Multiobjective optimization of a staggered-rotor octocopter design based on a surrogate model

著录项

• 来源
  《Aerospace science and technology》 |2023年第8期|568-581|共14页
• 作者

  He Zhu; Dongdong Li; Hong NieXiaohui WeiYuanzun Wei;

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• 作者单位

  National Key Laboratory of Rotorcraft Dynamics, Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

  State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

  State Key Laboratory of Mechanics and Control for Aerospace Structures, Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

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• 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
• 原文格式 PDF
• 正文语种 英语
• 中图分类
• 关键词

  Multiobjective optimization; Configuration; Octocopter design; Surrogate model;