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一种用于探测器地外天体起飞试验的位姿及运动模拟装置

刘万龙 孔凡超 邱法维 张奎好 胡旭坤 孙树江 牛向楠

航天器环境工程2015,Vol.32Issue(4):424-428,5.
航天器环境工程2015,Vol.32Issue(4):424-428,5.DOI:10.3969/j.issn.1673-1379.2015.04.016

一种用于探测器地外天体起飞试验的位姿及运动模拟装置

An attitude and motion simulation device for probe takeoff test from celestial bodies

刘万龙 1孔凡超 1邱法维 2张奎好 1胡旭坤 1孙树江 1牛向楠1

作者信息

  • 1. 北京航天试验技术研究所,北京 100074
  • 2. 北京三强同维机电液压科技发展有限公司,北京 102200
  • 折叠

摘要

Abstract

In the future extraterrestrial celestial detection, the landing, the sampling, the returns and other activities are usually involved. In this paper, the attitude and motion simulation device for space environment simulation tests for the detector return takeoff is studied. A six degree-of-freedom Stewart platform is proposed as the attitude and motion simulation device. The device can simulate the static and dynamic posture adjustment. The layout of the device in the vacuum chamber and the principle of the device are discussed. The device is controlled by an upper computer and lower computers. The motion parameters of the device could be set in the upper computer through software, and then the motion parameters are transferred to the lower computers for control. The device can meet the attitude and motion simulation requirements of the detector test.

关键词

探测器/地外天体/返回起飞/位姿运动模拟

Key words

probe/celestial bodies/return take off/attitude and motion simulation

分类

航空航天

引用本文复制引用

刘万龙,孔凡超,邱法维,张奎好,胡旭坤,孙树江,牛向楠..一种用于探测器地外天体起飞试验的位姿及运动模拟装置[J].航天器环境工程,2015,32(4):424-428,5.

基金项目

探月工程三期研制保障条件建设项目 ()

航天器环境工程

OACSTPCD

1673-1379

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