航空学报 > 2022, Vol. 43 Issue (10): 527449-527449   doi: 10.7527/S1000-6893.2022.27449

变体飞行器控制技术发展现状与展望

冉茂鹏1, 王成才1,2, 刘华华1, 王薇1, 吕金虎1   

  1. 1. 北京航空航天大学 自动化科学与电气工程学院, 北京 100191;
    2. 中国电子科学研究院, 北京 100041
  • 收稿日期:2022-05-16 修回日期:2022-05-22 发布日期:2022-06-27
  • 通讯作者: 冉茂鹏,E-mail:ranmp@buaa.edu.cn E-mail:ranmp@buaa.edu.cn
  • 基金资助:
    国家自然科学基金(61873295,61833016);北京航空航天大学青年拔尖人才支持计划(YWF-22-L-1205)

Research status and future development of morphing aircraft control technology

RAN Maopeng1, WANG Chengcai1,2, LIU Huahua1, WANG Wei1, LYU Jinhu1   

  1. 1. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China;
    2. China Academy of Electronics and Information Technology, Beijing 100041, China
  • Received:2022-05-16 Revised:2022-05-22 Published:2022-06-27
  • Supported by:
    National Natural Sciente Foundation of China(61873295, 61833016); Beihang Young Top Talents Support Plan(YWF-22-L-1205)

摘要: 变体飞行器可利用变形结构改变气动外形以适应复杂的环境和任务需求,在军事和民用领域均具有极高的发展潜力和应用价值。围绕变体飞行器控制技术这一难度高、发展快、应用前景广阔的研究方向,综述了变体飞行器控制技术的主要研究成果和国内外最新研究进展。首先,结合变体飞行器的发展历程,介绍了变体飞行器的研究背景与意义,指出开展变体飞行器控制技术研究的重要性。其次,对变形决策技术、控制系统建模技术和姿态控制技术等研究成果进行总结与分析。最后,对变体飞行器控制技术的未来研究方向进行了展望。

关键词: 变体飞行器, 控制技术, 变形决策, 控制系统建模, 姿态控制

Abstract: Morphing aircraft can adapt to the complex environment and mission requirements by changing the aerodynamic shape of the deformed structure. It has high development potential and application value in military and civil fields. In this paper, the main research achievements and the latest research progress of the control technology of morphing aircraft are reviewed. Firstly, the background and significance of morphing aircraft control technology are briefly introduced. Secondly, the research results of deformation decision technology, control system modeling and attitude control technology are summarized and analyzed. Finally, the important research directions in the control technology of morphing aircraft are also discussed.

Key words: morphing aircraft, control technology, deformation decision, control system modeling, attitude control

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