整机和系统设计 |
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基于悬吊法和气浮法的多自由度微重力模拟展开试验系统研究 |
李海月1, 程泽1, 赵丹妮1, 王浩威2, 李德勇1, 张加波1, 宋晓东3, 赵琳娜1 |
1.北京卫星制造厂有限公司, 北京 100094 2.北京空间飞行器总体设计部, 北京 100094 3.北京理工大学 宇航学院, 北京 100081 |
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Research on multi-degree-of-freedom microgravity simulation deployment test system based on suspension method and air flotation method |
LI Hai-yue1, CHENG Ze1, ZHAO Dan-ni1, WANG Hao-wei2, LI De-yong1, ZHANG Jia-bo1, SONG Xiao-dong3, ZHAO Lin-na1 |
1.Beijing Satellite Manufacturing Limited Company, Beijing 100094, China 2.Beijing Insitute of Spacecraft System Engineering, Beijing 100094, China 3.School of Aerospace Science, Beijing Institute of Technology, Beijing 100081, China |
引用本文:
李海月, 程泽, 赵丹妮, 王浩威, 李德勇, 张加波, 宋晓东, 赵琳娜. 基于悬吊法和气浮法的多自由度微重力模拟展开试验系统研究[J]. 工程设计学报, 2020, 27(4): 508-515.
LI Hai-yue, CHENG Ze, ZHAO Dan-ni, WANG Hao-wei, LI De-yong, ZHANG Jia-bo, SONG Xiao-dong, ZHAO Lin-na. Research on multi-degree-of-freedom microgravity simulation deployment test system based on suspension method and air flotation method. Chinese Journal of Engineering Design, 2020, 27(4): 508-515.
链接本文:
https://www.zjujournals.com/gcsjxb/CN/10.3785/j.issn.1006-754X.2020.00.055
或
https://www.zjujournals.com/gcsjxb/CN/Y2020/V27/I4/508
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