期刊文献+

空间机构运动行为模拟概念研究 被引量:18

Simulation Study on Motion Behavior of Spacecraft Mechanisms
下载PDF
导出
摘要 空间机构在太空执行各种运动功能,面对复杂的空间环境,空间机构设计必须考虑微重力环境或重力及其释放问题,而研究空间环境效应,首先需要地面模拟试验的配合。目前,长时间地面微重力环境无法理想模拟,空间机构地面模拟研究因此受到了一定制约。为此,本文在分析重力对运动关节界面间隙及运动阻力影响的基础上,提出以运动行为模拟代替运动环境模拟、开展空间机构地面模拟研究的设想,并指出需要解决的主要科学技术问题,建议开发空间机构运动行为地面模拟试验平台技术、重视大型空间精密操控机构的重力及其释放问题研究。 Spacecraft mechanisms perform various motion functions in space. In the unique space environment, microgravity, gravity and its release must be taken into account during the design of the spacecraft mechanisms. Generally, the ground simulation test is needed first in the study of space environment effects. However, because the gravitational field is everywhere on the ground, it is difficult to get a real microgravity environment for a long duration during the ground microgravity environment simulation test, which has been a challeuge for the research of spacecraft mechanisms. Therefore, based on analyzing the effects of gravity on motion resistance and interface of joint clearance, a novel idea to overcome the bottlenecks of ground based researches on spacecraft mechanisms was proposed : to simulate motion behavior of spacecraft mechanisms in microgravity environment instead of the microgravity environment simulation; some main scientific and technological problem to be solved were pointed out. In addition to fundamental researches, building a platform for ground motion behavior simulation test was proposed. In the end, on - orbit tests for proving the research results were proposed, and it is suggested that special attention must be paid to problems caused by gravity release of large accurate spacecraft mechanisms.
作者 王文魁
出处 《载人航天》 CSCD 2013年第5期59-66,共8页 Manned Spaceflight
基金 国家高技术研究发展计划(863计划)资助
关键词 空间机构 空间环境模拟 重力释放 运动行为 摩擦机制 Key words: spacecraft mechanisms space environments simulation gravity releasing motion behavior frictional mechanism
  • 相关文献

参考文献24

  • 1Edesona R,Agliett GSi,Tatnall ARL. Conventional stable structures for space optics:The state of the art[J].Acta Astronautica,2011,(66):13-32.
  • 2Kyoichi Ui,Tomoyuki Urabe,Saburo Matimaga. Three dimensional microgravity experiments of approaching/grasping phase of docking mechanism for nano-satellite with air thruster[J].Journal of the Japan Society for Aeronautical and Space Sciences,2005,(620):419-425.
  • 3陈烈民.航天器结构与机构[M]北京:中国科学技术出版社,2005454.
  • 4徐文福,梁斌,李成,刘宇,强文义.空间机器人微重力模拟实验系统研究综述[J].机器人,2009,31(1):88-96. 被引量:63
  • 5朱战霞;袁建平.航天器操作的微重力环境构建[M]北京:宇航出版社,2013.
  • 6朱光辰,贾世锦.出舱活动的地面试验验证[J].载人航天,2009,15(3):48-53. 被引量:14
  • 7韦娟芳.卫星天线展开过程的零重力环境模拟设备[J].空间电子技术,2006,3(2):29-32. 被引量:21
  • 8齐乃明,张文辉,高九州,马静.三维空间微重力地面模拟试验系统设计[J].机械工程学报,2011,47(9):16-20. 被引量:16
  • 9Moon FC,Li GX. Experimental study of chaotic vibrations in a pin-jointed space truss structure[J].AIAA Journal,1990,(05):915-921.
  • 10Flores P,Ambrosio J,Claro JCP. A study on dynamics of mechanical systems including joints with clearance and lubrication[J].Mechanism and Machine Theory,2006,(03):247-261.doi:10.1016/j.mechmachtheory.2005.10.002.

二级参考文献150

共引文献223

同被引文献142

引证文献18

二级引证文献57

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部