TY - GEN
T1 - A pose estimation method based on RGB-D system in the process of attaching asteroids
AU - Zhang, He
AU - Zheng, Yin
AU - Wang, Yan
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - Based on RGB-D system, a pose estimation algorithm framework integrating point cloud normal vector information, point cloud information and two-dimensional gray information is designed to solve the relative pose between spacecraft and non-cooperative target interest surface (NCTIS) during attaching asteroids. First, the framework fuses the organized point cloud obtained by the TOF (time of flight) camera with the color image to obtain the organized RGB-D point cloud data. Then, the normal vector feature of the point cloud is extracted and fused with the gray image information to perform variable scale template matching to track the NCTIS. The matching algorithm considering the normal vector feature improves the robustness and accuracy of the matching results. Finally, the relative pose between NCTIS and the spacecraft is estimated in real-time by the MRPs kinematics model based on the normal vector of NCTIS and the Kalman filter. The effectiveness of the proposed algorithm framework is verified by ground experiments, and the accuracy and real-time performance of pose estimation meet the mission requirements.
AB - Based on RGB-D system, a pose estimation algorithm framework integrating point cloud normal vector information, point cloud information and two-dimensional gray information is designed to solve the relative pose between spacecraft and non-cooperative target interest surface (NCTIS) during attaching asteroids. First, the framework fuses the organized point cloud obtained by the TOF (time of flight) camera with the color image to obtain the organized RGB-D point cloud data. Then, the normal vector feature of the point cloud is extracted and fused with the gray image information to perform variable scale template matching to track the NCTIS. The matching algorithm considering the normal vector feature improves the robustness and accuracy of the matching results. Finally, the relative pose between NCTIS and the spacecraft is estimated in real-time by the MRPs kinematics model based on the normal vector of NCTIS and the Kalman filter. The effectiveness of the proposed algorithm framework is verified by ground experiments, and the accuracy and real-time performance of pose estimation meet the mission requirements.
KW - Non-cooperative target
KW - Pose estimation
KW - RGB-D system
KW - Surface normal vector
UR - https://www.scopus.com/pages/publications/85200389959
U2 - 10.1109/CCDC62350.2024.10587422
DO - 10.1109/CCDC62350.2024.10587422
M3 - 会议稿件
AN - SCOPUS:85200389959
T3 - Proceedings of the 36th Chinese Control and Decision Conference, CCDC 2024
SP - 4674
EP - 4680
BT - Proceedings of the 36th Chinese Control and Decision Conference, CCDC 2024
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 36th Chinese Control and Decision Conference, CCDC 2024
Y2 - 25 May 2024 through 27 May 2024
ER -