测试技术学报2011，Vol.25Issue(6)：483-488,6.DOI:10.3969/j.issn.1671-7449.2011.06.003
控制力矩陀螺控制律设计及比较分析
Design and Comparative Analysis of Control Laws for Control Moment Gyroscope
陈钊 1杨亚非1
作者信息
- 1. 哈尔滨工业大学控制与仿真中心,黑龙江哈尔滨150080
- 折叠
摘要
Abstract
Control moment gyroscope is a commonly used controller in an attitude control system of spacecraft. Control methods research of control moment gyroscope can provide necessary theoretical basis for developing attitude control system of spacecraft. In this paper, three control laws for control moment gyroscope by successive loop closure/PD, pole placement, full state feedback linear quadratic regulator, are designed respectively, and the validity of the three methods are confirmed by controlling an actual system to meet the expected control target. The control performances of the methods are compared and analyzed, and the results of the three control strategies have provided theoretical guidance for further studies in this system.关键词
控制力矩陀螺/连续闭环/极点配置/全状态反馈线性二次型/控制方法Key words
control moment gyroscope/ successive loop closure/ pole placement/ full state feedback linear quadratic regulator/ control methods分类
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陈钊,杨亚非..控制力矩陀螺控制律设计及比较分析[J].测试技术学报,2011,25(6):483-488,6.
