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一种基于反步法的鲁棒自适应终端滑模控制
引用本文:周 丽,姜长生,都延丽.一种基于反步法的鲁棒自适应终端滑模控制[J].控制理论与应用,2009,26(6):678-682.
作者姓名:周 丽  姜长生  都延丽
作者单位:南京航空航天大学,自动化学院,江苏,南京,210016
基金项目:国家自然科学基金资助项目(90405011, 90716028).
摘    要:针对不确定严格反馈块控非线性系统, 提出了一种基于反步法的鲁棒自适应终端滑模变结构控制方法. 系统的未知不确定及外界干扰由模糊系统在线逼近, 利用反步法设计了变结构控制的终端滑模面, 并由此得到了鲁棒自适应终端滑模控制器, 使系统的跟踪误差在有限时间内趋于给定轨迹的任意小的邻域内. 通过Lyapunov定理证明了闭环系统所有信号最终有界. 对某战斗机6自由度机动仿真结果表明, 该方法具有强鲁棒性.

关 键 词:鲁棒自适应控制    反步法    终端滑模    模糊系统    机动飞行
收稿时间:2007/12/9 0:00:00
修稿时间:2009/4/27 0:00:00

A robust and adaptive terminal sliding mode control based on backstepping
ZHOU Li,JIAG Chang-sheng and DU Yan-li.A robust and adaptive terminal sliding mode control based on backstepping[J].Control Theory & Applications,2009,26(6):678-682.
Authors:ZHOU Li  JIAG Chang-sheng and DU Yan-li
Affiliation:College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing Jiangsu 210016, China;College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing Jiangsu 210016, China;College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing Jiangsu 210016, China
Abstract:A robust and adaptive terminal sliding mode control based on backstepping is presented for a general class of strict-block-feedback systems with uncertainties. Fuzzy logic systems are employed to compensate for the unknown uncertainties in the system. Adaptive backstepping method is then used to design the terminal sliding surface. A robust and adaptive variable-structure controller is thus obtained. The tracking error is driven onto the sliding surface and converges to an arbitrary small neighborhood of the desired trajectory in finite-time. Using the Lyapunov approach, we prove that all signals in the closed loop system are ultimately bounded. Finally, the simulation results of the nonlinear six-degree-offreedom maneuver flight of a fighter plane demonstrate that the proposed approach has strong robust performance.
Keywords:robust and adaptive control  backstepping  terminal sliding mode  fuzzy logic system  maneuver flight
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