Stereovision-based Noncooperative Spacecraft Pose Measurement via Circle and Planar Points

被引:1
|
作者
Jiang, Cuicui [1 ]
Fang, Yizhong [2 ,3 ]
Ding, Guopeng [4 ,5 ]
Chen, Xin [4 ,5 ]
Mao, Qingyun [4 ,5 ]
Hu, Qinglei [1 ,6 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] State Key Lab Expt Phys & Computat Math, Beijing 100076, Peoples R China
[3] Beijing Inst Space Long March Vehicle, Beijing 100076, Peoples R China
[4] Chinese Acad Sci, Key Lab Microsatellite, Shanghai 201203, Peoples R China
[5] Chinese Acad Sci, Innovat Acad Microsatellites, Shanghai 201203, Peoples R China
[6] Beihang Univ, Beijing Adv Innovat Ctr Big Data Based Precis Med, Beijing 100191, Peoples R China
基金
北京市自然科学基金; 中国国家自然科学基金;
关键词
Noncooperative spacecraft; Stereovision; Planar points; Orthogonal iteration; SATELLITE;
D O I
10.1109/CCDC52312.2021.9602482
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
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.
引用
收藏
页码:3104 / 3109
页数:6
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