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基于干扰观测器的非线性不确定系统自适应滑模控制
引用本文:于靖,陈谋,姜长生.基于干扰观测器的非线性不确定系统自适应滑模控制[J].控制理论与应用,2014,31(8):993-999.
作者姓名:于靖  陈谋  姜长生
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(61174102); 江苏省自然科学基金资助项目(SBK20130033); 高等学校博士学科点专项科研基金资助项目 (20133218110013); 南京航空航天大学基本科研业务费资助项目(NS2013028).
摘    要:本文研究了一类基于非线性干扰观测器的多输入多输出非线性不确定系统的边界层自适应滑模控制方法并应用于近空间飞行器高精度姿态控制.考虑系统存在不确定性和外部干扰上界未知的情况,设计了基于干扰观测器的边界层自适应滑模控制器,以消除传统滑模控制中的"抖振"现象,使跟踪误差趋近于零.同时,利用李雅普洛夫方法严格证明了闭环系统的稳定性.最后将所研究的自适应滑模控制方法,应用于某近空间飞行器的姿态控制中,仿真结果表明在不确定性和外部干扰作用下能保证姿态控制的稳定性,对参数不确定具有较好的鲁棒性.

关 键 词:近空间飞行器  非线性控制  干扰观测器  滑模控制  边界层控制
收稿时间:9/2/2013 12:00:00 AM
修稿时间:3/5/2014 12:00:00 AM

Adaptive sliding mode control for nonlinear uncertain systems based on disturbance observer
YU Jing,CHEN Mou and JIANG Chang-sheng.Adaptive sliding mode control for nonlinear uncertain systems based on disturbance observer[J].Control Theory & Applications,2014,31(8):993-999.
Authors:YU Jing  CHEN Mou and JIANG Chang-sheng
Affiliation:College of Automation Engineering, Nanjing Aeronautic and Astronautic University,College of Automation Engineering, Nanjing Aeronautic and Astronautic University and College of Automation Engineering, Nanjing Aeronautic and Astronautic University
Abstract:A boundary layer adaptive sliding-mode controller is developed for a class of multi-input and multi-output (MIMO) nonlinear uncertain systems based on the nonlinear disturbance observer (NDO). The developed adaptive sliding- mode controller has been applied to the high-precision attitude control for near space vehicles. Considering the system uncertainty and the unknown upper bound of the external disturbance, we design the boundary layer adaptive sliding-mode control scheme for eliminating the chattering phenomenon appeared in the traditional sliding-mode control and making the tracking error to approach zero. The rigorous stability of the closed-loop system is proved by using the Lyapunov method. Finally, simulation results demonstrate that the proposed control scheme can achieve good control performances for the attitude control of the near space vehicle under the unknown disturbance and the system uncertainty.
Keywords:near-space vehicle  nonlinear control  disturbance observer  sliding model control  boundary layer control
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