Simulation of the flapping wing aerial vehicle using flexible multibody dynamics

被引：1
|
作者：
Choi, JaeWon [1 ]
Gong, DuHyun [1 ]
Lee, Junhee [1 ]
Kim, Chongam [2 ]
Shin, SangJoon [2 ]
机构：
[1] Seoul Natl Univ, Dept Aerosp Engn, Seoul, South Korea
[2] Seoul Natl Univ, Inst Adv Aerosp Technol, Seoul 08826, South Korea
来源：
INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES | 2021年 / 13卷
关键词：
Insect-type; flapping wing; finite-element-based flexible multibody dynamics; geometrically exact beam; trailing edge control; FLIGHT; MODEL;
D O I：
10.1177/17568293211043305
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
An insect-type flapping wing micro aerial vehicle offers high aerodynamic efficiency and maneuverability in confined spaces. The complicated aerodynamic/structural behavior of flapping wing micro aerial vehicle, however, causes difficulties regarding the dynamic control and parametric design. This paper develops a moderately accurate numerical framework taking into account the passive motion of the main wings. Finite-element-based multibody dynamics and two-dimensional unsteady aerodynamics are combined to simulate the hover of a flapping wing micro aerial vehicle. In addition, flexible and rigid wings are compared through numerical simulation considering the flexibility. In terms of the average thrust, numerical simulation by fluid-structure interaction shows good agreements against the experimental results within 5% discrepancy.
引用
收藏
页数：12
相关论文
共 50 条
  • [31] Simulation and optimal design of a piezoelectric bimorph actuator for flapping-wing micro aerial vehicle
    Tan, Xiao-Bo
    Zhang, Wei-Ping
    Chi, Peng-Cheng
    Ke, Xi-Jun
    Zou, Cai-Jun
    Chen, Wen-Yuan
    Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2012, 46 (11): : 1852 - 1856
  • [32] Design of an active flapping wing mechanism and a micro aerial vehicle using a rotary actuator
    Fenelon, Michael A. A.
    Furukawa, Tomonari
    MECHANISM AND MACHINE THEORY, 2010, 45 (02) : 137 - 146
  • [33] AUTONOMOUS LOITERING CONTROL FOR A FLAPPING WING MINIATURE AERIAL VEHICLE WITH INDEPENDENT WING CONTROL
    Roberts, Luke
    Bruck, Hugh A.
    Gupta, Satyandra K.
    PROCEEDINGS OF THE ASME INTERNATIONAL DESIGN ENGINEERING TECHNICAL CONFERENCES AND COMPUTERS AND INFORMATION IN ENGINEERING CONFERENCE, 2014, VOL 5A, 2014,
  • [34] Yaw Control of a Hovering Flapping-Wing Aerial Vehicle With a Passive Wing Hinge
    Chukewad, Yogesh M.
    Fuller, Sawyer
    IEEE ROBOTICS AND AUTOMATION LETTERS, 2021, 6 (02): : 1864 - 1871
  • [35] Modelling wing wake and tail aerodynamics of a flapping-wing micro aerial vehicle
    Armanini, S. F.
    Caetano, J., V
    de Visser, C. C.
    Pavel, M. D.
    de Croon, G. C. H. E.
    Mulder, M.
    INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES, 2019, 11
  • [36] Experimental Study on the Wing-wake Interaction of a Flapping Wing Micro Aerial Vehicle
    Boon, Lua Kim
    Jadhav, Siddharth
    2017 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS'17), 2017, : 1292 - 1301
  • [37] Flight Dynamics of a Flapping-Wing Air Vehicle
    Krashanitsa, Roman Y.
    Silin, Dmitro
    Shkarayev, Sergey V.
    Abate, Gregg
    INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES, 2009, 1 (01) : 35 - 49
  • [38] Aerodynamic Analysis and Simulation of Flapping Wing Aerial Vehicles on Hovering
    Ren L.
    Deng H.
    Shen Q.
    Journal of Beijing Institute of Technology (English Edition), 2019, 28 (04): : 696 - 702
  • [39] Longitudinal modelling and control of a flapping-wing micro aerial vehicle
    Rakotomamonjy, Thomas
    Ouladsine, Mustapha
    Le Moing, Thierry
    CONTROL ENGINEERING PRACTICE, 2010, 18 (07) : 679 - 690
  • [40] Aerodynamic Analysis and Simulation of Flapping Wing Aerial Vehicles on Hovering
    Liangliang Ren
    Hongbin Deng
    Qiang Shen
    JournalofBeijingInstituteofTechnology, 2019, 28 (04) : 696 - 702
12345