首页 | 本学科首页   官方微博 | 高级检索  
     

主动磁控微卫星姿态控制
引用本文:刘海颖,王惠南,程月华. 主动磁控微卫星姿态控制[J]. 应用科学学报, 2007, 25(4): 377-381
作者姓名:刘海颖  王惠南  程月华
作者单位:1. 南京航空航天大学,自动化学院,江苏,南京,210016;南京航空航天大学,高新院微小卫星研究中心,江苏,南京,210016
2. 南京航空航天大学,自动化学院,江苏,南京,210016
3. 南京航空航天大学,高新院微小卫星研究中心,江苏,南京,210016
基金项目:高等学校博士学科点专项科研项目
摘    要:采用偏置动量轮加磁力矩器作为控制方案的非重力梯度微卫星不同于通常的速率阻尼—姿态捕获—动量轮起旋控制模式.针对这一问题,该文提出了B-DOT磁控加动量轮常值起旋、主动磁控加常值动量轮进行姿态捕获和稳定控制的方法,设计了限制姿态反馈控制律进行捕获和稳定控制,以及LQG稳定控制律.采用磁场测量与磁控分时处理的策略,考虑测量误差和干扰力矩,以及不同偏置动量进行仿真.结果表明该方法使整个控制过程操作简捷,初态控制阶段时间显著减少,稳态阶段具有较高的控制精度和抗干扰能力.

关 键 词:微卫星  主动磁控  B-DOT控制  限制姿态反馈  LQG控制
文章编号:0255-8297(2007)04-0377-05
修稿时间:2006-11-272007-03-02

Attitude Control of Micro-satellite with Active Magnetic Control
LIU Hai-ying,WANG Hui-nan,CHENG Yue-hua. Attitude Control of Micro-satellite with Active Magnetic Control[J]. Journal of Applied Sciences, 2007, 25(4): 377-381
Authors:LIU Hai-ying  WANG Hui-nan  CHENG Yue-hua
Affiliation:1. College of Automatic Control, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;2. Academy of Frontier Science, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:Different from the normal sequence consisting of attitude detumble,acquisition,and wheel speed-up,a method of attitude acquisition and stabilization for magnetic controlled micro-satellite is proposed,which uses B-dot controller,momentum wheel acceleration for detumble and active magnetic controller,and constant wheel.A limiting attitude feedback controller is designed for attitude capture and stabilization,and a LQG controller for attitude stabilization.Simulation is carried out using magnetic determination and control at different time.Measurement error,disturber moment and different bias momentum are considered.The result indicates that the method makes the control process simple and convenient,and can reduce initial control time with high control precision and robustness in stabilization.
Keywords:micro-satellite  active magnetic control  B-DOT controller  limiting attitude feedback  LQG controller
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号