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垂 直 起 降 固 定 翼 无 人 机 技 术 发 展 及 趋 势 分 析

  • Kelei Wang
  • , Zhou Zhou
  • , Yuewen Ma
  • , Wanshan Du
  • , Jiahao Guo
  • , Xu Li
  • , Yang Zhang
  • , Pengbo Sun
  • Northwestern Polytechnical University Xian

科研成果: 期刊稿件文献综述同行评审

33 引用 (Scopus)

摘要

The vertical takeoff and landing(VTOL)fixed wing unmanned aerial vehicle(UAV)has many advan⁃ tages,such as low requirements for takeoff and landing site,good maneuverability,high cruise speed and long en⁃ durance,etc.,which is a hot topic in the aviation field. The existing VTOL fixed wing UAV development status and their basic features around the world are described in this paper,and then the technical features faced by these different types of VTOL fixed wing UAV are analyzed. It indicates that the VTOL fixed wing UAV with higher cruise speed,longer battery life,and stronger ability of task load seems to be the main developing direction and in⁃ evitable trend in the future. Although the tilting rotor configuration and tail-seat configuration are still the main⁃ stream configuration of the VTOL fixed wing UAV in nowadays,the distributed electric propulsion (DEP)VTOL fixed wing UAV technology will become the hottest issues in the field of aerospace,therefore,it is neces⁃ sary to enhance the evolutionary research in the new-concept configurations and new principles of the high-perfor⁃ mance VTOL fixed wing UAV.

投稿的翻译标题Development and Trend Analysis of Vertical Takeoff and Landing Fixed Wing UAV
源语言繁体中文
页(从-至)1-13
页数13
期刊Advances in Aeronautical Science and Engineering
13
5
DOI
出版状态已出版 - 10月 2022
已对外发布

关键词

  • VTOL fixed wing UAV
  • development status
  • dis⁃ tributed electric propulsion
  • tail-seat configuration
  • tilting rotor configuration

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