parallel sessions

Tuesday September 18, 2007
Rotary- Flapping- Flexible-wing MAV systems
Chaired by : S. SHKARAYEV, University of Arizona, Tucson, AZ, USA

The effects of platform on low aspect ratio flexible wings

L. Zuo and J. Wang

Fluid Mechanics Institute Beijing University of Aeronautics and Astronautics, Beijing, China

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A small and lightweight aircraft for a wide range of flight velocity

Y. Otsuka, H. Tokutake, S. Sunada, T.Aoki

Osaka Prefecture University, Osaka, Japan

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Video (1) (2)  

B-UAV tracking control integrating planned yaw and longitudinal/lateral inputs

R. Mlayeh, L. Beji and A. Abichou

Ecole Polytechnique de Tunisie, Tunisia

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IG-500, The World Smallest Inertial Navigation System

T. Bonnevie, R. Syriani and A. Guinamard

SBG-Systems, France

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One way to design the control law of a mini- UAV

B. Lang, A. Bonneuil, L. Mairiniac, E. Poupon, E. Poudevigne, J-M. Friedt, P. Paquier

National Engineering Institute in Mechanics and Microtechnologies (ENSMM), Besançon, France

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Tuesday September 18, 2007
Fixed-wing MAV systems
Chaired by : C. LE TALLEC, ONERA, Chatillon, France

Automated Mission Planning for a Fleet of Micro Air Vehicles

P.-S. Huard

Ecole Nationale de l’Aviation Civile (ENAC)Toulouse, France

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Theoretical and Experimental Investigations of Aerodynamic Characteristics of MUAVs

V. Brusov, V. Petruchik

Moscow Aviation Institute, Moscow, Russia

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Experimental Investigations of Biplane Bimotor Fixed-Wing Micro Air Vehicles

C. Thipyopas, B. Bataillé, J.-M. Moschetta

Institut Supérieur de l’Aéronautique et de l’Espace (ISAE), Toulouse, France

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Experimental Comparison of Biplane and Monoplane MAVs

S. Serokhvostov, A. Kornushenko

Moscow Institute of Physics and Technology, Russia

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Development of a flying test bench using small UAVs

S. Furukawa, J. Fujinaga, H. Tokutake, S. Sunada

Osaka Prefecture University, Osaka, Japan

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Video (1)