| Tuesday morning 18 September 2007 |
Parallel session A Rotary- Flapping-
Flexible-wing MAV systems Chaired by : S. SHKARAYEV, University of Arizona, Tucson, AZ, USA |
Parallel Session B Fixed-Wing MAV
Systems Chaired by : C. LE TALLEC, ONERA, Chatillon, France |
| 1030 |
MAV07-PARA1 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 |
MAV07-PARB1 Automated Mission Planning for a Fleet of Micro Air Vehicles P.-S. Huard Ecole Nationale de l’Aviation Civile (ENAC), Toulouse, France |
| 1050 |
MAV07-PARA2 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 |
MAV07-PARB2 Theoretical and Experimental Investigations of Aerodynamic Characteristics of MUAV V. Brusov, V. Petruchik Moscow Aviation Institute, Moscow, Russia |
| 1110 |
MAV07-PARA3 B-UAV tracking control integrating planned yaw and longitudinal/lateral inputs R. Mlayeh, L. Beji and A. Abichou Ecole Polytechnique de Tunisie, Tunisia |
MAV07-PARB3 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 |
| 1130 |
MAV07-PARA4 IG-500, the World Smallest Inertial Navigation System T. Bonnevie, R. Siryani, A. Guinamard SBG-Systems, France |
MAV07-PARB4 Experimental Comparison of Biplane and Monoplane MAVs S. Serokhvostov, A. Kornushenko Moscow Institute of Physics and Technology, Russia |
| 1150 |
MAV07-PARA5 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 |
MAV07-PARB5 Development of a flying test bench using small UAVs S. Furukawa, J. Fujinaga, H. Tokutake, S. Sunada Osaka Prefecture University, Osaka, Japan |