Abstract Continuous momentum management for space station based on LESO
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Continuous momentum management for space station based on LESO

机译:基于LESO的空间站持续动量管理

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摘要

AbstractStrong disturbance and long life requirement of the space station make momentum management (MM) an important consideration in its design. To deal with the MM problem, this paper proposes a disturbance rejection control architecture based on the linear extended state observer (LESO) and the linear quadratic regulator (LQR) method. LESO is designed to estimate the variant disturbance of the space station. A special compensation strategy on each axis is proposed based on the working mechanism of the disturbance. The designed LESO and the closed-loop system are proved to be stable. Simulation results show that, by rejecting the strong and abrupt disturbance with higher-order cyclic terms, the proposed control scheme can achieve desirable control accuracy.
机译: 摘要 空间站的强烈干扰和长寿命要求使其成为动量管理(MM)设计中的重要考虑因素。针对MM问题,本文提出了一种基于线性扩展状态观测器(LESO)和线性二次调节器(LQR)方法的干扰抑制控制架构。 LESO旨在估算空间站的各种干扰。根据扰动的工作机理,提出了各轴的特殊补偿策略。事实证明,所设计的LESO和闭环系统是稳定的。仿真结果表明,通过用高阶循环项拒绝强烈和突然的扰动,该控制方案可以达到理想的控制精度。

著录项

  • 来源
    《Aerospace science and technology》 |2018年第1期|364-370|共7页
  • 作者单位

    School of Electrical Engineering and Intelligentization, Dongguan University of Technology;

    Department of Systems Design Engineering, University of Waterloo;

    Key Lab of Systems & Control, Academy of Mathematics and Systems Science, CAS;

    College of Automation Science and Engineering, South China University of Technology;

    Key Lab of Systems & Control, Academy of Mathematics and Systems Science, CAS,School of Mathematical Sciences, University of Chinese Academy of Sciences;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Momentum management; Attitude control; Control moment gyro; Linear extended observer;

    机译:动量管理;姿态控制;控制力矩陀螺;线性扩展观测器;

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