Real-Time Crater-Based Monocular 3-D Pose Tracking for Planetary Landing and Navigation

被引:6
作者
Liu, Chang [1 ]
Guo, Wulong [2 ]
Hu, Weiduo [2 ]
Chen, Rongliang [1 ,3 ]
Liu, Jia [1 ,3 ]
机构
[1] Chinese Acad Sci, Shenzhen Inst Adv Technol, Shenzhen 518055, Peoples R China
[2] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[3] Shenzhen Key Lab Exascale Engn & Sci Comp, Shenzhen 510855, Peoples R China
基金
中国国家自然科学基金;
关键词
Three-dimensional displays; Real-time systems; Image edge detection; Solid modeling; Cameras; Space vehicles; Fourier series; Computer vision; crater; landing guidance; navigation; pose tracking; AUTONOMOUS NAVIGATION; INERTIAL NAVIGATION; POSITION ESTIMATION; SPACECRAFT; ALGORITHM; OPTIMIZATION; TUTORIAL; ATTITUDE;
D O I
10.1109/TAES.2022.3184660
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article proposes a vision-based framework to track the pose of lander in real time during planetary exploration with craters as landmarks. The contour of landmark crater is represented with three-dimensional Fourier series offline. During tracking, for the first instant, the tracking system is initialized by crater-based correspondence and optimization. For each subsequent instant, with the initial guess from the extended Kalman filter (EKF), the lander pose is determined by L1-norm minimization of the reprojection errors of the crater contour models in the descent image. The covariance of the determined pose is inferred based on Laplace distribution. With this covariance, the EKF generates the final estimate to pose and gives the initial guess for the pose at the next instant. Sufficient trails verify the efficacy of the proposed method.
引用
收藏
页码:311 / 335
页数:25
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