论文

基于状态观测器的空间机械臂关节故障诊断

  • 贾庆轩 ,
  • 符颖卓 ,
  • 陈钢 ,
  • 徐文倩
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  • 北京邮电大学 自动化学院, 北京 100876

收稿日期: 2019-12-13

  修回日期: 2020-01-15

  网络出版日期: 2020-02-21

基金资助

中央高校基本科研业务费专项资金(2019PTB-012);载人航天工程预研项目(18051030101)

State observer based joint failure diagnosis of space manipulators

  • JIA Qingxuan ,
  • FU Yingzhuo ,
  • CHEN Gang ,
  • XU Wenqian
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  • School of Automation, Beijing University of Posts and Telecommunications, Beijing 100876, China

Received date: 2019-12-13

  Revised date: 2020-01-15

  Online published: 2020-02-21

Supported by

The fundamental Research Funds for the Central Universities (2019PTB-012); Research Fund of the Manned Space Engineering (18051030101)

摘要

为了实时检测空间机械臂关节故障的发生并获得有效的故障信息,提出一种基于状态观测器的关节故障诊断方法。通过结合滑模变结构控制理论设计滑模状态观测器,获得机械臂各运行状态的残差信息,并将其与设定的阈值比较,实现关节故障的检测。进而引入不同的故障模式,构建故障数据库,将实际关节故障所导致的机械臂故障残差信息与故障数据库对比,完成故障发生位置及其故障程度的识别。所提诊断方法考虑了空间机械臂系统内部强耦合特性,能够及时检测故障的发生并获取有效的故障信息。最后以7自由度空间机械臂为对象开展数值仿真研究,验证了所提关节故障诊断方法的有效性。

本文引用格式

贾庆轩 , 符颖卓 , 陈钢 , 徐文倩 . 基于状态观测器的空间机械臂关节故障诊断[J]. 航空学报, 2021 , 42(1) : 523728 -523728 . DOI: 10.7527/S1000-6893.2020.23728

Abstract

To detect the joint failure of space manipulators in real time and obtain effective fault information, a fault diagnosis method based on state observers is proposed. Through the design of a sliding mode state observer based on the sliding mode control theory, the residual information of each running status for the manipulator is obtained. A comparison of the residual information and the preset threshold is then conducted to achieve joint failure detection. In addition, different failure modes are introduced to build a failure database with which the residual information of the manipulator caused by the actual joint failure is compared, thereby realizing the location and degree identification of the failure. Taking the strong coupling characteristics of the space manipulator into account, the fault diagnosis method proposed in this paper can detect the joint failure in time and obtain effective fault information. The effectiveness and correctness of the proposed method is verified by numerical simulation of a 7-DOF space manipulator.

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