首页 | 本学科首页   官方微博 | 高级检索  
     检索      

微重力充液系统大幅晃动动力学及其在航天高技术中的应用
引用本文:王照林,张乃恭.微重力充液系统大幅晃动动力学及其在航天高技术中的应用[J].宇航学报,1993,14(4):35-40.
作者姓名:王照林  张乃恭
作者单位:清华大学 (王照林),中国科学院(张乃恭)
基金项目:国家自然科学基金,航天部五院资助课题
摘    要:本文首先论述了在微重力环境下充液系统大幅晃动动力学的理论基础,其次阐明了它在充液航天器动力学与控制中的应用,最后分析了液体大幅晃动自由边界的确定以及数值稳定性等问题。

关 键 词:大幅晃动  微重力  航天飞机

On the Large-scale Amplitude Sloshing Dynamics of Liquid-filled System under Low-gravity Environments and Its Applications in Space Technology
Wang Zhaoling Zhang Naigong.On the Large-scale Amplitude Sloshing Dynamics of Liquid-filled System under Low-gravity Environments and Its Applications in Space Technology[J].Journal of Astronautics,1993,14(4):35-40.
Authors:Wang Zhaoling Zhang Naigong
Institution:Wang Zhaoling Zhang Naigong(Tsinghua University) (Chinese Academy of Sciences)
Abstract:In this paper,firstly,the theoretical foundation of large-scale amplitude sloshing dynamics of liquid-filld system is expounded under low-gravity environments. And then,its applications are clarified in the field of dynamics and control of spacecraft filled with liquid. Lastly, the free boundary determination of large-scale amplitude sloshing and the numerical stability of date are analyzed.
Keywords:Large-scale amplitude sloshing  Low-gravity  Sloshing suppression  Free boundary  Space shuttle  Areo-space shuttle  
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号