| 助推-滑翔导弹总体一体化优化设计 |
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| 引用本文： | 徐玮,孙丕忠,夏智勋.助推-滑翔导弹总体一体化优化设计[J].固体火箭技术,2008,31(4). |
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| 作者姓名： | 徐玮 孙丕忠 夏智勋 |
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| 作者单位： | 国防科技大学,航天与材料工程学院,长沙,410073 |
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| 摘 要： | 综合考虑固体火箭发动机设计、弹道设计和总体特性相互作用和相互影响,建立了新概念助推-滑翔导弹总体一体化设计优化模型和系统分析模型.应用遗传算法优化了19个设计参数,并与弹道导弹优化结果进行了比较.结果表明,助推-滑翔导弹具有很强的机动突防能力,且具有增程能力.
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| 关 键 词： | 助推-滑翔导弹 一体化设计 优化设计 遗传算法 |
Integration design and optimization for boost-glider missile |
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| XU Wei,SUN Pi-zhong,XIA Zhi-xun.Integration design and optimization for boost-glider missile[J].Journal of Solid Rocket Technology,2008,31(4). |
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| Authors: | XU Wei SUN Pi-zhong XIA Zhi-xun |
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| Abstract: | Considering SRM design,trajectory design and system characteristics,a series of mathematical models for optimization design of boost-glider missile were established.The optimizing calculation for 19 variables of boost-glider missile was finished by means of genetic algorithm.The calculation results were compared with those of ballistic missile.The results show that the boost-glider missile possesses better maneuver penetration capability and extended-yange capability. |
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| Keywords: | boost-glider missile integration design optimum design genetic algorithm |
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