Design, modeling, and control of morphing aircraft:A review

被引：0
|
作者：
Lingling CHU [1 ,2 ,3 ]
Qi LI [1 ,2 ]
Feng GU [1 ,2 ]
Xintian DU [1 ,2 ]
Yuqing HE [1 ,2 ]
Yangchen DENG [4 ]
机构：
[1] State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences
[2] Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences
[3] University of Chinese Academy of Sciences
[4] Shenyang Aircraft Design & Research Institute
来源：
Chinese Journal of Aeronautics | 2022年 / 35卷 / 05期
基金：
国家重点研发计划; 中国国家自然科学基金;
关键词：
D O I：
暂无
中图分类号：
V279 [无人驾驶飞机]; V249.1 [飞行控制];
学科分类号：
081105 ; 1111 ;
摘要：
A morphing aircraft can adapt its configuration to suit different types of tasks, which is also an important requirement of Unmanned Aerial Vehicles(UAV). The successful development of an unmanned morphing aircraft involves three steps that determine its ability and intelligent: configuration design, dynamic modeling and flight control. This study conducts a comprehensive survey of morphing aircraft. First, the methods to design the configuration of a morphing aircraft are presented and analyzed. Then, the nonlinear dynamic characteristics and aerodynamic interference caused by a morphing wing are described. Subsequently, the dynamic modeling and flight control methods for solving the flight control problems are summarized with respect to these features.Finally, the general as well as special challenges ahead of the development of intelligent morphing aircraft are discussed. The findings can provide a theoretical and technical reference for designing future morphing aircraft or morphing-wing UAVs.
引用
收藏
页码：220 / 246
页数：27
相关论文
共 50 条
  • [31] Actor-Critic-Based Optimal Adaptive Control Design for Morphing Aircraft
    Lee, Hanna
    Kim, Seong-hun
    Kim, Youdan
    IFAC PAPERSONLINE, 2020, 53 (02): : 14863 - 14868
  • [32] Morphing Aircraft Sizing Using Design Optimization
    Crossley, William A.
    Skillen, Michael D.
    Frommer, Joshua B.
    Roth, Brian D.
    JOURNAL OF AIRCRAFT, 2011, 48 (02): : 612 - 622
  • [33] Morphing aircraft: The need for a new design philosophy
    Ajaj, Rafic M.
    Beaverstock, Christopher S.
    Friswell, Michael I.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 49 : 154 - 166
  • [34] Chained smooth switching control for morphing aircraft
    Wang, Qing
    Wang, Tong
    Dong, Chao-Yang
    Jiang, Wei-Lai
    Kongzhi Lilun Yu Yingyong/Control Theory and Applications, 2015, 32 (07): : 949 - 954
  • [35] Novel robust control framework for morphing aircraft
    Chunsheng Liu
    Shaojie Zhang
    Journal of Systems Engineering and Electronics, 2013, 24 (02) : 281 - 287
  • [36] Novel robust control framework for morphing aircraft
    Liu, Chunsheng
    Zhang, Shaojie
    JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2013, 24 (02) : 281 - 287
  • [37] Trajectory Optimization and Tracking Control of a Morphing Aircraft
    Dai, Pei
    Yan, Binbin
    Pang, Minghui
    Jiang, Yilei
    Yin, Yingming
    Wang, Mingang
    2020 5TH INTERNATIONAL CONFERENCE ON MECHANICAL, CONTROL AND COMPUTER ENGINEERING (ICMCCE 2020), 2020, : 746 - 750
  • [38] Modeling of Dynamic Loading of Morphing-Wing Aircraft
    Obradovic, B.
    Subbarao, K.
    JOURNAL OF AIRCRAFT, 2011, 48 (02): : 424 - 435
  • [39] Integrated Design of a Morphing Winglet for Active Load Control and Alleviation of Turboprop Regional Aircraft
    Dimino, Ignazio
    Andreutti, Giovanni
    Moens, Frederic
    Fonte, Federico
    Pecora, Rosario
    Concilio, Antonio
    APPLIED SCIENCES-BASEL, 2021, 11 (05): : 1 - 27
  • [40] Dynamic modeling for a morphing aircraft and dynamic characteristics analysis
    Zhang, Jie
    Wu, Sentang
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2015, 41 (01): : 58 - 64
12345