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姿态运动对落舱微重力的影响研究
Alternative TitleON THE INFLUENCE OF ATTITUDE MOTION ON THE LEVELS OF MICROGRAVITY IN A DROPCAPSULE
楼岳; 孙先仿; 北京8701信箱
Department火箭与气球探空技术研究室
Source Publication空间科学学报
1997
Volume17Issue:3Pages:282-288
ISSN0254-6124
Language中文
Keyword落舱 微重力 姿态运动 均匀设计 高空气球
Abstract本文采用试验的均匀设计方法,结合地对气动力矩的理论估算,利用计算机仿真,研究了姿态运动对落舱微重力水平的影响.结果表明,在落舱下落的前60s内,要想保持优于10g数量级的微重力水平,以满足一般科学实验的要求,则必须安装姿态控制系统.
Other AbstractThe method of experimental uniform design,山eoretical computations and computer simulations were used in the research on the influence of attitude motion on the levels of crogravity in the dropcapsule.It is shown that an attitude control system must be set up on the dropcapsule if one wants to keep 60s of microgravity time with microgravity levels less than 10-3g.
Funding Project中国科学院空间科学与应用研究中心
Document Type期刊论文
Identifierhttp://ir.nssc.ac.cn/handle/122/1678
Collection其他部室
Corresponding Author北京8701信箱
Recommended Citation
GB/T 7714
楼岳,孙先仿,北京8701信箱. 姿态运动对落舱微重力的影响研究[J]. 空间科学学报,1997,17(3):282-288.
APA 楼岳,孙先仿,&北京8701信箱.(1997).姿态运动对落舱微重力的影响研究.空间科学学报,17(3),282-288.
MLA 楼岳,et al."姿态运动对落舱微重力的影响研究".空间科学学报 17.3(1997):282-288.
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