Stereo Vision-Based Relative Position and Attitude Estimation of Non-Cooperative Spacecraft

被引:7
|
作者
Chang, Liang [1 ,2 ]
Liu, Jixiu [3 ]
Chen, Zui [2 ]
Bai, Jie [1 ]
Shu, Leizheng [3 ]
机构
[1] Tongji Univ, Sch Automot Studies, Shanghai 201804, Peoples R China
[2] Chinese Acad Sci, Innovat Acad Microsatellites, CAS, Shanghai 201210, Peoples R China
[3] Chinese Acad Sci, Technol & Engn Ctr Space Utilizat, Key Lab Space Utilizat, Beijing 100094, Peoples R China
关键词
non-cooperative target; stereo vision; attitude estimation; pose measurement; KALMAN FILTER; NAVIGATION;
D O I
10.3390/aerospace8080230
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In on-orbit services, the relative position and attitude estimation of non-cooperative spacecraft has become the key issues to be solved in many space missions. Because of the lack of prior knowledge about manual marks and the inability to communicate between non-cooperative space targets, the relative position and attitude estimation system poses great challenges in terms of accuracy, intelligence, and power consumptions. To address these issues, this study uses a stereo camera to extract the feature points of a non-cooperative spacecraft. Then, the 3D position of the feature points is calculated according to the camera model to estimate the relationship. The optical flow method is also used to obtain the geometric constraint information between frames. In addition, an extended Kalman filter is used to update the measurement results and obtain more accurate pose optimization results. Moreover, we present a closed-loop simulation system, in which the Unity simulation engine is employed to simulate the relative motion of the spacecraft and binocular vision images, and a JetsonTX2 supercomputer is involved to conduct the proposed autonomous relative navigation algorithm. The simulation results show that our approach can estimate the non-cooperative target's relative pose accurately.
引用
收藏
页数:21
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