旋转失效卫星的运动观测及消旋接触方案设计

Translated title of the contribution: Motion Observation and Contact Scheme Design for Detumbling Rotating Failed Satellites

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

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

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.

Translated title of the contributionMotion Observation and Contact Scheme Design for Detumbling Rotating Failed Satellites
Original languageChinese (Traditional)
Pages (from-to)930-937
Number of pages8
JournalYuhang Xuebao/Journal of Astronautics
Volume43
Issue number7
DOIs
Publication statusPublished - Jul 2022

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