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Full Length Article | Open Access

Non-cooperative target recognition and relative motion estimation with inertial measurement unit assistance

Xiangtian ZHAOaShiqiang WANGbChao ZHANGcShijie ZHANGa,d( )Yafei ZHAOa
State Key Laboratory of Networking and Switching Technology, Beijing University of Posts and Telecommunications, Beijing 100876, China
Beijing Institute of Remote Sensing Equipment, Beijing 100854, China
Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150080, China
Yinhe Hangtian (Beijing) Communication Technology Co. Ltd., Beijing 100192, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

This study investigated the problems of non-cooperative target recognition and relative motion estimation during spacecraft rendezvous maneuvers. A structure integrating an Inertial Measurement Unit (IMU) and a visual camera was presented. The angular velocity output of the IMU was used to calculate the motion trajectories of star points in multiple image frames, which can highlight the motion of non-cooperative targets with respect to the image background to improve the probability of target recognition. To solve the problem of target misidentification caused by new star points entering the field of view, a target-tracking link based on IMU prediction was introduced to track the position of the target in the image. Furthermore, a measurement model was constructed using the line-of-sight vector generated from target recognition, and the relative motion state was estimated using a Huber-based non-linear filter. Semi-physical and numerical simulations were performed to evaluate the effectiveness and efficiency of the proposed method.

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Chinese Journal of Aeronautics

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Cite this article:
ZHAO X, WANG S, ZHANG C, et al. Non-cooperative target recognition and relative motion estimation with inertial measurement unit assistance. Chinese Journal of Aeronautics, 2025, 38(4). https://doi.org/10.1016/j.cja.2024.09.031

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Received: 27 March 2024
Revised: 05 May 2024
Accepted: 07 July 2024
Published: 24 September 2024
© 2024 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).