Book Of Mavs

600. Weight. 270. The complete autonomous flight without human operations ... Size. 450. Weight. 500. The BYU system is very safe due to fully electrical hardware ... Tim McLAIN,. Chair of Dept of Mechanical Engineering, Brigham Young.
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Book Of Mavs MAV07

Outdoor Competition

Book Of Mavs MAV07 Size is given in millimeters, and weight in grams.

Kyuho Lee University of Florida, USA [email protected] Size

300

Weight

300 GATOR

Hesam Salehipour Isfahan University of Tachnology, Iran [email protected] Size

400

Weight

480

Delta platform wing flying at maximum speed of 22 m/s with full throttle setting, started from the very initial steps of UAV design.

HOMA

Lab of Aerodynmaics and Propulsion Supaero Toulouse, France [email protected] Size

400

Weight

250

Aircraft using biplan effect, and propulsed by contrarotative motors, Tyto is equipped with paparazzi guidance system, developed in ENAC.

TYTO

Murat Bronz Istanbul Technical University, Turkey [email protected] Size

500

Weight

266

Also equipped with the open source Paparazzi Autopilot, this plane was designed with Catia V5 CAD. The team is thinking to a smaller version, with a 300 mm wingspan, whose design is still going on.

STORM1

Book Of Mavs MAV07

Martin Mueller M.A.C., Germany [email protected] Size

460

Weight

245

The MAC 07 Mav project deploys an autonomous, delta shaped, electronically propelled fixed wing airplane made from expanded polypropylene for the outdoor task.

RED AIRCRAFT

Stephane Querry IPSA, France [email protected] Size

400

Weight

250/300 SQUIRREL

VAMUdeS Université de Sherbrooke, Canada [email protected] Size

480

Weight

400 THE BEAST

Michael Griffis University of Arizona, USA [email protected] Size

300

Weight

300 WILDCAT

Book Of Mavs MAV07

C. De Wagter Delft University, The Netherlands [email protected] Size

495

Weight

455

The design of Mavpilot3, equipped on that plane, was checked and improved by Royal Netherlands Navy.

HOLIDAY-50 AV

Lee Whitcher University of Sheffield (LEEDS) [email protected] Size

475

Weight

480

The structure is made of EPP to allow for a high degree of crashworthiness.

ZOOLANDER

Pierre-Selim Huard ENAC, France [email protected] Size

330

Weight

300

The use of paparazzi system by its designers...

SLAYER

Jared Yates Brigham Young University [email protected] Size

330

Weight

280

Brigham Young University is using a Procerus Technology autopilot system with an in-house developed user interface designed specifically for this competition.

BLACKOUT

Book Of Mavs MAV07

Kwang Yoon Konkuk University [email protected] Size

495

Weight

470

The Team developed a fixed wing micro air vehicle which can be piloted semi-automatically. In order to decrease its total weight and size, we chose a system that gets flight data from vehicle to ground control system.

KU-HAWK

Simone Duranti UAV Tech, Linkoping University, Sweden [email protected] Size

400

Weight

500

The PingWing is a new design carried out within the UAVTech Group and is capable of fully autonomous in-flightreconfigurable GPS-guided flight.

PING WING

Jeremy Tyler ENAC, Toulouse, France [email protected] Size

330

Weight

260 TWISTED LOGIC

Book Of Mavs MAV07

Outdoor Technological Demonstrators

Book Of Mavs MAV07

Hesam Salehipour Isfahan University of technology, Iran [email protected] Size

400

Weight

480 IUT-MAV

Hiroshi Tokutake Osaka Prefecture University, Japan [email protected] Size

600

Weight

270

The complete autonomous flight without human operations can be performed. In outdoor technology demonstrations, autonomous flight and auto landing will be shown.

MANTA

Stéphane Querry IPSA, France [email protected] Size

480

Weight

500

This bi-rotor UAV will be powered by the Micav 1.1 Autopilot.

DRIPPLE

Kwang Yoon Konkuk University [email protected] Size

110

Weight

43

This UAV has successfully flown for 7 minutes at the flight test.

KU-BATWING

Book Of Mavs MAV07

Lee Whitcher University of Sheffield, UK

Size

475

Weight

480 ZOOLANDER

Book Of Mavs MAV07

Indoor Competition

Book Of Mavs MAV07

Petter Muren Proxflyer, Norway [email protected] Size

200

Weight

25

This team will also bring record-breaking aircrafts... Watch indoor technological demonstrators too !!

