考 虑 吸 波 材 料 的 雷 达 散 射 截 面 伴 随 优 化 方 法

Lin Zhou, Jiangtao Huang, Shidong Zhong, Gang Liu, Jun Deng, Zhenghong Gao

科研成果: 期刊稿件文章同行评审

摘要

The development of anti-stealth technology has put forward higher requirements for the stealth performance of military aircraft. This study establishes a discrete adjoint equation of Maxwell’s equation considering the absorbing material to perform optimization design of low observable aircraft considering the absorbing material. The fast multilayer multipole expansion form of the adjoint equation is derived,achieving efficient RCS gradient calculation with re⁃ spect to shape parameters,material electrical parameters,and coating thickness. A switch function is proposed to conduct absorbing material coating position optimization. Shape parameters,material coating position,coating thick⁃ ness,and electromagnetic parameters are optimized using the adjoint method. Numerical results indicate that the ad⁃ joint approach can further reduce the cavity RCS compared to the ideal conductor shape design and material coating. Also,the adjoint approach is able to optimize the design of material parameters and coating thickness,providing guid⁃ ance for the selection and coating of the absorbing material. Optimization of the coating position based on the switch function can achieve optimal allocation of the absorbing material with the constraint of total material weight. The pro⁃ posed RCS adjoint optimization method considering the absorbing material can provide technical support for the effi⁃ cient design of coating position and absorbing material coefficients.

投稿的翻译标题Radar cross section optimization based on adjoint approach considering radar absorbing material
源语言繁体中文
文章编号130347
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
45
24
DOI
出版状态已出版 - 25 12月 2024

关键词

  • electromagnetic adjoint equation
  • gradient optimization
  • impedance boundary condition
  • radar absorbing material
  • radar cross section

指纹

探究 '考 虑 吸 波 材 料 的 雷 达 散 射 截 面 伴 随 优 化 方 法' 的科研主题。它们共同构成独一无二的指纹。

引用此