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陨坑视觉导航的位姿估计误差建模OA

Modeling of pose estimation error in crater visual navigation

中文摘要英文摘要

在月球极区着陆探测任务中,基于陨坑视觉导航估计着陆器位姿可以实现高精度着陆定位.为解决陨坑视觉导航中位姿估计误差传递机理不明确、工程实用化参数缺失等关键问题,开展了陨坑视觉导航的位姿估计误差建模研究.通过提出一种基于加权最小二乘法的位姿误差模型,以估计多种因素影响下的位姿误差.首先,结合陨坑视觉导航位姿估计原理,完成位姿误差溯源分析与基础建模.其次,以重投影误差最小化为目标,构建位姿误差模型.最后,采用加权最小二乘法,完成位姿误差的定量估计.基于月球极区数字高程模型(Digital Elevation Model,DEM)和数字正射影像(Digital Orthophoto Map,DOM)数据,模拟月球着陆器的陨坑视觉导航,开展基于蒙特卡洛仿真的位姿误差估计实验,研究不同误差源和特征参数对位姿误差的影响.实验结果表明,当像素检测误差为5 pixel、陨坑数量为15时,平移误差估计值小于95 m.本文误差模型可实现多因素影响下位姿误差的定量估计,提出的工程参数方案满足月球极区着陆百米级导航精度要求,为陨坑导航方案设计提供了理论基础.

High-precision positioning is required for lunar polar landing,and crater-based visual navigation can be used to estimate the lander pose.However,this approach is limited by an insufficiently character-ized mechanism for pose estimation error propagation and by the lack of practical engineering parameters.To address these issues,pose error modeling for crater visual navigation is investigated.A pose error mod-el based on weighted least squares is proposed to quantify pose errors under the combined effects of multi-ple factors.First,traceability analysis and baseline modeling of pose errors are performed according to the pose estimation principle of crater visual navigation.Second,a pose error model is formulated by minimiz-ing the reprojection error.Finally,weighted least squares is applied to obtain quantitative pose error esti-mates.Using DEM and DOM data from the lunar polar region,crater visual navigation for a lunar lander is simulated,and Monte Carlo-based experiments are conducted to evaluate the effects of different error sources and feature parameters on pose accuracy.When the pixel detection error is 5 pixels and 15 craters are used,the estimated translation error is below 95 m.The developed model enables quantitative pose er-ror estimation under multiple contributing factors,and the proposed engineering parameter scheme satis-fies the 100 m-level navigation accuracy requirement for lunar polar landing.This work provides a theoreti-cal basis for the design of crater-based navigation schemes.

黄建斌;何云涛;王安然;李小路;徐立军

北京航空航天大学 仪器科学与光电工程学院,北京 100191北京航空航天大学 电子信息工程学院,北京 100191北京控制工程研究所,北京 100190北京航空航天大学 仪器科学与光电工程学院,北京 100191北京航空航天大学 仪器科学与光电工程学院,北京 100191

航空航天

视觉导航月球极区着陆位姿估计误差模型

visual navigationlunar polar landingpose estimationerror model

《光学精密工程》 2026 (3)

403-414,12

空间智能控制技术国家重点实验室开放基金(No.2024-CXPT-GF-JJ-012-13)光电测量与智能感知中关村开放实验室开放基金(No.LabSOMP-2023-06)

10.37188/OPE.20263403.0403

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