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A 6-DOF Navigation Method based on Iterative Closest Imaging Point Algorithm

机译:基于迭代最近成像点算法的六自由度导航方法

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摘要

To achieve six degree-of-freedom autonomous navigation of an inboard spacecraft, a novel algorithm called iterative closest imaging point (ICIP) is proposed, which deals with the pose estimation problem of a vision navigation system (VNS). This paper introduces the basics of the ICIP algorithm, including mathematical model, algorithm architecture, and convergence theory. On this basis, a navigation method is proposed. This method realizes its initialization using a Gaussian mixture model-based Kalman filter, which simultaneously solves the 3D-to-2D point correspondences and the camera pose. The initial value sensitivity, computational efficiency, robustness, and accuracy of the proposed navigation method are discussed based on simulation results. A navigation experiment verifies that the proposed method works effectively. The three-axis Euler angle accuracy is within 0.19° (1σ), and the three-axis position accuracy is within 1.87?mm (1σ). The ICIP algorithm estimates the full-state pose by merely finding the closest point couples respectively form the images obtained by the VNS and predicted at an initial value. Then the optimized solution of the imaging model is iteratively calculated and the full-state pose is obtained. Benefiting from the absence of a requirement for feature matching, the proposed navigation method offers advantages of low computational complexity, favorable stability, and applicability in an extremely simple environment in comparison with conventional methods.
机译:为了实现机载航天器的六自由度自主导航,提出了一种称为迭代最近成像点(ICIP)的新颖算法,该算法解决了视觉导航系统(VNS)的姿态估计问题。本文介绍了ICIP算法的基础知识,包括数学模型,算法体系结构和收敛理论。在此基础上,提出了一种导航方法。该方法使用基于高斯混合模型的卡尔曼滤波器来实现其初始化,该滤波器同时求解3D到2D点的对应关系和相机姿态。基于仿真结果,讨论了所提出的导航方法的初始值敏感性,计算效率,鲁棒性和准确性。导航实验验证了该方法的有效性。三轴欧拉角精度在0.19°(1σ)之内,三轴位置精度在1.87?mm(1σ)之内。 ICIP算法仅通过查找分别形成由VNS获得并以初始值预测的图像的最接近点对来估计全态姿势。然后,迭代计算成像模型的优化解,并获得全态姿势。与传统方法相比,受益于对特征匹配的需求,所提出的导航方法具有计算复杂度低,有利的稳定性以及在极其简单的环境中的适用性的优点。

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