| 可重复使用垂直起降运载火箭软着陆动力学仿真研究 |
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| 引用本文： | 杨文淼.可重复使用垂直起降运载火箭软着陆动力学仿真研究[J].科学技术与工程,2017,17(21). |
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| 作者姓名： | 杨文淼 |
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| 作者单位： | 上海宇航系统工程研究所 |
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| 摘 要： | 随着航天技术的飞速发展,可重复使用运载火箭成为未来运载火箭技术的发展趋势。结合一种可重复使用垂直起降运载火箭着陆系统,基于ADAMS软件平台,开发了模拟作为主要缓冲材料的铝蜂窝力学性能子程序。建立了软着陆动力学仿真模型,实现了对可重复使用垂直起降运载火箭着陆过程的动力学仿真分析。仿真结果对可重复使用垂直起降运载火箭的研究具有一定参考价值。
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| 关 键 词： | 动力学仿真 垂直起降 软着陆 ADAMS子程序 |
| 收稿时间： | 2017/1/16 0:00:00 |
| 修稿时间： | 2017/1/16 0:00:00 |
Dynamic Simulation of VTOL Reusable Launch Vehicle Soft-landing |
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| yangwenmiao.Dynamic Simulation of VTOL Reusable Launch Vehicle Soft-landing[J].Science Technology and Engineering,2017,17(21). |
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| Authors: | yangwenmiao |
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| Institution: | Aerospace System Engineering Shanghai |
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| Abstract: | With the rapid development of space technology, reusable launch vehicles become the future trend of launch vehicle technology. In this paper, in combination with one VTOL reusable rocket landing system, the simulation routine of mechanical properties of aluminum honeycomb was developed based on ADAMS software platform. The dynamic simulation model of VTOL reusable soft-landing was established. The process of VTOL reusable rocket soft-landing was analyzed. The results have a certain reference value for VTOL reusable launch vehicle research. |
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| Keywords: | dynamic simulation VTOL soft-landing ADAMS subroutines |
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