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
  • [41] Autonomous flight control with different strategies applied during the complete flight cycle for flapping-wing flying robots
    Zhong, SiPing
    Wang, Song
    Xu, WenFu
    Liu, JunTao
    Pan, ErZhen
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2023, 66 (11) : 3343 - 3354
  • [42] Modeling and Trajectory Generation of Bird-like Flapping-wing Micro Air Vehicle
    Mu, Xinxing
    He, Xiuyu
    Zhang, Liang
    Fu, Qiang
    He, Wei
    2020 CHINESE AUTOMATION CONGRESS (CAC 2020), 2020, : 3832 - 3837
  • [43] Bionic Design and Attitude Control Measurement in a Double Flapping-Wing Micro Air Vehicle
    Zhang, Xuedong
    Deng, Huichao
    Xiao, Shengjie
    Yang, Lili
    Ding, Xilun
    INTELLIGENT ROBOTICS AND APPLICATIONS, ICIRA 2019, PART VI, 2019, 11745 : 240 - 254
  • [44] Flight control of a large-scale flapping-wing flying robotic bird: System development and flight experiment
    Xu, Wenfu
    Pan, Erzhen
    Liu, Juntao
    Li, Yihong
    Yuan, Han
    CHINESE JOURNAL OF AERONAUTICS, 2022, 35 (02) : 235 - 249
  • [45] Rapid Inertial Reorientation of an Aerial Insect-sized Robot Using a Piezo-actuated Tail
    Singh, Avinash
    Libby, Thomas
    Fuller, Sawyer B.
    2019 INTERNATIONAL CONFERENCE ON ROBOTICS AND AUTOMATION (ICRA), 2019, : 4154 - 4160
  • [46] An Insect-Like Flapping-Wing Device Actuated by a Compressed Unimorph Piezoelectric Composite Actuator
    Nguyen, Quoc Viet
    Park, Hoon Cheol
    Goo, Nam Seo
    Byun, Doyoung
    INTELLIGENT UNMANNED SYSTEMS: THEORY AND APPLICATIONS, 2009, 192 : 101 - +
  • [47] Global Linear Parameter-Varying Modeling of Flapping-Wing Dynamics Using Flight Data
    Armanini, S. F.
    Karasek, M.
    de Visser, C. C.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2018, 41 (11) : 2338 - 2360
  • [48] Flight control of flapping-wing robot with three paired direct-driven piezoelectric actuators
    Jimbo, T.
    Ozaki, T.
    Amano, Y.
    Fujimoto, K.
    IFAC PAPERSONLINE, 2020, 53 (02): : 9391 - 9398
  • [49] Experimental and numerical study of different wing number and flapping-rotation decomposition of a flapping wing rotor unmanned aerial vehicle
    Wang, Ziyu
    Kan, Zi
    Li, Huadong
    Zhao, Shiwei
    Li, Daochun
    Xiang, Jinwu
    PHYSICS OF FLUIDS, 2024, 36 (02)
  • [50] Wingbeat Shape Modulation for Flapping-Wing Micro-Air-Vehicle Control During Hover
    Doman, David B.
    Oppenheimer, Michael W.
    Sigthorsson, David O.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (03) : 724 - 739