is effective and feasible.
引用
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页码:1 / 8
页数:7
相关论文
共 19 条
  • [1] Gavrilets V., Autonomous aerobatic maneuvering of miniature helicopters, pp. 31-54, (2003)
  • [2] Cai G., Chen B.M., Lee T.H., Unmanned Rotorcraft Systems, pp. 97-128, (2011)
  • [3] Tischler M.B., Aircraft and Rotorcraft System Identification, pp. 321-430, (2003)
  • [4] Kim H.J., Shim D.H., A flight control system for aerial robots: Algorithms and experiments, Control Engineering Practice, 11, 2, pp. 1389-1400, (2003)
  • [5] Gribble J.J., Linear quadratic gaussian/loop transfer recovery design for a helicopter in low-speed flight, Journal of Guidance, Control, and Dynamics, 16, 4, pp. 754-761, (1993)
  • [6] Cai G.W., Chen B.M., Dong X., Et al., Design and implementation of a robust and nonlinear flight control system for an unmanned helicopter, Mechatronics, 21, 5, pp. 803-820, (2011)
  • [7] Sun X.D., Clarke T., Application of hybrid μ/H<sub>∞</sub> control to modern helicopters, Proceedings of the International Conference on Control'94. Part2, pp. 1532-1537, (1994)
  • [8] Oosterom M., Babuska R., Design of a gain-scheduling mechanism for flight control laws by fuzzy clustering, Control Engineering Practice, 14, 7, pp. 769-781, (2006)
  • [9] Liu C., Chen W.H., John A., Tracking control of small-scale helicopters using explicit nonlinear MPC augmented with disturbance observers, Control Engineering Practice, 20, 3, pp. 258-268, (2012)
  • [10] Chen M., Ge S.S., Ren B., Robust attitude control of helicopters with actuator dynamics using neural networks, IET Control Theory and Applications, 4, 12, pp. 2837-2854, (2010)