| 大型复杂航天器的柔性附件展开的动力学分析 |
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| 引用本文： | 马兴瑞,王天舒.大型复杂航天器的柔性附件展开的动力学分析[J].中国空间科学技术,2000,20(4):1-7,14. |
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| 作者姓名： | 马兴瑞 王天舒 |
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| 作者单位： | 中国航天科技集团公司,北京 |
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| 摘 要： | 分析了复杂航天器在柔性附件展开过程中的几个关键问题，并提出了相应的解决方案，编制了应用软件。通过数值模拟详细分析了其附件的展开过程，讨论的内容包括卫星姿态角和姿态角速度的变化规律、柔性附件的展开运动及其弹性振动等。
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| 关 键 词： | 柔性体 航天器 动力学仿真 动力学分析 |
Dynamics Analysis of Lager Spacecraft With Deploying Flexible Appendages |
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| Ma Xingrui.Dynamics Analysis of Lager Spacecraft With Deploying Flexible Appendages[J].Chinese Space Science and Technology,2000,20(4):1-7,14. |
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| Authors: | Ma Xingrui |
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| Abstract: | The several important problems such as deployment procedure of flexible appendages on complex spacecraft are analyzed,and corresponding programme and application software are introduced.Appendages deployment is analyzed by numerical simulation.The contents including attitude motion,attitude velocity,deployment and vibration of flexible appendages etc are discussed. |
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| Keywords: | Flexible body Spacecraft Dynamic simulation Analyzing |
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