航空学报 > 2011, Vol. 32 Issue (5): 873-880   doi: CNKI:11-1929/V.20101213.1745.001

基于SMDO的滑模控制器设计及其在导弹上的应用

曾宪法1, 王洁瑶2, 王小虎1, 王铁军1   

  1. 1. 北京控制与电子技术研究所, 北京 100038;
    2. 哈尔滨工业大学 航天学院, 黑龙江 哈尔滨 150001
  • 收稿日期:2010-08-20 修回日期:2010-09-19 出版日期:2011-05-25 发布日期:2011-05-19
  • 通讯作者: Tel.: 010-63301556 E-mail: wangxh_lf@sina.com E-mail:wangxh_lf@sina.com
  • 作者简介:曾宪法(1982- ) 男,博士研究生。主要研究方向:飞行器制导与控制。 Tel: 010-63301461 E-mail: xianfa110@163.com王洁瑶(1988- ) 女,本科生。主要研究方向:飞行器设计。王小虎(1962- ) 男,博士,研究员,博士生导师。主要研究方向:精确制导与控制。 Tel: 010-63301556 E-mail: wangxh_lf@sina.com王铁军(1976- ) 男,博士,工程师。主要研究方向:飞行器控制。

Design of Sliding Mode Controller Based on SMDO and Its Application to Missile Control

ZENG Xianfa1, WANG Jieyao2, WANG Xiaohu1, WANG Tiejun1   

  1. 1. Beijing Institute of Control & Electronics Technology, Beijing 100038, China;
    2. School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
  • Received:2010-08-20 Revised:2010-09-19 Online:2011-05-25 Published:2011-05-19

摘要: 提出了一种基于滑模干扰观测器(SMDO)的滑模控制器(SMC)设计方法。针对一类级联多输入多输出(MIMO)非线性系统,根据奇异摄动原理将其分为内、外回路分别进行控制器设计。以外回路为例,分析了传统基于饱和函数的滑模控制的鲁棒性,针对其在面临干扰时鲁棒性较差的问题,在名义滑模控制律的基础上设计了基于超扭曲算法的SMDO以实现对干扰的估计和补偿。将该方法应用于导弹控制系统的设计中,通过仿真表明,基于SMDO的滑模控制器(SMDO-SMC)有效提高了控制系统的鲁棒性和性能。

关键词: 滑模干扰观测器, 滑模控制, 超扭曲算法, 导弹, 鲁棒控制

Abstract: A sliding mode controller (SMC) design approach based on the sliding mode disturbance observer (SMDO) is proposed. A class of cascade multiple-input multiple-output (MIMO) nonlinear system is separated into outer and inner loops based on the singular perturbation principle, and the controllers are designed in the two loops respectively. The robustness of the traditional saturation-function-based sliding mode controller is analyzed in the outer loop, and it is found to be weak in the presence of disturbances. To overcome this problem, together with the nominal sliding mode control law, SMDOs based on the super-twisting algorithm are designed to estimate and compensate for disturbances. Finally, the approach is applied to a missile control system design. The simulation results demonstrate that SMDO-based sliding mode controller (SMDO-SMC) effectively improves both the robustness and control performance of the control system.

Key words: sliding mode disturbance observer, sliding mode control, super-twisting algorithm, missiles, robust control

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