J4 ›› 2016, Vol. 13 ›› Issue (2): 235-248.doi: 10.1016/S1672-6529(16)60297-4

• 论文 • 上一篇    下一篇

Hybrid Design and Performance Tests of a Hovering Insect-inspired Flapping-wing Micro Aerial Vehicle

Quoc-Viet Nguyen, Woei Leong Chan, Marco Debiasi   

  1. Temasek Laboratories, National University of Singapore, Singapore 117411, Singapore
  • 收稿日期:2015-09-05 修回日期:2016-03-05 出版日期:2016-04-10 发布日期:2016-04-10
  • 通讯作者: Quoc-Viet Nguyen E-mail:tslnqv@nus.edu.sg, nguyenqv@gmail.com
  • 作者简介:Quoc-Viet Nguyen, Woei Leong Chan, Marco Debiasi

Hybrid Design and Performance Tests of a Hovering Insect-inspired Flapping-wing Micro Aerial Vehicle

Quoc-Viet Nguyen, Woei Leong Chan, Marco Debiasi   

  1. Temasek Laboratories, National University of Singapore, Singapore 117411, Singapore
  • Received:2015-09-05 Revised:2016-03-05 Online:2016-04-10 Published:2016-04-10
  • Contact: Quoc-Viet Nguyen E-mail:tslnqv@nus.edu.sg, nguyenqv@gmail.com
  • About author:Quoc-Viet Nguyen, Woei Leong Chan, Marco Debiasi

摘要:

Hovering ability is one of the most desired features in Flapping-Wing Micro Air Vehicles (FW-MAVs). This paper presents a hybrid design of flapping wing and fixed wing, which combines two flapping wings and two fixed wings to take advantage of the double wing clap-and-fling effect for high thrust production, and utilizes the fixed wings as the stabilizing surfaces for inherently stable hovering flight. Force measurement shows that the effect of wing clap-and-fling significantly enhances the cycle-averaged vertical thrust up to 44.82% at 12.4 Hz. The effect of ventral wing clap-and-fling due to presence of fixed wings produces about 11% increase of thrust-to-power ratio, and the insect-inspired FW-MAV can produce enough cycle-averaged vertical thrust of 14.76 g for lift-off at 10 Hz, and 24 g at maximum frequency of 12.4 Hz. Power measurement indicates that the power consumed for aerodynamic forces and wing inertia, and power loss due to gearbox friction and mechanism inertia was about 80% and 20% of the total input power, respectively. The proposed insect-inspired FW-MAV could endure three-minute flight, and demonstrate a good flight performance in terms of vertical take-off, hovering, and control with an onboard 3.7 V-70 mAh LiPo battery and control system.

关键词: insect-inspired flapping wing, hovering, clap-and-fling, MAV, vertical takeoff

Abstract:

Hovering ability is one of the most desired features in Flapping-Wing Micro Air Vehicles (FW-MAVs). This paper presents a hybrid design of flapping wing and fixed wing, which combines two flapping wings and two fixed wings to take advantage of the double wing clap-and-fling effect for high thrust production, and utilizes the fixed wings as the stabilizing surfaces for inherently stable hovering flight. Force measurement shows that the effect of wing clap-and-fling significantly enhances the cycle-averaged vertical thrust up to 44.82% at 12.4 Hz. The effect of ventral wing clap-and-fling due to presence of fixed wings produces about 11% increase of thrust-to-power ratio, and the insect-inspired FW-MAV can produce enough cycle-averaged vertical thrust of 14.76 g for lift-off at 10 Hz, and 24 g at maximum frequency of 12.4 Hz. Power measurement indicates that the power consumed for aerodynamic forces and wing inertia, and power loss due to gearbox friction and mechanism inertia was about 80% and 20% of the total input power, respectively. The proposed insect-inspired FW-MAV could endure three-minute flight, and demonstrate a good flight performance in terms of vertical take-off, hovering, and control with an onboard 3.7 V-70 mAh LiPo battery and control system.

Key words: insect-inspired flapping wing, hovering, clap-and-fling, MAV, vertical takeoff