| 具有刚-柔-液-控耦合的航天器动力学研究进展 |
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| 引用本文： | 岳宝增,宋晓娟.具有刚-柔-液-控耦合的航天器动力学研究进展[J].力学进展,2013,43(1):163-173. |
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| 作者姓名： | 岳宝增 宋晓娟 |
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| 作者单位： | 北京理工大学宇航学院力学系, 北京100081 |
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| 基金项目： | 国家自然科学基金(10772026,11072030);中国教育部博士点博士资助项目(20080070011)~~ |
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| 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.
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| 关 键 词： | 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 |
| 收稿时间： | 2012-03-01 |
| 修稿时间： | 2012-07-09 |
ADVANCES IN RIGID-FLEXIBLE-LIQUID-CONTROL COUPLING DYNAMICS OF SPACECRAFT |
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| YUE Baozeng,SONG Xiaojuan.ADVANCES IN RIGID-FLEXIBLE-LIQUID-CONTROL COUPLING DYNAMICS OF SPACECRAFT[J].Advances in Mechanics,2013,43(1):163-173. |
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| Authors: | YUE Baozeng SONG Xiaojuan |
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| Institution: | School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China |
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| 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. |
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| Keywords: | liquidlled spacecraft attitude dynamics coupling of multi-body-liquid-control system nonlinear dynamics and control |
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