助推-滑翔导弹总体一体化优化设计  

Integration design and optimization for boost-glider missile

作　　者：徐玮[1] 孙丕忠[1] 夏智勋[1] 

机构地区：[1]国防科技大学航天与材料工程学院,长沙410073

出　　处：《固体火箭技术》2008年第4期317-320,共4页Journal of Solid Rocket Technology

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。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,

关 键 词：助推-滑翔导弹 一体化设计 优化设计 遗传算法 

分 类 号：V421.1[航空宇航科学与技术—飞行器设计]