| 近空间飞行器固体火箭助推器/助推弹道总体设计优化 |
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| 引用本文： | 胡诗国,方洋旺,刘万俊.近空间飞行器固体火箭助推器/助推弹道总体设计优化[J].火力与指挥控制,2011,36(10):143-147. |
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| 作者姓名： | 胡诗国 方洋旺 刘万俊 |
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| 作者单位： | 空军工程大学工程学院,西安,710038 |
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| 基金项目： | 国家自然科学基金资助项目(60874040) |
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| 摘 要： | 研究一种近空间飞行器的固体火箭助推器/助推弹道总体优化问题.在选定喷管构型、推进剂、壳体材料、绝热层材料及药柱结构的前提下,建立包含热力学分析与计算、质量分析与计算、气动力分析与计算和弹道设计与计算的系统分析模型,采用一种基于可行性规则与结合模拟退火的混合粒子群优化算法求解最优解.优化结果表明建立的系统分析模型和采用的...
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| 关 键 词： | 近空间飞行器 固体火箭助推器 混合粒子群算法 模拟退火算法 最优设计 |
Design Optimization of Solid Rocket Booster Based on Hybrid Particle Swarm Optimization Algorithm for NSV |
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| HU Shi-guo,FANG Yang-wang,LIU Wan-jun.Design Optimization of Solid Rocket Booster Based on Hybrid Particle Swarm Optimization Algorithm for NSV[J].Fire Control & Command Control,2011,36(10):143-147. |
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| Authors: | HU Shi-guo FANG Yang-wang LIU Wan-jun |
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| Institution: | HU Shi-guo,FANG Yang-wang,LIU Wan-jun(Air Force Engineering University Engineering College,Xi'an 710038,China) |
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| Abstract: | To serve the nonlinear programming problem which has multi-variables with constrains of Design optimization of solid rocket booster for a Near Space Vehicle(NSV),a system analysis model including the thermodynamics analysis and calculating sub-model,the mass analysis and calculating sub-model,the aerodynamics analysis and calculating sub-model,and the trajectory design and calculating sub-model was establish under the precondition of given nozzle structural,propellant,shell materiel,adiabatic materiel and r... |
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| Keywords: | Near Space Vehicle(NSV) solid rocket booster hybrid particle swarm algorithm simulated annealing optimum design |
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