Information Infrastructure Institute (iCUBE)
Aerospace Robotics Laboratory
Department of Aerospace Engineering, University of Illinois at Urbana-Champaign (Prof. Soon-Jo Chung)
Department of Electrical and Computer Engineering (Prof. Arun K. Somani)
Iowa State University
Improved results are coming soon at
https://netfiles.uiuc.edu/sjchung/www/index.html
Duration : 0:1:10
This is the first flight of Loki, the UAV that my design team has been designing and building since August 2006.
Duration : 0:8:40
Information Infrastructure Institute (iCUBE)
Aerospace Robotics Laboratory
Department of Aerospace Engineering
(Prof. Soon-Jo Chung)
Department of Electrical and Computer Engineering (Prof. Arun K. Somani)
Iowa State University
Koray Celik, Soon-Jo Chung, and Arun Somani, “MVCSLAM: Mono-Vision Corner SLAM for Autonomous Micro-Helicopters in GPS Denied Environments,” Proc. of the AIAA Guidance, Navigation, and Control Conference and Exhibit, Honolulu, HI, August 2008, AIAA-2008-6670.
Duration : 0:3:24
Aggressor II helicopter UAV demonstration of isted mode (or pilot directed mode) using a joystick. This helicopter UAV is a joint product of Viking Aerospace and Leptron Robotic Helicopters.
Duration : 0:8:13
Come visit us at: www.geocities.com/asmara.aerospace/. Hi Guys, this video was made in 2004 for the members in my UAV team.Nice souvenir to keep and watch 20years down the road for us.Perhaps its kind of nice to put it up in YouTube. UPMX was the successful prototype used before our best selling RJX1 was created.
Duration : 0:9:45
This video shows the Aggressor II UAV (joint product of Viking Aerospace and Leptron Industrial Helicopters) performing automatic takeoff, stop waypoints, cruise waypoints, auto homing mode, and automatic landing in light winds (~15-20 mph winds).
Duration : 0:4:15
This is the maiden flight of the 2nd Proof of Concept UAV (aka POC2) built by the Vanderbilt Aerospace Club during the 2008-2009 academic year. The aircraft has a 4′-wingspan, retractable landing gear, and is designed with a folding propeller, rotating wing, and folding V-tails in order to fit inside the team’s 16′-tall rocket. More information can be found at the Vanderbilt Aerospace Club website:
http://www.vanderbilt.edu/USLI
Duration : 0:1:39