Free flight testing and performance evaluation of a passively morphing ornithopter

Aimy Wissa, Jared Grauer, Nelson Guerreiro, James Hubbard, Cornelia Altenbuchner, Yashwanth Tummala, Mary I. Frecker, Richard Roberts

Research output: Contribution to journalArticle

8 Citations (Scopus)

Abstract

Unmanned Aerial Vehicles (UAVs) are proliferating in both the civil and military markets. Flapping wing UAVs, or ornithopters, have the potential to combine the agility and maneuverability of rotary wing aircraft with excellent performance in the low Reynolds number flight regimes. The purpose of this paper is to present new free flight experimental results for an ornithopter equipped with single degree of freedom compliant spines. The compliant spines are designed and optimized in terms of mass, maximum von-Mises stress, and desired wing bending deflections. The spines are inserted in an experimental ornithopter wing leading edge spar, in order to achieve a set of desired kinematics during the up and down strokes of a flapping cycle. The ornithopter is flown at Wright Patterson Air Force Base in the Air Force Research Laboratory Small Unmanned Air Systems (SUAS) indoor flight facility. Vicon® motion tracking cameras are used to track the motion of the vehicle for four different wing configurations. The effect of the presence of the compliant spine on the wings and body kinematics, as well as the leading edge spar deflection during free flight is presented in this paper. Several metrics were used to evaluate the vehicle performance with various compliant spine designs inserted in the leading edge spar of the wings. Results show that passively morphing the wings, via adding compliance in the leading edge spar, does not require additional power expenditure and is beneficial to the overall vertical and horizontal propulsive force production.

Original languageEnglish (US)
Pages (from-to)21-40
Number of pages20
JournalInternational Journal of Micro Air Vehicles
Volume7
Issue number1
DOIs
StatePublished - Mar 1 2015

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Free flight
Testing
Unmanned aerial vehicles (UAV)
Kinematics
Air
Vehicle performance
Maneuverability
Research laboratories
Reynolds number
Cameras
Aircraft

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

Wissa, A., Grauer, J., Guerreiro, N., Hubbard, J., Altenbuchner, C., Tummala, Y., ... Roberts, R. (2015). Free flight testing and performance evaluation of a passively morphing ornithopter. International Journal of Micro Air Vehicles, 7(1), 21-40. https://doi.org/10.1260/1756-8293.7.1.21
Wissa, Aimy ; Grauer, Jared ; Guerreiro, Nelson ; Hubbard, James ; Altenbuchner, Cornelia ; Tummala, Yashwanth ; Frecker, Mary I. ; Roberts, Richard. / Free flight testing and performance evaluation of a passively morphing ornithopter. In: International Journal of Micro Air Vehicles. 2015 ; Vol. 7, No. 1. pp. 21-40.
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Wissa, A, Grauer, J, Guerreiro, N, Hubbard, J, Altenbuchner, C, Tummala, Y, Frecker, MI & Roberts, R 2015, 'Free flight testing and performance evaluation of a passively morphing ornithopter', International Journal of Micro Air Vehicles, vol. 7, no. 1, pp. 21-40. https://doi.org/10.1260/1756-8293.7.1.21

Free flight testing and performance evaluation of a passively morphing ornithopter. / Wissa, Aimy; Grauer, Jared; Guerreiro, Nelson; Hubbard, James; Altenbuchner, Cornelia; Tummala, Yashwanth; Frecker, Mary I.; Roberts, Richard.

In: International Journal of Micro Air Vehicles, Vol. 7, No. 1, 01.03.2015, p. 21-40.

Research output: Contribution to journalArticle

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