| 近程地对地战术导弹总体/发动机一体化优化设计 |
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| 引用本文： | 董春平. 近程地对地战术导弹总体/发动机一体化优化设计[J]. 战术导弹技术, 1991, 0(2): 16-26 |
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| 作者姓名： | 董春平 |
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| 作者单位： | 航空航天部210所 |
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| 摘 要： | 地对地战术导弹总体/发动机一体化优化设计是把飞行器和发动机作为一个系统,以系統性能最佳作为目标值来优选飞行器总体和发动机的设计参数。针对近程地对地战术导弹建立了最优控制过程模型及一体化的全系統模型。着重分析了一体化模型建立,融内外弹道为一体,各级同时优化,并应用庞特里雅金(Pontryagin)最小值原理和非线性多目标规划理论进行了求解。
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| 关 键 词： | 战术导弹 总体 发动机 优化 ~#一体化设计 |
INTEGRATED OPTIMUM DESIGN OF AIRFRAME/ENGINE FOR SHORT RANGE SURFACE TO SURFACE MISSILE |
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| Dong Chunping Institute NO. of MAS. INTEGRATED OPTIMUM DESIGN OF AIRFRAME/ENGINE FOR SHORT RANGE SURFACE TO SURFACE MISSILE[J]. Tactical Missile Technology, 1991, 0(2): 16-26 |
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| Authors: | Dong Chunping Institute NO. of MAS |
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| Affiliation: | Dong Chunping Institute NO. 210 of MAS |
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| Abstract: | Integrative optimum design of airframe/engine for surface to surface tactical missile is described. The design parameters of airframe and engine are optimized regarding airframe and engine as an independent system and optimum performances of the system as a good. Optimal control process model and the model of the integrated system have been set up for the short range surface to surface tactical missile. The design of setting up integrated model, merging internal-external trajectory into a single whole and simultaneous optimization for multistage are analysed particularly. The solution is gained by using pontryagin's minimum principle and nonlinear multiple objective programming theory. |
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| Keywords: | Tactical missile System Engire Optimization ~#Integrated design |
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