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基于多学科设计优化弹道导弹概念设计研究 被引量:5

Ballistic missile conceptual design based on multidisciplinary design optimization
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摘要 为提高弹道导弹概念设计中各学科的协同效应,缩短概念方案研制周期,以设计出综合性能更好、效能更高的飞行器方案,以iSIGHT为集成与优化平台,建立了多学科设计优化弹道导弹概念设计系统,综合弹道导弹概念设计各个学科的知识,应用有效的设计/优化策略,来组织和管理弹道导弹概念设计过程。将混合优化策略应用于弹道导弹重量、弹道和动力一体化优化设计,很好地解决了各学科间复杂耦合带来的计算问题,给出了方案优化结果,证实了该算法的有效性。 To improve collaboration among different disciplinary in the conceptual design of ballistic missiles, to shorten development cycle of conceptual scheme and obtain conceptual scheme with better integrated performance, knowledge of each disciplinary was integrated and proper optimization strategy was selected to manage the process of ballistic missile conceptual design based on a conceptual design system developed on iSIGHT integration and optimization platform. Hybrid optimal strategy was applied in conceptual design of ballistic missile with three disciplinary, namely weight disciplinary, propulsion disciplinary and trajectory disciplinary, as a result the calculation problems caused by coupling relationship between disciplinary were well solved. Optimization results were provided, as well as the validity of the optimization algorithm was also proved.
出处 《计算机集成制造系统》 EI CSCD 北大核心 2007年第12期2289-2293,共5页 Computer Integrated Manufacturing Systems
关键词 弹道导弹概念设计 系统集成 多学科设计优化 混合优化策略 ballistic missile conceptual design system integration multidisciplinary design optimization hybrid optimal strategy
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参考文献5

  • 1STANLEY D O, UNAL R, JOYNER C R. Application of Taguchi methods to propulsion system optimization for SSTO vehicles [J]. Journal of Spacecraft and Rockets, 1993, 29 (4) : 453-459.
  • 2OLDS J R. Results of a rocket-based combined-cycle SSTO design using parametric MDO methods [M]//SAE Technical Paper Series. Atlanta, Ga. , USA: Georgia Institute of Technology, 1994:941165.
  • 3HE Linshu. Solid ballistic missiles design[M]. Beijing: Beijing University of Aeronautics & Astronautics Press, 2004: 15-34,62-82.
  • 4VARFOLOMEYEV V I, KOPYTOV M I. Design and testing of ballistic missiles [R]. N71-13001, Moscow, Russia: Miliary Publishing House of the Ministry of Defence USSR, 1970: 120-128, USSR.
  • 5Saqlain Akhtar,He Lin-shu.Optimization and Sizing for Propulsion System of Liquid Rocket Using Genetic Algorithm[J].Chinese Journal of Aeronautics,2007,20(1):40-46. 被引量:5

二级参考文献1

  • 1Ph.D.Candidate:Wang Gang Fluid Mechanics Institute, Beijing University of Aeronautics and Astronautics, Beijing 100083, China,Supervisor: Deng Xue ying (Beijing University of Aeronautics and Astronautics) Members of Dissertation Defense Committee: Tong Bing gang (Graduate School of the Chinese Academy of Sciences),Chairman Gu Zhi fu (Peking University) Yang Qi de (China Aerodynamics Research and Development Center) Lv Zhi yong (Beijing University of Aeronautics and Astronautics) Liu Pei qing (Beijing University of Aeronautics and Astronautics).EXPERIMENTAL STUDY OF FLOWFIELD STRUCTURE AROUND AN OGIVE-CYLINDER[J].Journal of Hydrodynamics,2003,15(5):109-109. 被引量:18

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