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一种新的航天器姿态快速测量方法

张杰 张巍 范生宏 王顺 鲁利刚

无线电通信技术2017,Vol.43Issue(4):67-70,4.
无线电通信技术2017,Vol.43Issue(4):67-70,4.DOI:10.3969/j.issn.1003-3114.2017.04.16

一种新的航天器姿态快速测量方法

A New Method for Rapid Measurement of Spacecraft Attitude

张杰 1张巍 2范生宏 3王顺 3鲁利刚1

作者信息

  • 1. 北京卫星制造厂,北京 100080
  • 2. 北京控制工程研究所,北京 100190
  • 3. 北京普达迪泰科技有限公司,北京 100083
  • 折叠

摘要

Abstract

Aiming at the problem of frequent alignment in the process of spacecraft alignment and experiment,a new method is proposed to measure the attitude of spacecraft components.This method uses the adjusting device to adjust the XOY surface of satellite coordinate system parallel with the Geodetic plane,then according to the calibration data of entire satellite cubic mirror and component cubic mirror,calculates the theodolite angle quickly,and guide the rapid adjustment of product component attitude.The experimental results show that the precision of this method can meet the design requirements,and the measurement efficiency is significantly improved.

关键词

航天器姿态/准直测量/快速调整

Key words

spacecraft attitude/alignment measurement/rapid adjustment

引用本文复制引用

张杰,张巍,范生宏,王顺,鲁利刚..一种新的航天器姿态快速测量方法[J].无线电通信技术,2017,43(4):67-70,4.

基金项目

国防科研基础计划项目 ()

无线电通信技术

1003-3114

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