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Mini UAVs Development

Mini UAVs Development. Project AURYON. Jérôme De Miras Boris Vidolov. History. - Autonomous fly Automatic control Embedded systems 3D Real time simulation - UAV prototypes development One Flyer Four blades - International Universities Mini UAVs Competition. One Flyer.

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Mini UAVs Development

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  1. Mini UAVs Development Project AURYON Jérôme De MirasBoris Vidolov Journées Micro-drones Toulouse : 1/10/03

  2. History • - Autonomous fly • Automatic control • Embedded systems • 3D Real time simulation • - UAV prototypes development • One Flyer • Four blades • - International Universities Mini UAVs Competition Journées Micro-drones Toulouse : 1/10/03

  3. One Flyer Journées Micro-drones Toulouse : 1/10/03

  4. Four Blades Journées Micro-drones Toulouse : 1/10/03

  5. Project AURYON Aerial Navigation Unmanned with Outdoor Robotic eYe Approach • Development based on realistic and available techniques • Integration of existing technology solutions "of the market" Journées Micro-drones Toulouse : 1/10/03

  6. Team Jérôme De miras Boris Vidolov Etienne Arnoult Stéphane Bonnet Professors & researchers Technical experts Students Coordination Management - Communication - Sponsoring Mechanical design, Engine design, Computer simulation, Manufacturing Students Mecanical engineering Avionics system, Video & transmission system, Simulator design, Web site Students Computer Science Total :  30 members Journées Micro-drones Toulouse : 1/10/03

  7. Planning June 2005 Today June 2004 Tests & improvements Manufacturing Dimensionning & design Technical solutions Function analysis Technical survey March 2003 Throughout the project Journées Micro-drones Toulouse : 1/10/03

  8. Technical Summary Propulsion Energy and motorization choices. Structure Lift, Dimensions and Security. Data processing and embarked electronic Main integrated functions, some algorithm results Journées Micro-drones Toulouse : 1/10/03

  9. Propulsion • Determination of the Power to develop : Hypothesis considered: Result : Ppropuslion = 900W, or 1.2cv Main solution :Thermal A 2 or 4 cycles engine, from 5 to 10cc, propulsion module weight 1,2 kg. What kind of energy? Flight range set : 35 min Secondary solution :Electrical Ions-Polymeres batteries Journées Micro-drones Toulouse : 1/10/03

  10. Structure General shape Maximum thrust minimum dimensions : Ø rotor = highest dimension Thermal propulsion : 2 or 4 cycles engine, module weight 1,2 kg. Motion : Counter-rotating propellers with variable pitches, 2 cyclic boards with electrical mixing. Security, protection : Composite shield Camera : 2 axis of rotation Journées Micro-drones Toulouse : 1/10/03

  11. Functional diagram Analogy information flux Numeric information flux Journées Micro-drones Toulouse : 1/10/03

  12. Embedded functions Emission/reception data Obstacle detection GPS tracking trajectory Take off and landing Flightstabilization + Video transmission Journées Micro-drones Toulouse : 1/10/03

  13. Ground station Saving data (video + sensor data) Emission / Reception of data Emission of order Order interpretation + Trajectory definition. Visualization of received data. Power source Journées Micro-drones Toulouse : 1/10/03

  14. Simulation platform On-line real-time data service. Simulation of physical models. + Virtual reality Trajectory definition. Visualization of received data (by software in the loop). Journées Micro-drones Toulouse : 1/10/03

  15. Some developments Journées Micro-drones Toulouse : 1/10/03

  16. Test platform Journées Micro-drones Toulouse : 1/10/03

  17. Obstacle detection Journées Micro-drones Toulouse : 1/10/03

  18. Ground Station Journées Micro-drones Toulouse : 1/10/03

  19. Order interface Journées Micro-drones Toulouse : 1/10/03

  20. Electrical Helicopter Journées Micro-drones Toulouse : 1/10/03

  21. Experimentation Journées Micro-drones Toulouse : 1/10/03

  22. Questions ? Journées Micro-drones Toulouse : 1/10/03

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