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基于切变流形函数和模糊控制的微小卫星姿态磁控制
引用本文:李太玉,张育林. 基于切变流形函数和模糊控制的微小卫星姿态磁控制[J]. 上海航天, 2006, 23(2): 1-5
作者姓名:李太玉  张育林
作者单位:1. 上海航天技术研究院,上海,200233
2. 酒泉卫星发射中心,甘肃,酒泉,732750
摘    要:研究了一种用李亚普诺夫方法和模糊控制理论实现微小卫星姿态磁控制的方法。通过构造李亚普诺夫函数给出切变流形函数,获得了一开关控制,并从理论上证明了系统的收敛性。用模糊控制法消除常规开关控制固有的抖振,给出了模糊控制律。理论分析和仿真结果表明,该姿态磁控制方法简单、姿态精度高、鲁棒性强,可用于微小卫星的姿态磁控制。

关 键 词:微小卫星  姿态控制  磁力矩器  李亚普诺夫方法  模糊控制  抖振
文章编号:1006-1630(2006)02-0001-05
收稿时间:2005-10-13
修稿时间:2005-11-28

Magnetic Attitude Control Basing on the Sliding Mode Function and the Fuzzy Control for Microsatellite
LI Tai-yu,ZHANG Yu-lin. Magnetic Attitude Control Basing on the Sliding Mode Function and the Fuzzy Control for Microsatellite[J]. Aerospace Shanghai, 2006, 23(2): 1-5
Authors:LI Tai-yu  ZHANG Yu-lin
Affiliation:1. Shanghai Academy of Spaceflight Technology, Shanghai 200233, China; 2. Jiuquan Satellite Launch Center, Jiuquan Gansu 732750, China
Abstract:A magnetic attitude control law for microsatellite was studied using Lyapunov function and fuzzy control in this paper.The sliding module function was educed through constructing a Lyapunov function that gave a sliding function,and a switch control was gained.The convergence of the system was proved.The sliding module vibration of the switch control was eliminated using fuzzy control,and the fuzzy control law was given.The theoretical analysis and simulation results showed that the law was simple,which had advantages of high attitude precision and good robustness.The law could be used in the magnetic attitude control for microsatellte.
Keywords:Microsatellite  Attitude control  Magnetorquer  Lyapunov function  Fuzzy control  Vibration
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