航空学报 > 2003, Vol. 24 Issue (6): 541-545

CMG磁悬浮转子系统的模型与控制律

俞文伯, 栾胜, 房建成   

  1. 北京航空航天大学宇航学院第五研究室 北京 100083
  • 收稿日期:2002-11-13 修回日期:2003-05-20 出版日期:2003-12-25 发布日期:2003-12-25

Model and Control Law of CMG Active Magnetic Bearing Rotor

YU Wen-bo, LUAN Sheng, FANG Jian-cheng   

  1. The Fifth Lab.; Beijing University of Aeronautics and Astronautics; Beijing 100083; China
  • Received:2002-11-13 Revised:2003-05-20 Online:2003-12-25 Published:2003-12-25

摘要: 以刚体的平动和转动为状态构造主动磁轴承(AMB) 转子控制系统模型,可以清晰反映控制力矩(CMG) 陀螺效应的影响。利用此模型,着重分析了目前常用的分散控制和分散加交叉控制方式下转子的后向涡动特征,并提出模态解耦控制的概念,指出此控制律可以根除转子的后向涡动,且具有最佳的稳定性。

关键词: 陀螺动力学, 主动磁轴承, 解耦控制

Abstract: The model of AMB rotor control system in industry can not manifest the gyro effect in CMG, so that it isinconvenient to design the control law against the rotor vortex. A system moeel based on the rotor translation androtation is introduced , and the gyro effect is clearly reflected. The backward vortex under different methods of AMBcontrol including the decentralized control and cross2feedback control are analysed. The concept of Modal DecoupleControl is put forward , and the backward vortex of rotor can be diminished at original offset situation and better stability is achieved under this control law.

Key words: gyro dynamics, active magnetic bearing, decouple control

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