旋转失效卫星的运动观测及消旋接触方案设计

Yue Zang, Quan Hu*, Yao Zhang, Quan An, Hongbo Wang

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

3 引用 (Scopus)

摘要

Based on the detumbling of a rotating failed satellite, a feature point motion tracking recognition method with dual optical flow constraints is proposed. By using binocular vision, this method can observe the motion of the non cooperative rotating failed satellite, and provide a contact scheme for the detumbling operation of the manipulator. Firstly, the feature points that can be stably tracked in the sequence images are identified, and their trajectories are recorded. The change frequency of the feature point trajectory is detected by the frequency domain analysis method, so as to obtain the target rotation angular velocity. The effectiveness of the proposed target motion observation method is verified by the ground physical experiments. Then, according to the trajectories of the tracked feature points, the motion envelope of the target and the appropriate contact area of the target surface are analyzed. According to the motion characteristics of the target and the time constraints for the detumbling operation, the contact strength constraints to complete the detumbling are given, and then the operational performance requirements of the manipulator are obtained, which provides a reference for the engineering application of contact detumbling.

投稿的翻译标题Motion Observation and Contact Scheme Design for Detumbling Rotating Failed Satellites
源语言繁体中文
页(从-至)930-937
页数8
期刊Yuhang Xuebao/Journal of Astronautics
43
7
DOI
出版状态已出版 - 7月 2022

关键词

  • Binocular vision
  • Contact detumbling
  • Failed satellite
  • Motion observation

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