J4 ›› 2014, Vol. 11 ›› Issue (1): 36-51.doi: 10.1016/S1672-6529(14)60018-4

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  • 收稿日期:2013-03-04 修回日期:2013-12-04 出版日期:2014-01-10 发布日期:2014-01-10

Pitching Moment Generation in an Insect-Mimicking Flapping-Wing System

Tri Quang Truong, Vu Hoang Phan, Sanjay P. Sane, Hoon Cheol Park   

  1. 1. Biomimetics and Intelligent Microsystem Laboratory &|Artificial Muscle Research Center, Konkuk University, Seoul 143-701, Korea
    2. Department of Advanced Technology Fusion, Konkuk University, Seoul 143-701, Korea
    3. National Centre for Biological Sciences, Tata Institute of Fundamental Research, Bangalore, India
  • Received:2013-03-04 Revised:2013-12-04 Online:2014-01-10 Published:2014-01-10
  • Contact: Hoon Cheol Park E-mail:hcpark@konkuk.ac.kr
  • About author:Tri Quang Truong, Vu Hoang Phan, Sanjay P. Sane, Hoon Cheol Park

关键词: flapping-wing system, pitching moment, flapping angle, unsteady blade element theory, mean aerodynamic center, center of gravity

Abstract:

Unlike birds, insects lack control surfaces at the tail and hence most insects modify their wing kinematics to produce control forces or moments while flapping their wings. Change of the flapping angle range is one of the ways to modify wing kinematics, resulting in relocation of the mean Aerodynamic force Center (mean AC) and finally creating control moments. In an attempt to mimic this feature, we developed a flapping-wing system that generates a desired pitching moment during flap-ping-wing motion. The system comprises a flapping mechanism that creates a large and symmetric flapping motion in a pair of wings, a flapping angle change mechanism that modifies the flapping angle range, artificial wings, and a power source. From the measured wing kinematics, we have found that the flapping-wing system can properly modify the flapping angle ranges. The measured pitching moments show that the flapping-wing system generates a pitching moment in a desired direction by shifting the flapping angle range. We also demonstrated that the system can in practice change the longitudinal attitude by generating a nonzero pitching moment.

Key words: flapping-wing system, pitching moment, flapping angle, unsteady blade element theory, mean aerodynamic center, center of gravity