TY - GEN
T1 - Factor-Graph-Based Camera/Lidar Fusion for Defunct Spacecraft Attitude Estimation
AU - Chen, Hang
AU - Guo, Pengyu
AU - Liu, Yueyang
AU - Shao, Xiaodong
AU - Hu, Qinglei
N1 - Publisher Copyright:
© 2025 Technical Committee on Control Theory, Chinese Association of Automation.
PY - 2025
Y1 - 2025
N2 - To address the estimation accuracy degradation due to insufficient computational performance of satellite platforms that cannot meet the high-frequency sampling requirements of visual sensors, a camera/LIDAR fused relative navigation method is proposed within a graph optimization framework by exploiting the conservation of momentum. Firstly, measurement data preprocessing is conducted, where an elliptical arc recognition algorithm is used to detect circular visual features on the surface of the defunct spacecraft, obtaining camera attitude observation. Simultaneously, the Iterative Closest Point (ICP) algorithm is employed to acquire LIDAR attitude measurement data. Secondly, pseudo-measurement factors are designed for both the camera and LIDAR, and a variational integration factor is designed for the attitude increment between adjacent moments of the defunct target. Finally, a sliding-window-based factor graph optimization is performed, maintaining high estimation accuracy with lowfrequency measurements, to achieve the Maximum A Posteriori (MAP) estimation of the relative attitude of the defunct noncooperative spacecraft.
AB - To address the estimation accuracy degradation due to insufficient computational performance of satellite platforms that cannot meet the high-frequency sampling requirements of visual sensors, a camera/LIDAR fused relative navigation method is proposed within a graph optimization framework by exploiting the conservation of momentum. Firstly, measurement data preprocessing is conducted, where an elliptical arc recognition algorithm is used to detect circular visual features on the surface of the defunct spacecraft, obtaining camera attitude observation. Simultaneously, the Iterative Closest Point (ICP) algorithm is employed to acquire LIDAR attitude measurement data. Secondly, pseudo-measurement factors are designed for both the camera and LIDAR, and a variational integration factor is designed for the attitude increment between adjacent moments of the defunct target. Finally, a sliding-window-based factor graph optimization is performed, maintaining high estimation accuracy with lowfrequency measurements, to achieve the Maximum A Posteriori (MAP) estimation of the relative attitude of the defunct noncooperative spacecraft.
KW - Relative visual navigation
KW - defunct spacecraft
KW - factor graph optimization
KW - multi-sensor fusion
KW - variational integration
UR - https://www.scopus.com/pages/publications/105020283563
U2 - 10.23919/CCC64809.2025.11178757
DO - 10.23919/CCC64809.2025.11178757
M3 - 会议稿件
AN - SCOPUS:105020283563
T3 - Chinese Control Conference, CCC
SP - 4176
EP - 4181
BT - Proceedings of the 44th Chinese Control Conference, CCC 2025
A2 - Sun, Jian
A2 - Yin, Hongpeng
PB - IEEE Computer Society
T2 - 44th Chinese Control Conference, CCC 2025
Y2 - 28 July 2025 through 30 July 2025
ER -