The design optimisation of an insect-inspired micro air vehicle

AT Conn, SC Burgess, CS Ling, R Vaidyanathan

Research output: Contribution to journalArticle (Academic Journal)peer-review

6 Citations (Scopus)


Insect-inspired micro air vehicles (MAVs) have been the subject of extensive research in recent years for a range of novel applications. The current generation of vehicles, however, has yet to match even a fraction of the performance of insect flight, in particular with respect to manoeuvrability and payload capacity. Precise reproduction of insect-like flapping motion on the micro-vehicle scale holds significant potential to address this deficiency. The design and optimisation of this critical aspect of an insect-inspired MAV is the subject of this paper. The actuated flapping mechanism must deliver a high power output via complex wing kinematics, which should be dynamically adjustable for controlled flight without the need for traditional control surfaces. This paper first addresses several key flapping MAV design criteria that greatly influence the power requirements and aerodynamic forces for flight, through an assessment of design parameters such as wing length and wingbeat frequency. Two solutions are then proposed that meet these requirements while satisfying the current limitations of miniature actuation technologies and issues related to mechanism constraint. The first of these, the development of an ‘artificial muscle’ actuator is crucial to the feasibility of a highly adjustable, lightweight under-constrained flapping mechanism. A prototype ‘artificial muscle’ based on a silicone dielectric elastomer was tested and found to produce a strain output comparable to muscle. We also report the development of an alternative flapping mechanism solution utilising conventional rotary DC motors. The novel parallel crankrocker (PCR) mechanism produces similar wing kinematics to insects and, unlike previously developed DC motor-driven MAV flapping mechanisms, it allows dynamically adjustable control of the wing angle of attack. Aerodynamic testing of a PCR prototype found that it produced a maximum lift force of 6.4 g per wing pair at a wingbeat frequency of 13.2 Hz. Wind tunnel testing with high-speed flow visualisation footage showed that the measured lift forces are augmented by a bound leading edge vortex on the downstroke, which is the most important unsteady aerodynamic phenomenon attributed to insect flight.
Translated title of the contributionThe design optimisation of an insect-inspired micro air vehicle
Original languageEnglish
Pages (from-to)12 - 27
Number of pages15
JournalInternational Journal of Design & Nature and Ecodynamics
Publication statusPublished - 2008

Bibliographical note

Publisher: WIT Press

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