Stable Flight of a Flapping-Wing Micro Air Vehicle Under Wind Disturbance

被引:20
|
作者
Lee, Jonggu [1 ,2 ]
Ryu, Seungwan [1 ,2 ]
Kim, H. Jin [1 ,2 ]
机构
[1] Seoul Natl Univ, Dept Mech & Aerosp Engn, Seoul 08826, South Korea
[2] Seoul Natl Univ, Automat & Syst Res Inst ASRI, Seoul 08826, South Korea
关键词
Biologically-Inspired Robots; Robust; Adaptive Control of Robotic Systems; Biomimetics; STABILITY; DYNAMICS; TRACKING;
D O I
10.1109/LRA.2020.3009064
中图分类号
TP24 [机器人技术];
学科分类号
080202 ; 1405 ;
摘要
Flapping-wing micro air vehicles (FWMAVs) inspired by the nature are interesting flight platforms due to their efficiency, concealment and agility. However, most studies have been conducted in indoor environments where external disturbance is excluded because these FWMAVs are susceptible to disturbance due to their complex dynamics and small size. In order for these bio-inspired robots to perform various tasks outside, a capability to react robustly to external disturbance is essential. In this letter, we propose an algorithm that allows a FWMAV to fly well even under external disturbance. First, we derive the attitude dynamics of the FWMAV based on flight data. Then, we design a robust attitude controller using DOBC based on the dynamics. Also, we add a flight mode selector to recognize disturbance autonomously and switch to the robust control mode. Finally, we experiment outdoor flight of the FWMAV with wind disturbance. The FWMAV recognizes the existence of disturbance autonomously, and produces additional control inputs to compensate the disturbance. The proposed algorithm is validated with experiments.
引用
下载
收藏
页码:5685 / 5692
页数:8
相关论文
共 50 条
  • [31] Active disturbance rejection attitude control for the dove flapping wing micro air vehicle in intermittent flapping and gliding flight
    Liang, Shaoran
    Song, Bifeng
    Xuan, Jianlin
    Li, Yubin
    INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES, 2020, 12
  • [32] Effects of camber angle on aerodynamic performance of flapping-wing micro air vehicle
    Yoon, Sang-Hoon
    Cho, Haeseong
    Lee, Junhee
    Kim, Chongam
    Shin, Sang-Joon
    JOURNAL OF FLUIDS AND STRUCTURES, 2020, 97
  • [33] Transition Flight Trajectory Optimization for a Flapping-Wing Micro Air Vehicle with Unsteady Vortex-Lattice Method
    Lee, Sang-Gil
    Yang, Hyeon-Ho
    Addo-Akoto, Reynolds
    Han, Jae-Hung
    AEROSPACE, 2022, 9 (11)
  • [34] Improvements to Evolutionary Model Consistency Checking for a Flapping-Wing Micro Air Vehicle
    Gallagher, John C.
    Boddhu, Sanjay
    Matson, Eric
    Greenwood, Garrison
    2014 IEEE INTERNATIONAL CONFERENCE ON EVOLVABLE SYSTEMS (ICES), 2014, : 203 - 210
  • [35] Control of a Flapping-Wing Micro Air Vehicle: Sliding-Mode Approach
    Bluman, James E.
    Kang, Chang-Kwon
    Shtessel, Yuri
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2018, 41 (05)
  • [36] Design and Flight Performance of a Bio-Inspired Hover-Capable Flapping-Wing Micro Air Vehicle with Tail Wing
    Xiao, Shengjie
    Sun, Yuhong
    Ren, Dapeng
    Hu, Kai
    Deng, Huichao
    Wang, Yun
    Ding, Xilun
    AEROSPACE, 2023, 10 (11)
  • [37] A Flapping-Wing Micro Air Vehicle with Interchangeable Parts for System Integration Studies
    Sahai, Ranjana
    Galloway, Kevin C.
    Karpelson, Michael
    Wood, Robert J.
    2012 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS (IROS), 2012, : 501 - 506
  • [38] Aerodynamics of a bio-inspired flexible flapping-wing micro air vehicle
    Nakata, T.
    Liu, H.
    Tanaka, Y.
    Nishihashi, N.
    Wang, X.
    Sato, A.
    BIOINSPIRATION & BIOMIMETICS, 2011, 6 (04)
  • [39] Elastic Element Integration for Improved Flapping-Wing Micro Air Vehicle Performance
    Sahai, Ranjana
    Galloway, Kevin C.
    Wood, Robert J.
    IEEE TRANSACTIONS ON ROBOTICS, 2013, 29 (01) : 32 - 41
  • [40] Fabrication of composite hinge mechanism for flapping-wing motion of micro air vehicle
    Kang, Lae-Hyong
    Jang, Hee-Suk
    Leem, Ju-Young
    Han, Jae-Hung
    COMPOSITES RESEARCH, 2009, 22 (06): : 7 - 12