| 注册
首页|期刊导航|航天器工程|基于星箭对接环同心圆结构的卫星姿态估计方法

基于星箭对接环同心圆结构的卫星姿态估计方法

鄂薇 魏承 王典军 经姚翔 赵阳

航天器工程2018,Vol.27Issue(2):41-46,6.
航天器工程2018,Vol.27Issue(2):41-46,6.DOI:10.3969/j.issn.1673-8748.2018.02.007

基于星箭对接环同心圆结构的卫星姿态估计方法

Satellite Pose Estimation Method Based on Concentric Circle Structure of Docking Ring

鄂薇 1魏承 1王典军 2经姚翔 2赵阳1

作者信息

  • 1. 哈尔滨工业大学航天工程与力学系,哈尔滨 150001
  • 2. 中国空间技术研究院通信卫星事业部,北京 100094
  • 折叠

摘要

Abstract

Using single circle feature of docking ring to estimate pose of satellite has two solu-tions,which cannot be easily applied to practical applications.In this paper,the docking ring is treated as a concentric structure composed of inner and outer rings,so the normal vector of the spatial ring can be resolved according to the algebraic constraints of the concentric circles.Then the attitude of target satellite relate to tracking satellite can be determined.Several groups of sim-ulation experiments are carried out to calculate and analyze the pose estimation error with differ-ent measuring distances and noise levels.The monocular vision-based pose estimation of the doc-king ring with unknown diameter and uncertain center is achieved and verified without any extra measurement information.The result can provide the support for pose estimation of space non-cooperative obj ect.

关键词

星箭对接环/同心圆环/姿态估计/单目视觉/射影变换

Key words

docking ring/concentric circle/pose estimation/monocular vision/proj ective trans-formation

分类

信息技术与安全科学

引用本文复制引用

鄂薇,魏承,王典军,经姚翔,赵阳..基于星箭对接环同心圆结构的卫星姿态估计方法[J].航天器工程,2018,27(2):41-46,6.

基金项目

国家自然科学基金(11772102) (11772102)

航天器工程

OA北大核心CSCDCSTPCD

1673-8748

访问量0
|
下载量0
段落导航相关论文