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非合作航天器逆深度参数化姿态估计

刘宗明 曹姝清 张宇 叶东

光学精密工程2017,Vol.25Issue(2):451-459,9.
光学精密工程2017,Vol.25Issue(2):451-459,9.DOI:10.3788/OPE.20172402.0451

非合作航天器逆深度参数化姿态估计

Inverse depth parameterized attitude estimation for non-cooperative spacecraft

刘宗明 1曹姝清 2张宇 3叶东2

作者信息

  • 1. 哈尔滨工业大学,电气工程及自动化学院,黑龙江哈尔滨150001
  • 2. 上海航天控制技术研究所,上海201109
  • 3. 上海市空间智能控制技术重点实验室,上海201109
  • 折叠

摘要

Abstract

Purpose:to achieve on-orbit servicing or off-orbit removal of non-cooperative targets in space,such as inactive satellites,space debris,especially slowly rotating targets,accurate measurement of relative attitude between the tracking aircraft and target aircraft is necessary.Method:firstly,used inverse depth parameterization to represent the coordinate value,angular altitude,azimuth angle and depth information of the camera,which could effectively complete the monocular vision attitude estimation under small parallax error;secondly,established a motion model and measurement model of the camera relative to the non-cooperative target;finally,achieved the relative motion attitude estimation between the camera and target based on single candidate RANSAC and EKF.Results:for three-axes stable targets,the attitude measurement accuracy during the approaching process is approximately 0.5°;for slowly rotating targets (constant velocity),the relative angle error is about 3.5%,with an average angular velocity error of approximately 0.1°/s.All these parameters can meet the requirements for relative attitude measurements of engineering spatial non-cooperative targets.

关键词

非合作目标/逆深度参数/姿态估计/EKF/RANSAC

Key words

non-cooperative target/inverse depth parameterization/attitude estimation/EKF/RANSAC

分类

信息技术与安全科学

引用本文复制引用

刘宗明,曹姝清,张宇,叶东..非合作航天器逆深度参数化姿态估计[J].光学精密工程,2017,25(2):451-459,9.

基金项目

上海市青年科技启明星计划(No.16QB1401000) (No.16QB1401000)

光学精密工程

OA北大核心CSCDCSTPCD

1004-924X

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