期刊文献+

腿式小行星探测器附着稳定性分析

Analysis on adhesion stability of legged-type asteroid detector
下载PDF
导出
摘要 在以小行星为目标的深空探测活动中,探测器承担了附着及采样探测的重要任务。文中以附着为研究目标,首先建立腿式小行星探测器在星体表面附着的多刚体动力学模型。考虑小行星星表环境特点,提出3项表征探测器附着性能的评价指标,基于多体动力学仿真模型对典型1-2模式下的附着性能进行分析,验证其附着性能。采用全因子试验设计方法选取地形及速度参数的样本点,代入至多刚体动力学模型进行计算,基于动力学仿真结果,建立了不同地形及速度参数同附着性能评价指标之间的代理模型,并利用代理模型对探测器的各项附着性能的稳定边界、综合稳定边界及变化趋势进行研究分析。 In the deep space-exploration activities targeted at asteroids,the detector undertakes important tasks of adhesion and sampling detection.In this article,the multi-rigid body dynamic simulation model of the legged-type asteroid detector attached to the star surface is set up.With the environmental characteristics of the star surface into consideration,three evaluation indexes are proposed to characterize the detector’s adhesion stability.Based on the multi-rigid body dynamic simulation model,the adhesion performance under the typical 1-2 mode is explored and verified.The full-factorial experimental design is applied to select sample points of the terrains and velocity parameters,which are introduced into the multi-rigid body dynamic simulation model.Based on the results of dynamic simulation,a surrogate model between different terrains and velocity parameters on one hand and the evaluation indexes of the adhesion performance on the other hand is worked out.The surrogate model is used to analyze the stability boundary of the detector’s adhesion performance,as well as its comprehensive stability boundary and changing trend.
作者 王辉 王春洁 WANG Hui;WANG Chun-jie(School of Mechanical Engineering and Automation,Beihang University,Beijing 100191;State Key Laboratory of Virtual Reality and Systems,Beihang University,Beijing 100191;Beijing Institute of Aerospace Systems Engineering,Beijing 100076)
出处 《机械设计》 CSCD 北大核心 2022年第9期11-17,共7页 Journal of Machine Design
基金 国家自然科学基金资助项目(U2037602)。
关键词 小行星探测 多体动力学 代理模型 稳定性分析 asteroid exploration multi-body dynamics surrogate model stability analysis
  • 相关文献

参考文献3

二级参考文献28

  • 1赵振,刘才山,陈滨.三维含摩擦多刚体碰撞问题的数值计算方法[J].中国科学(G辑),2006,36(1):72-88. 被引量:9
  • 2姚文莉,王育平,边力,赵振.多刚体系统接触碰撞动力学研究进展[J].力学与实践,2007,29(6):9-12. 被引量:11
  • 3Binzel R P,Lupishko D,Martino M D. Asteroids Ⅲ:physical properties of near-earth objects[M].Tucson:University of Arizona Press,2002.255-271.
  • 4Chapman C R. The hazard of near-earth asteroid impacts on earth[J].{H}Earth and Planetary Science Letters,2004,(222):1-15.
  • 5Blessing M,Quintana E,Persaud R. Asteroids working group report[A].2006.
  • 6Hilchenbach M,Kuchemann O,Rosenbauer H. Impact on a comet:rosetta lander simulations[J].{H}Planetary and Space Science,2000,(48):361-369.
  • 7Lavender R E. Touchdown dynamics analysis of spacecraft for soft lunar landing[R].NASA TN D-2001,1964.1-32.
  • 8Herr R W,Leonard H W. Dynamic model investigation of touchdown stability of lunar-landing vehicles[R].NASA TN D-4215,1967.1-22.
  • 9Wang Shaochun,Deng Zongquan,Hu Ming. Dynamic model building and simulation for mechanical main body of lunar lander[J].Journal of Central South University,2005,(03):329-334.
  • 10Chen Jinbao,Nie Hong. Overloading of landing based on the deformation of the lunar lander[J].Chinese Journal of Aeronautics,2008,(21):43-47.

共引文献12

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