Monday afternoon / 17 September 2007
 
Session 1      MAV Design, Aerodynamics & Propulsion 

Chaired by :  C. BOLLER, University of Sheffield, Leeds, UK

1430 1455 1520
 
MAV07-PLE1A 

Aerodynamics of VTOL Micro Air Vehicles

S. Shkarayev, University of Arizona, Tucson, AZ ; J.-M. Moschetta and B. Bataillé, SUPAERO, Toulouse, France

 
MAV07-PLE1B 

Plasma Flow Control at MAV Reynolds Numbers

B. Göksel, Electrofluidsystems Ltd. Holding, Berlin, Germany;

D. Greenblatt, R. Bannasch, I. Rechenberg. O. Paschereit, TU Berlin, Berlin, Germany

 
MAV07-PLE1C 

Presentation of the MAVDEM project

A. Joulia and C. Le Tallec, ONERA, Chatillon, France

 
 
 
Monday afternoon / 17 September 2007
 
Session 2      MAV Navigation and Mission Planning 

Chaired by :  P. VÖRSMANN, Technische Universität Braunschweig, Germany

1615 1640 1705
 
MAV07-PLE2A 

Path Planning for a Fixed Wing Micro Air Vehicle in Fuzzy Quadtree Framework

S. Ghosh, A. Halder and M. Sinha, Indian Institute of Technology (IIT), Kharagpur, India

 
MAV07-PLE2B 

Flight Control for Micro Aerial Vehicles Using Artificial Intelligence

T. Krüger, Technische Universität Braunschweig, Germany ; L. Krüger, Mavionics, Braunschweig, Germany ;  A. Kuhn, Andata Development Technologies, Hallein, Austria ;

J. Axmann and P. Vörsmann, Technische Universität Braunschweig, Germany 

 
MAV07-PLE2C 

Soaring behaviors in UAVs : 'animat' design methodology and current results

S. Doncieux, G. Tatur, J.-B. Mouret and J.-A. Meyer, Institut des Systèmes Intelligents et Robotique, LIP6, Paris, France

 
Tuesday afternoon / 18 September 2007
 
Session 3      Flapping-wing MAVs, fluid-structure interaction 

Chaired by :  W. SHYY, University of Michigan, Ann Arbor, MI

1315 1340 1405
 
MAV07-PLE3A 

Experimental Elastic Deformation Characterization of a Flapping-Wing MAV using Visual Image Correlation

K. Stewart, R. Albertani, University of Florida, Shalimar, FL

 
MAV07-PLE3B 

The Use of Resonant Structures for Miniaturizing FMAVs

C. Bolsman, Delft University of Technology, The Netherlands ; B. Palsson, Chalmers University of Technology, Sweden ; H. Goosen, R. Munnig Schmidt and F. van Keulen, Delft University of Technology, The Netherlands 

 
MAV07-PLE3C 

Unsteady Mechanical Aspects of Flexible Wings: an Experimental Investigation Applied to Biologically Inspired MAVs.

R. Albertani, REEF, University of Florida, FL ; B. Stanford and P. Ifju, University of Florida, Gainesville, FL

 
 
 
Thursday morning / 20 September 2007
 
Session 4      Sense and Avoid, Autopilots for MAV Systems 

Chaired by :  T. HAMEL, I3S, UNSA-CNRS, Nice, France

0900 0925 0950
 
MAV07-PLE4A 

Flight Controller Design and Autonomous Flight Tests of 60cm-sized UAV

J. Fujinaga, H. Tokutake and S. Sunada, Osaka Prefecture University, Japan

 
MAV07-PLE4B 

Strategies for the Implementation of a Sense and Avoid System for Unmanned Aerial Vehicles

J. B. Park and P. Vörsmann, Technische Universität Braunschweig, Germany 

 
MAV07-PLE4C 

Design concepts for a novel attitude sensor for Micro Aerial Vehicles based on dragonfly ocellar vision

G. Stange, R. Berry and J. van Kleef, Australian National University, Canberra, Australia

 
 
Thursday morning / 20 September 2007
 
Session 5      Flapping-MAVs, Flight Control and Navigation 

Chaired by :  J. A. MULDER, Delft University of Technology, The Netherlands

1115 1140 1205
 
MAV07-PLE5A 

A Dynamic Model and System Identification Procedure for the Autonomous Ornithopter

B. Malladi, R. Krashanitsa, D. Silin and S. Shkarayev, University of Arizona, Tucson, AZ

 
MAV07-PLE5B 

Flapping-wing flight in bird-sized UAVs for the ROBUR project: from an evolutionary optimization to a real flapping-wing mechanism

E. de Margerie, J.-B. Mouret, Institut des Systèmes Intelligents et Robotique, LIP6, Paris, France ; T. Ravasi, P. Martinelli and C. Grand, Institut Universitaire de Technologie de Cachan, France

 
MAV07-PLE5C 

Experimental investigation on the aft-element flapping of a two-element airfoil at high attack angle

T. Guang-kun, S. Gong-Xin and S. Wen-han, Beijing University of Aeronautics and Astronautics (BUAA), Beijing, China

 
 
Friday morning / 21 September 2007
 
Session 6      Rotary-wing MAV Systems 

Chaired by :  P. DOHERTY, Linköping University, Sweden

1030 1055 1120
 
MAV07-PLE6A 

Rotorcraft Using Minimal Sensing For Fully Autonomous Control

J. Roberts, T. Stirling, J.-C. Zufferey and D. Floreano, Laboratory of Intelligent Systems, Ecole Polytechnique de Lausanne (EPFL), Lausanne, Switzerland

 
MAV07-PLE6B 

Modeling and development of a quadrotor UAV

G. Pradel, K. Benzemrane, G. Damm, N. Azouz, Informatique, Biologie Intégrative et Systèmes Complexes (IBISC), Université d’Evry, Evry, France

 
MAV07-PLE6C 

Nonlinear Attitude and Position Control of a Micro Quadrotor using Sliding Mode and Backstepping Techniques

P. Adigbli, Institute of Automatic Control Engineering, Technische Universität München, Germany ; J.-B. Mouret, S. Doncieux, J.-A. Arcady, Institut des Systèmes Intelligents et Robotique, LIP6, Paris