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卫星姿态跟踪系统的鲁棒控制器设计
引用本文:李琳琳,杨国军,赵长安.卫星姿态跟踪系统的鲁棒控制器设计[J].中国航空学报,2001,14(2).
作者姓名:李琳琳  杨国军  赵长安
作者单位:School of Astronautics,Harbin Institute of Technology Harbin 150001,China
摘    要:研究了具有参数不确定性和外部干扰的卫星姿态跟踪控制问题。针对这一类多输入/多输出不确定非线性系统,提出了一个基于不确定项上界的鲁棒输出跟踪控制器设计方法。应用输入/输出反馈线性化法和李亚普诺夫方法,设计了一个控制律,它可确保系统输出按指数规律跟踪期望输出。该控制器计算简单,易于实现。仿真结果表明:即使系统存在不确定性,仍可在闭环系统中实现精确的姿态控制。

关 键 词:卫星姿态控制  不确定非线性系统  反馈线性化  输出跟踪

Robust Controller Design for Satellite Attitude Tracking System
LI Lin-lin,YANG Guo-jun,ZHAO Chang-an.Robust Controller Design for Satellite Attitude Tracking System[J].Chinese Journal of Aeronautics,2001,14(2).
Authors:LI Lin-lin  YANG Guo-jun  ZHAO Chang-an
Abstract:The attitude tracking control problem for a satellite with parameter uncertainties and external distur- bances is considered in this paper. For this class of multi-input multi-output uncertain nonlinear systems, a design method of robust output tracking controllers is proposed based on the upper-bounds of the uncertainties. Using the input/output feedback linearization approach and Lyapunov method, a control law is designed, which guarantees .that the system output exponentially tracks the given desired output. The proposed controller is easy to compute and complement. Simulation results show that, in the closed-loop system, precise attitude control is accomplished in spite of the uncertainties in the system.
Keywords:satellite attitude control  uncertain nonlinear systems  feedback linearization  output tracking
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