Untethered flight of an insect-sized flapping-wing microscale aerial vehicle

被引:386
|
作者
Jafferis, Noah T. [1 ,2 ]
Helbling, E. Farrell [1 ,2 ]
Karpelson, Michael [2 ]
Wood, Robert J. [1 ,2 ]
机构
[1] Harvard Univ, John A Paulson Sch Engn & Appl Sci, Cambridge, MA 02138 USA
[2] Harvard Univ, Wyss Inst Biol Inspired Engn, Cambridge, MA 02138 USA
基金
美国国家科学基金会;
关键词
TAKEOFF; DESIGN; POWER;
D O I
10.1038/s41586-019-1322-0
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
Heavier-than-air flight at any scale is energetically expensive. This is greatly exacerbated at small scales and has so far presented an insurmountable obstacle for untethered flight in insect-sized (mass less than 500 milligrams and wingspan less than 5 centimetres) robots. These vehicles(1-4) thus need to fly tethered to an offboard power supply and signal generator owing to the challenges associated with integrating onboard electronics within a limited payload capacity. Here we address these challenges to demonstrate sustained untethered flight of an insect-sized flapping-wing microscale aerial vehicle. The 90-milligram vehicle uses four wings driven by two alumina-reinforced piezoelectric actuators to increase aerodynamic efficiency (by up to 29 per cent relative to similar two-wing vehicles(5)) and achieve a peak lift-to-weight ratio of 4.1 to 1, demonstrating greater thrust per muscle mass than typical biological counterparts(6). The integrated system of the vehicle together with the electronics required for untethered flight (a photovoltaic array and a signal generator) weighs 259 milligrams, with an additional payload capacity allowing for additional onboard devices. Consuming only 110-120 milliwatts of power, the system matches the thrust efficiency of similarly sized insects such as bees(7). This insect-scale aerial vehicle is the lightest thus far to achieve sustained untethered flight (as opposed to impulsive jumping(8) or liftoff(9)).
引用
收藏
页码:491 / +
页数:17
相关论文
共 50 条
  • [1] System Identification and Linear Time-Invariant Modeling of an Insect-Sized Flapping-Wing Micro Air Vehicle
    Finio, Benjamin M.
    Perez-Arancibia, Nestor O.
    Wood, Robert J.
    2011 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, 2011, : 1107 - 1114
  • [2] Nonlinear trajectory control of a flapping-wing micro aerial vehicle
    Khanmirza, Esmaeel
    Yousefi-Koma, Aghil
    Tarvirdizadeh, Bahram
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2012, 84 (01): : 58 - 65
  • [3] Should friction losses be included in an electromechanical model of a bioinspired flapping-wing micro aerial vehicle to estimate the flight energetic requirements?
    Park, Moonsoo
    Ventikos, Yiannis
    Abolfathi, Ali
    BIOINSPIRATION & BIOMIMETICS, 2022, 17 (03)
  • [4] Research Progress on Bio-inspired Flapping-Wing Rotor Micro Aerial Vehicle Development
    Pan, Yingjun
    Guo, Shijun
    Huang, Xun
    JOURNAL OF BIONIC ENGINEERING, 2024, 21 (04) : 1621 - 1643
  • [5] Biomimetic Flapping Wing Aerial Vehicle
    Fenelon, Michael. A. A.
    2008 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND BIOMIMETICS, VOLS 1-4, 2009, : 1053 - 1058
  • [6] Force generation and wing deformation characteristics of a flapping-wing micro air vehicle 'DelFly II' in hovering flight
    Percin, M.
    van Oudheusden, B. W.
    de Croon, G. C. H. E.
    Remes, B.
    BIOINSPIRATION & BIOMIMETICS, 2016, 11 (03)
  • [7] Development of Flapping-wing Micro Air Vehicle in Asia
    Tan, Xiaobo
    Zhang, Weiping
    Ke, Xijun
    Chen, Wenyuan
    Zou, Caijun
    Liu, Wu
    Cui, Feng
    Wu, Xiaosheng
    Li, Hongyi
    PROCEEDINGS OF THE 10TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA 2012), 2012, : 3939 - 3942
  • [8] Development of an Insect-like Flapping-Wing Micro Air Vehicle with Parallel Control Mechanism
    Chen, Zihao
    Zhang, Weiping
    Mou, Jiawang
    Zhao, Jiaxin
    APPLIED SCIENCES-BASEL, 2022, 12 (07):
  • [9] Time-Varying Model Identification of Flapping-Wing Vehicle Dynamics Using Flight Data
    Armanini, S. F.
    de Visser, C. C.
    de Croon, G. C. H. E.
    Mulder, M.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (03) : 526 - 541
  • [10] Liftoff of a Motor-Driven, Flapping-Wing Microaerial Vehicle Capable of Resonance
    Hines, Lindsey
    Campolo, Domenico
    Sitti, Metin
    IEEE TRANSACTIONS ON ROBOTICS, 2014, 30 (01) : 220 - 232