2010 IEEE/ASME International Conference on Advanced Intelligent Mechatronics 2010
DOI: 10.1109/aim.2010.5695796
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Fault-tolerant pose estimation of space objects

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Cited by 8 publications
(3 citation statements)
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“…The pose estimation of uncooperative space objects is a key technology for many space missions such as target recognition and on-orbit service [1,2]. In contrast to other state-of-the-art systems, a monocular camera ensures pose estimation under low power and low hardware complexity [3].…”
Section: Introductionmentioning
confidence: 99%
“…The pose estimation of uncooperative space objects is a key technology for many space missions such as target recognition and on-orbit service [1,2]. In contrast to other state-of-the-art systems, a monocular camera ensures pose estimation under low power and low hardware complexity [3].…”
Section: Introductionmentioning
confidence: 99%
“…Because of the merits of non-contact, low power consumption, high accuracy and efficiency, the poseestimation based on vision become the most suitable solution for the near-range phase of ARD.In their paper, NK Philip and MR Ananthasayanamdescribed a scheme of relative position control based on phase-plane control technique and relative attitude control based on relative quaternion feedback and obtained good result [3] .V.Lepetit introduced a non-iterative solution to the PnP problem,which is superior in its rapidity and accuracy to the other iterative techniques [4] .C. P. Lu regarded the relative pose estimation as a minimization problem of the object-space collinear error and proposed a fast orthogonal iterative (OI) algorithm with well global convergence [5] .Thienel and his colleagues devised a non-linear method to estimate the pose of spacecraftand carried out some tests of tracking controls, but its disadvantage lies in that muchpriorknowledge is needed [6] .Khansari-Zadeh proposed a new algorithm of estimation and navigation with vision information based on neural networks, and its accuracy and robustness were verified via a detailed modeling and simulation,and validated through a complete virtual environment based on the six degrees of freedom (6-DOF) nonlinear aircraft dynamical system in an autonomous aerial refueling (AAR) mission [7][8] .Farhad Aghiliand his companionspresented a fault-tolerant estimation method for the pose of space objects using 3-D vision data by integrating Kalman filter (KF) with an algorithm of Iterative Closest Point (ICP) in a closed-loop configuration [9] , in which the Euler-Hill Equations are employed to derive a discrete-time model so as to open out the evolution process of the relative translational motion of a tumbling target satellite with respect to a chaser satellite which is freely falling in a nearby orbit.Daero Lee, Henry Pernicka presented a new approach based on the unscented Kalman filterand got more robust results than the extended Kalman filter [10] . S. S. Mehta and P. Barooah developed a novel method to obtain a refined poseestimationfrom two views captured by a calibrated monocular camera.…”
Section: Introductionmentioning
confidence: 99%
“…Frame-to-frame object tracking with ICP should be fed from independent pose estimates. Some have used the navigation filter's propagated pose as an initial input to ICP [41], but this is inherently dangerous for two reasons.…”
Section: Uncorrelated Pose Estimates In Navigation Filtersmentioning
confidence: 99%