Recent Progress Towards Developing an Insect-Inspired Flapping-Wing Micro Air Vehicle

Abstract : This paper presents an overview of the on-going research activities at Shrivenham, aimed at the design of an autonomous flapping-wing micro air vehicle. After introducing the problem of insect wing kinematics and aerodynamics, we describe our quasi-three-dimensional aerodynamic model for flapping wings. This is followed by a brief discussion of some aerodynamic issues relating to the lift-generating leading-edge vortex. New results are then presented on modelling of wing aeroelastic deflections. Finally, some brief observations are made on flight control requirements for an insect-inspired flapping-wing micro air vehicle. Overall, it is shown that successful development of such a vehicle will require a multi-disciplinary approach, with significant developments in a number of disciplines. Progress to date has largely been concerned with hover. Little is known about the requirements for successful manoeuvre.

[1]  R. Zbikowski,et al.  Sensor-rich feedback control: a new paradigm for flight control inspired by insect agility , 2004, IEEE Instrumentation & Measurement Magazine.

[2]  A. R. Ennos.  The kinematics and aerodynamics of the free flight of some diptera , 1989 .

[3]  L. Zeng,et al.  Measuring the body position, attitude and wing deformation of a free-flight dragonfly by combining a comb fringe pattern with sign points on the wing , 2002 .

[4]  R. Zbikowski.  On aerodynamic modelling of an insect–like flapping wing in hover for micro air vehicles , 2002, Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences.

[5]  Hirokazu Matsumoto,et al.  A fringe shadow method for measuring flapping angle and torsional angle of a dragonfly wing , 1996 .

[6]  R J Wootton,et al.  Approaches to the structural modelling of insect wings. , 2003, Philosophical transactions of the Royal Society of London. Series B, Biological sciences.

[7]  Adrian L. R. Thomas,et al.  FLOW VISUALIZATION AND UNSTEADY AERODYNAMICS IN THE FLIGHT OF THE HAWKMOTH, MANDUCA SEXTA , 1997 .

[8]  Willmott,et al.  Measuring the angle of attack of beating insect wings: robust three-dimensional reconstruction from two-dimensional images , 1997, The Journal of experimental biology.

[9]  Thomas L Daniel,et al.  Flexible Wings and Fins: Bending by Inertial or Fluid-Dynamic Forces?1 , 2002, Integrative and comparative biology.

[10]  M. Dickinson,et al.  UNSTEADY AERODYNAMIC PERFORMANCE OF MODEL WINGS AT LOW REYNOLDS NUMBERS , 1993 .

[11]  Adrian L. R. Thomas,et al.  Leading-edge vortices in insect flight , 1996, Nature.

[12]  J. Leishman,et al.  Phase-locked particle image velocimetry measurements of a flapping wing , 2006 .

[13]  C. Ellington,et al.  The three–dimensional leading–edge vortex of a ‘hovering’ model hawkmoth , 1997 .

[14]  L. Zeng,et al.  A video tracking system for measuring the position and body deformation of a swimming fish , 2002 .

[15]  Kevin Knowles,et al.  Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 1: Methodology and analysis , 2006 .

[16]  T. Daniel,et al.  The Journal of Experimental Biology 206, 2989-2997 © 2003 The Company of Biologists Ltd , 2003 .

[17]  Kevin Knowles,et al.  Aerodynamic modelling of insect-like flapping flight for micro air vehicles , 2006 .

[18]  Kevin Knowles,et al.  Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 2: Implementation and validation , 2006 .

[19]  M. Dickinson,et al.  Wing rotation and the aerodynamic basis of insect flight. , 1999, Science.

[20]  N. Strausfeld.  Atlas of an Insect Brain , 1976, Springer Berlin Heidelberg.

[21]  Andrew R Harvey,et al.  High-speed photogrammetry system for measuring the kinematics of insect wings. , 2006, Applied optics.

[22]  Shirley Dex,et al.  JR 旅客販売総合システム（マルス）における運用及び管理について , 1991 .

[23]  A. A. Biewener,et al.  Biomechanics-- structures and systems : a practical approach , 1992 .

[24]  Gary D. Lock,et al.  Energy requirements for the flight of micro air vehicles , 2001, The Aeronautical Journal (1968).

[25]  Max F. Platzer,et al.  Flapping-wing Micro Air Vehicles , 2006 .

[26]  Ellington,et al.  A computational fluid dynamic study of hawkmoth hovering , 1998, The Journal of experimental biology.

[27]  W. Pilkey.  Formulas for stress, strain, and structural matrices , 1994 .

[28]  C. Ellington.  The Aerodynamics of Hovering Insect Flight. III. Kinematics , 1984 .

[29]  S. K. Tolani,et al.  A Strain Energy Comparison of Discrete Modeling for Vibrating Continuous Systems , 1972 .

[30]  R. Bishop,et al.  The Matrix Analysis of Vibration , 1979 .

[31]  Rafał Żbikowski,et al.  Design Guidelines for Flapping-Wing Micro UAVs , 2005 .

[32]  A K Soh,et al.  Experimental studies of the material properties of the forewing of cicada (Homóptera, Cicàdidae) , 2004, Journal of Experimental Biology.

[33]  M. Dickinson,et al.  Spanwise flow and the attachment of the leading-edge vortex on insect wings , 2001, Nature.

[34]  Daniel C. Kammer,et al.  Dynamic Response of a Radial Beam With Nonconstant Angular Velocity , 1987 .