| 再入飞行器总体参数多目标优化设计 |
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| 引用本文： | 王瑞臣. 再入飞行器总体参数多目标优化设计[J]. 导弹与航天运载技术, 1993, 0(1): 49-55 |
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| 作者姓名： | 王瑞臣 |
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| 作者单位： | 北京特殊机电研究所 |
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| 摘 要： | 在内部装填物参数给定的情况下,减小再入飞行器的质量和雷达截面具有重要意义。本文以再入飞行器的质量和雷达截面为目标函数进行多目标优化。本文的理论和计算方法可用于再入飞行器总体设计的方案论证阶段。
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| 关 键 词： | 再入飞行器 头锥 最佳设计 |
Multi-object Optimization of Reentry Vehicle''''s Parameters |
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| Yu Debin Wang Ruichen. Multi-object Optimization of Reentry Vehicle''''s Parameters[J]. Missiles and Space Vehicles, 1993, 0(1): 49-55 |
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| Authors: | Yu Debin Wang Ruichen |
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| Affiliation: | Beijing Institute of Special Mechanical and Electronic Devices |
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| Abstract: | A suitable mathematical model and an optimum method of system design of the reentry vehicle have been established. The paper herein optimizes the objectives of the mass and the RCS of the reentry vehicle, and makes the objectives smallest. |
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| Keywords: | Reentry vehicle Nose cone Optimum design. |
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