Decentralized active damping control for aeroelastic morphing wing

被引：1
|
作者：
Svoboda, Filip [1 ]
Hengster-Movric, Kristian [1 ]
Hromcik, Martin [1 ]
Sika, Zbynek [2 ]
机构：
[1] Czech Tech Univ, Fac Elect Engn, Karlovo Namesti 13, Prague 12135, Czech Republic
[2] Czech Tech Univ, Fac Mech Engn, Tech 4, Prague 16000, Czech Republic
来源：
AEROSPACE SCIENCE AND TECHNOLOGY | 2023年 / 139卷
关键词：
Decentralized control; Morphing wing; Aeroelasticity; Linear matrix inequalities; MULTIAGENT SYSTEMS; STATE-FEEDBACK; DESIGN; AIRCRAFT; SYNCHRONIZATION; CONSENSUS; NETWORKS;
D O I：
10.1016/j.ast.2023.108415
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper introduces a novel decentralized control design procedure for an aeroelastic morphing wing. The control goal is active damping of this flexible system. The model is developed as a multi-agent system with inherent interconnections between the agents. The control system then takes advantage of the model structure and interconnections rather than relying on the entire system's model. This brings benefits, especially with a growing number of agents where the control design dimension remains low. Therefore, the proposed control design is especially suitable for morphing wings with a large number of actuation points. The result is presented in the Linear Matrix Inequalities (LMIs) form. A numerical example shows the application of the proposed algorithm. & COPY; 2023 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数：10
相关论文
共 50 条
  • [41] Active flutter suppression of wing with morphing flap
    Ouyang, Yan
    Gu, Yingsong
    Kou, Xiping
    Yang, Zhichun
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 110
  • [42] Aeroelastic Response of a Z-Shaped Folding Wing During the Morphing Process
    Xie, Changchuan
    Chen, Zhiying
    Chao, An
    [J]. AIAA JOURNAL, 2022, 60 (05) : 3166 - 3179
  • [43] Computational and Experimental Validation of the Active Morphing Wing
    Smith, D. D.
    Lowenberg, M. H.
    Jones, D. P.
    Friswell, M. I.
    [J]. JOURNAL OF AIRCRAFT, 2014, 51 (03): : 925 - 937
  • [44] Geometrically nonlinear static aeroelastic analysis of composite morphing wing with corrugated structures
    Tsushima, Natsuki
    Yokozeki, Tomohiro
    Su, Weihua
    Arizono, Hitoshi
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 88 : 244 - 257
  • [45] Subcritical and supercritical nonlinear aeroelastic behavior of a morphing wing with bilinear hinge stiffness
    Zhou, Xinghua
    Huang, Rui
    [J]. COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2021, 103
  • [46] Flow separation control on morphing wing
    College of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China
    不详
    [J]. Gongcheng Lixue, 2009, 5 (228-233+238):
  • [47] Flight dynamic modeling and control for a telescopic wing morphing aircraft via asymmetric wing morphing
    Yue, Ting
    Zhang, Xiangyang
    Wang, Lixin
    Ai, Junqiang
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 70 : 328 - 338
  • [48] Smart panel with active damping units.: Implementation of decentralized control
    Diaz, Cristobal Gonzalez
    Paulitsch, Christoph
    Gardonio, Paolo
    [J]. JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2008, 124 (02): : 898 - 910
  • [49] Morphing wing strategy of a deformable wing and its cooperative control
    Deng, Xiaowei
    Li, Xiaolei
    Xiang, Zhihua
    Zhang, Xianxiang
    Sun, Guanghui
    [J]. Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University, 2023, 44 (09): : 1563 - 1570
  • [50] Active Aeroelastic Control Over a Multisurface Wing: Modeling and Wind-Tunnel Testing
    De Gaspari, A.
    Ricci, S.
    Riccobene, L.
    Scotti, A.
    [J]. AIAA JOURNAL, 2009, 47 (09) : 1995 - 2010
12345