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Autonomous assembly with collision avoidance of a fleet of flexible spacecraft based on disturbance observer

机译:基于干扰观测器的挠性航天器舰队的自动避碰自动组装

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摘要

This paper presents a distributed control law with disturbance observer for the autonomous assembly of a fleet of flexible spacecraft to construct a large flexible space structure. The fleet of flexible spacecraft is driven to the pre-assembly configuration firstly, and then to the desired assembly configuration. A distributed assembly control law with disturbance observer is proposed by treating the flexible dynamics as disturbances acting on the rigid motion of the flexible spacecraft. Theoretical analysis shows that the control law can actuate the fleet to the desired configuration. Moreover, the collision avoidance between the members is also considered in the process from initial configuration to pre-assembly configuration. Finally, a numerical example is presented to verify the feasibility of proposed mission planning and the effectiveness of control law.
机译:本文提出了一种带有扰动观测器的分布式控制律,用于自主组装柔性航天器以构造大型柔性空间结构。首先将挠性航天器的舰队驱动到预组装配置,然后再驱动到所需的组装配置。通过将挠性动力学视为对挠性航天器的刚性运动产生的扰动,提出了具有扰动观测器的分布式装配控制律。理论分析表明,控制律可以使机群达到理想的构型。此外,在从初始构造到预组装构造的过程中还考虑了构件之间的避免碰撞。最后,通过数值例子验证了拟议任务计划的可行性和控制律的有效性。

著录项

  • 来源
    《Acta astronautica》 |2018年第6期|86-96|共11页
  • 作者

    Chen Ti; Wen Hao;

  • 作者单位
  • 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

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