PROXFLYER MAV07

Boris Bataillé Supaero, Toulouse, France [email protected] Size

200

Weight

100 CYCLOPE

Club Microdrones de Supaero Supaero, Toulouse, France [email protected] Size

355

Weight

490

The Br2C results of a long study on ducted fans. Pay attention to the very special shape of the shroud ! The aircraft is also equipped with the last version of Supaero Autopilot.

Br2C

Martin Mueller M.A.C., Germany [email protected] Size

350

Weight

unknown

This indoor Mav is based on mechanics of a commercially made RC helicopter.

HELICOPTER

Book Of Mavs MAV07

Stéphane Querry IPSA, France [email protected] Size

480

Weight

500

This bi-rotor UAV will be powered by the Micav 1.1 Autopilot.

DRIPPLE

Simone Duranti UAV Tech, Linkoping University, Sweden [email protected] Size

400

Weight

500

This Mav is a downsized version of the vehicle that has been awarded the best rotorcraft at Mav05.

LinkMAV

Patrice Rosier IMA, France [email protected] Size

350

Weight

250 Immersion Micro Auxiliary

Kwang Yoon Konkuk University [email protected] Size

470

Weight

450

The team chose a co-axial rotor system to solve anti-torque rotation problem.

KU-LOITER

Book Of Mavs MAV07

Gavin Kumar University of Arizona, USA [email protected] Size

300

Weight

192

A project carried out in only three months !

PHAETON (Mini-Vertigo)

C. De Wagter Delft University, The Netherlands [email protected] Size

295

Weight

16 DELFLY II

Dominique Bernard Supaero, Toulouse, France [email protected] Size

350

Weight

450 VISION

Travis Millet Brigham Young University, USA [email protected] Size

450

Weight

500

The BYU system is very safe due to fully electrical hardware and implemented failsafe.

FRENZY

Book Of Mavs MAV07

Jeremy Tyler ENAC, Toulouse, France [email protected] Size

330

Weight

260 TWISTED LOGIC

Book Of Mavs MAV07

Indoor Technological Demonstrators

Book Of Mavs MAV07

Petter Muren Proxflyer [email protected] Size

unknown

Weight

1g

The smallest remotely operated helicopter !

PICOFLYER-II

Kwang Yoon Konkuk University [email protected] Size

360

Weight

30,6

This vision sensing with landing gear system ornithopter can perform under 5m/s of head wind and has 15min of flight duration.

KU-BUZZ

Bill Sillin University of Arizona, USA [email protected] Size

130

Weight

8,6

An attempt to make the smallest remotely controlled ornithopter fly during at least one minute.

KOLIBRI

Jean-Claude Pesce Marseilles, France [email protected] Size

165

Weight

60 MICROx4

Book Of Mavs MAV07

James Roberts EPFL, Switzerland [email protected] Size

550

Weight

600 VTOLMAV

Damien Poinsot ONERA&SUPAERO, France [email protected] Size

750

Weight

1500

This project will try to perform translation and stationary flight, but also an automatic switch between both of them.

VERTIGO

Dominique Barnard SUPAERO, France dominique [email protected] Size

750

Weight

1000 CONTRAROTATIF

Gavin Kumar University of Arizona, USA [email protected] Size

300

Weight

192

A project carried out in only three months !

PHAETON (Mini-Vertigo)

Book Of Mavs MAV07

Judges Panels

Book Of Mavs MAV07

MAV07 Outdoor Competition  Gregg ABATE, US Air Force Research Laboratory Munitions Directorate, USA  Guy BROUQUIERES, French Federation for model aircraft (FFAM)  Nicolas DUFETELLE, UAV Executive, French MoD Procurement Agency (DGA), France  Patrick FABIANI, Head of Control & Flight Dynalmics Dept, ONERA, France  Tim McLAIN, Chair of Dept of Mechanical Engineering, Brigham Young University, UT, USA  Evgeny SOKOLOV, Head of Laboratory, Central Research and Developing Institute of Robotics and Technical Cybernetics, Russia

MAV07 Indoor Competition  Aurelia AUTRAN, Mini-UAV system engineer, French MoD Procurement Agency (DGA), France  Christian BOLLER, Professor in Smart Structural Design, University of Sheffield, UK  Guy BROUQUIERES, French Federation for model aircraft (FFAM)  John JOHNSON, Aviation and Missile Technology, U.S. Army International Technology Center-Atlantic, London, UK  Surya SURAMPUDI, European Office of Aerospace Research and Development, UK  Hiroshi TOKUTAKE, Dept of Aerospace Engineering, Osaka Prefecture University, Japan

Director of Flight Operations  Philippe BATAILLE,

Direction Générale de L’Aviation Civile (DGAC)