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An investigation into the longitudinal dynamics and control of a flapping wing micro air vehicle at hovering flight

Published online by Cambridge University Press:  04 July 2016

K. Loh ,
M. Cook  and
P. Thomasson
K. Loh
Affiliation:
Flight Dynamics Group, College of Aeronautics, Cranfield University, UK
M. Cook
Affiliation:
Flight Dynamics Group, College of Aeronautics, Cranfield University, UK
P. Thomasson
Affiliation:
Flight Dynamics Group, College of Aeronautics, Cranfield University, UK
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Abstract

This paper describes the research into the flight dynamics modelling and flight control of a flapping wing micro aerial vehicle (MAV). The equations of motion based on a multi-body representation of the vehicle and the flapping wings were derived and form the basis for the simulation program, which was developed using MATLAB and SIMULINK. The aerodynamic forces were obtained through experimental methods and form the basis for the aerodynamic model.

The hovering and low speed flight of the MAV was investigated using a SIMULINK simulation model. Various flight control concepts, inspired by observation of insect and bird flight, were investigated in some detail. The concepts include the control of flap frequency, flap and pitch phasing (wing beat kinematics) and shift in centre of gravity position. The paper concludes with a comparison of the control concepts and their feasibility for a practical vehicle application.

Type
Research Article
Information
The Aeronautical Journal , Volume 107 , Issue 1078 , December 2003 , pp. 743 - 753
Copyright
Copyright © Royal Aeronautical Society 2003 

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