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
基金
中国国家自然科学基金; 国家重点研发计划;
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 80 条
  • [71] Mechanism for Warp-Controlled Twist of a Morphing Wing
    Vos, Roelof
    Gurdal, Zafer
    Abdalla, Mostafa
    [J]. JOURNAL OF AIRCRAFT, 2010, 47 (02): : 450 - 457
  • [72] Macro-fiber composite actuators for a swept wing unmanned aircraft
    Bilgen, O.
    Kochersberger, K. B.
    Inman, D. J.
    [J]. AERONAUTICAL JOURNAL, 2009, 113 (1144) : 385 - 395
  • [73] Wing Shape Control through an SMA-Based Device
    Barbarino, S.
    Ameduri, S.
    Lecce, L.
    Concilio, A.
    [J]. JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2009, 20 (03) : 283 - 296
  • [74] Vibration and Flutter Characteristics of a Folding Wing[J] . Matthew P. Snyder,Brian Sanders,Franklin E. Eastep,Geoffrey J. Frank.Journal of aircraft . 2009 (3)
  • [75] Theoretical and experimental aeroelastic study for folding wing structures
    Tang, Deman
    Dowell, Earl H.
    [J]. JOURNAL OF AIRCRAFT, 2008, 45 (04): : 1136 - 1147
  • [76] GAIN-SCHEDULED FLIGHT CONTROL LAW FOR FLEXIBLE AIRCRAFT: A PRACTICAL APPROACH[J] . Guilhem Puyou,Caroline Berard.IFAC Proceedings Volumes . 2007 (7)
  • [77] Aeroelasticity of nonconventional airplane configurations - Past and future
    Livne, E
    Weisshaar, TA
    [J]. JOURNAL OF AIRCRAFT, 2003, 40 (06): : 1047 - 1065
  • [78] Survey of gain-scheduling analysis and design
    Leith, DJ
    Leithead, WE
    [J]. INTERNATIONAL JOURNAL OF CONTROL, 2000, 73 (11) : 1001 - 1025
  • [79] Multidisciplinary design optimization
    Lewis, K
    [J]. AEROSPACE AMERICA, 2000, 38 (12) : 65 - 65
  • [80] Gain-scheduled control: Relaxing slow variation requirements by velocity-based design[J] . Leith DJ.,Leithead WE..Journal of Guidance, Control, and Dynamics: A Publication of the American Institute of Aeronautics and Astronautics Devoted to the Technology of Dynamics and Control . 2000 (6)