具有刚-柔-液-控耦合的航天器动力学研究进展

岳宝增; 宋晓娟

doi:10.6052/1000-0992-12-025

具有刚-柔-液-控耦合的航天器动力学研究进展

doi: 10.6052/1000-0992-12-025

北京理工大学宇航学院力学系, 北京100081

基金项目: 国家自然科学基金(10772026,11072030)及中国教育部博士点博士资助项目(20080070011)

详细信息

作者简介:
岳宝增, 男, 北京理工大学宇航学院力学系教授、博士生导师. 主要研究方向为动力学与控制(包括非线性系统动力学、液体晃动动力学及复杂航天器姿态动力学与控制), 现任全国一般力学专业委员会委员、《力学学报》特邀编委、《力学与实践》编委; 在AIAA Journal, Physical Review,Nonlinear Dynamics, Science China,《力学进展》、《力学学报》及《宇航学报》等学术刊物上发表学术论文80 多篇, SCI 检索论文20 篇、EI 检索30 多篇, 中科院出版基金资助出版专著《液体大幅晃动动力学》一部. 先后承担中国自然科学基金项目4 项、教育部博士点基金项目1 项及其他科研项目.

通讯作者:
岳宝增

中图分类号: V412.4
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出版历程
- 收稿日期: 2012-03-01
- 修回日期: 2012-07-09
- 刊出日期: 2013-01-24

ADVANCES IN RIGID-FLEXIBLE-LIQUID-CONTROL COUPLING DYNAMICS OF SPACECRAFT

School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Funds: The project was supported by the Natural Science Foundation of China(10772026,11072030),Ph.D.Programs Foundation of Ministry of Education of China(20080010011).

More Information

Corresponding author: YUE Baozeng

摘要

摘要: 从现代复杂航天器姿态非线性动力学、液体燃料晃动动力学与控制问题、航天器刚-柔耦合系统动力学建模问题、航天器刚-液耦合动力学、航天器刚-柔-液-控耦合动力学、充液航天器实验问题等方面概述了近年来国内外在充液航天器多体耦合动力学相关领域的最新研究进展. 分别从液体燃料晃动动力学建模问题、航天器刚-柔-液-控耦合系统非线性理论和方法、计算机数值仿真及物理实验问题等方面展望了有待进一步加强的研究课题.
- 充液航天器 /
- 姿态动力学 /
- 刚-柔-液-控耦合系统 /
- 非线性动力学及控制
Abstract: This paper summarized the recent research progress about the attitude nonlinear dynamics of liquid filled spacecraft and coupling dynamics of multi-body-liquid-control nonlinear systems. The developments and achievements in some important research fields, such as dynamics modeling of liquidlled spacecraft with flexible appendage, liquid sloshing dynamics modeling, nonlinear theory and method for spacecrafts with coupling of multi-body-liquid-control, numerical simulation and experiments, are reviewed. The prospects of future researches on concerned topics are also presented in the final section.
- liquidlled spacecraft /
- attitude dynamics /
- coupling of multi-body-liquid-control system /
- nonlinear dynamics and control

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参考文献(82)

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