航空学报 > 1993, Vol. 14 Issue (1): 99-103

一种新的自适应滑动模控制器设计方法

孙富春1, 孙增圻2   

  1. 1. 每军工程学院301教研究室,烟台 264001;2. 青华大学计算机系 ,北京 100084
  • 收稿日期:1991-04-17 修回日期:1992-10-15 出版日期:1993-01-25 发布日期:1993-01-25

A NEW ADAPTIVE CONTROLLER DESIGN APPROACH BASED ON ARMA MODEL

Sun Fu-chun1, Sun Zeng-qi2   

  1. 1. Faculty 301 of Naval Aeronautical Engineering Institute, Yantai, 264001;2. Department of Computer, Tsinghua University, Beijing, 100084
  • Received:1991-04-17 Revised:1992-10-15 Online:1993-01-25 Published:1993-01-25

摘要: 基于ARMA模型研究了一类具有输出反馈的离散系统滑动模变结构控制方法,提出的算法将滑动模变结构控制与系统的参数辨识结合在一起,从而使设计系统具有较强的自适应性和鲁棒性。提出方法的可行性和优化性通过一实例获得验证。

关键词: 离散系统, 滑动模控制, 自适应

Abstract: Based on ARMA model, a sliding mode controller design approach for discrete-time system using output feedback is developed in this paper, which can be considered as the extension of the variable structure system design approach for continuous-time systems to discrete-time system. This paper also deals with the effect of the introduction of quasi-sliding mode on system performance, and establishes the dynamic balance conditions. Combining the approach proposed in this paper and system parameter identification, the system performance is further improved. Finally, the effectiveness and the good performance of the design approach are examined by a numerical example.

Key words: discrete-time systems, the sliding mode control, adaptiveness