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Volume 26 Issue 1
Jan.  2000
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Journal of Beijing University of Aeronautics and Astronautics  > 2000  >  26(1): 67-69.
Wei Xinguo, Chen Xiao, Song Jingminget al. Kind of novel micro integrative transceiver module[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(8): 973-976. (in Chinese)
Citation: LI Jing, LI Tian, WU Zheet al. Use of Fuzzy Optimization in Conceptual Design of Fighter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(1): 67-69. (in Chinese)
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Use of Fuzzy Optimization in Conceptual Design of Fighter

  • 1.

    Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics

  • 2. Shenyang Institute of Aircraft

  • Received Date: 30 Jun 1998
  • Publish Date: 31 Jan 2000
    Abstract
  • Linear function is used to form the satisfactory functions of the objectives and constraints of the integrated aerodynamic-stealth design of fighter geometrical parameters, such as the root chord and tip chord of the wing, half span of basic wing, the leading-edge sweepback of the wing, the sideway elongation coefficient and the radius of the fuselage at the interface position with the wing, and then,basing on these functions, the multiobjective fuzzy optimization model was established. Punishment function is used to transfer the constrained optimization to unconstrained optimization and the Nelder and Mead Method is used to solve this optimization problem.

     

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  • [1] 航空气动力手册编写组.航空气动力手册[M].北京:国防工业出版社,1983. [2]刘千刚. 复杂构形的亚、跨、超音速定常及非定常气动力的Green函数算法综述 . 航空学报,1996,17(2):137~143． [3]克拉特E F.雷达散射截面——预估、测量和减缩[M]. 阮颖铮译.北京:电子工业出版社,1988.
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