TY - GEN
T1 - Stereovision-based Noncooperative Spacecraft Pose Measurement via Circle and Planar Points
AU - Jiang, Cuicui
AU - Fang, Yizhong
AU - DIng, Guopeng
AU - Chen, Xin
AU - Mao, Qingyun
AU - Hu, Qinglei
N1 - Publisher Copyright:
© 2021 IEEE.
PY - 2021
Y1 - 2021
N2 - In this paper, a novel approach based on the feature circle and planar points is proposed for the relative pose measurement of the noncooperative spacecraft. Specifically, the approach uses information from the stereovision-based navigation system to provide multiple perspective projections of the circle and planar points on the noncooperative spacecraft. Then the circle center position is recovered and the normal direction is determined by duality disambiguation. Furthermore, a point depth of recovery from the stereovision is used to define the direction from the circle center to the point, which is regarded as the initial attitude for the stereovision-based orthogonal iteration pose estimation to avoid the local minimal value of the iteration method. Therefore, by utilizing the initial attitude and the orthogonal iteration algorithm based on planar points, the pose ambiguity from the planar points is eliminated and the roll angle around the circle normal direction is available. Finally, numerical simulations are conducted to validate the effectiveness of the proposed algorithm.
AB - In this paper, a novel approach based on the feature circle and planar points is proposed for the relative pose measurement of the noncooperative spacecraft. Specifically, the approach uses information from the stereovision-based navigation system to provide multiple perspective projections of the circle and planar points on the noncooperative spacecraft. Then the circle center position is recovered and the normal direction is determined by duality disambiguation. Furthermore, a point depth of recovery from the stereovision is used to define the direction from the circle center to the point, which is regarded as the initial attitude for the stereovision-based orthogonal iteration pose estimation to avoid the local minimal value of the iteration method. Therefore, by utilizing the initial attitude and the orthogonal iteration algorithm based on planar points, the pose ambiguity from the planar points is eliminated and the roll angle around the circle normal direction is available. Finally, numerical simulations are conducted to validate the effectiveness of the proposed algorithm.
KW - Noncooperative spacecraft
KW - Orthogonal iteration
KW - Planar points
KW - Stereovision
UR - https://www.scopus.com/pages/publications/85125202325
U2 - 10.1109/CCDC52312.2021.9602482
DO - 10.1109/CCDC52312.2021.9602482
M3 - 会议稿件
AN - SCOPUS:85125202325
T3 - Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021
SP - 3104
EP - 3109
BT - Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 33rd Chinese Control and Decision Conference, CCDC 2021
Y2 - 22 May 2021 through 24 May 2021
ER -