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| 航天器动力学发展概况 | |
| 引用本文： | 马兴瑞,苟兴宇,李铁寿,王本利.航天器动力学发展概况[J].宇航学报,2000,21(3):1-5. |
| 作者姓名： | 马兴瑞 苟兴宇 李铁寿 王本利 |
| 作者单位： | 1. 中国航天科技集团 北京 100830 2. 北京控制工程研究所 北京 100080 3. 哈尔滨工业大学 哈尔滨 150001 |
| 摘 要： | 分析了现代航天器动力学的复杂性，将现代航天器动力学的发展概括为以下几个方面：１）局部动力学的研究受到重视；２）部件级子系统动力学研究的深入；３）耦合动力学研究进入非线性阶段；４）整体航天器动力学模型精化与一体化仿真；５）航天器与航天器之间相对运动动力学研究方兴未艾等。文章对这几个方面分别作了简单评述或讨论。 |
| 关 键 词： | 航天器动力学 刚体弹性体 液体 发展概况 |
| 修稿时间： | 1999年12月1日 |
DEVELOPMENT GENERALIZATION OF SPACECRAFT DYNAMICS |
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| Ma Xingrui.DEVELOPMENT GENERALIZATION OF SPACECRAFT DYNAMICS[J].Journal of Astronautics,2000,21(3):1-5. | |
| Authors: | Ma Xingrui |
| Abstract: | The complexity of modern spacecraft dynamics was discussed. The development of modern spacecraft dynamics was generalized as follows: 1)Attention to the local dynamics was paid more and more;2)The dynamics of appendage subsystem was studied deeply;3)The study of coupling dynamics was focused on nonlinearity;4)The dynamical model and its simulations of the whole spacecraft became more and more accurate;5)The study of relative motion dynamics between spacecrafts was in the ascendant.Some comments and discussions were made. |
| Keywords: | Spacecraft\ Dynamics\ Rigid body\ Flexible body\ Liquid |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |