KU-Loiter MAV with Rotary Wings - ero-mav.......all informations about
Bae-Soon Kwan, Min-Gyu Chun and Kwang-Joon Yoon. Smart Robot Center in Institute of Intelligent Vehicle & System Tech. Dept. of Aerospace Information ...
KU-Loiter MAV with Rotary Wings Bae-Soon Kwan, Min-Gyu Chun and Kwang-Joon Yoon Smart Robot Center in Institute of Intelligent Vehicle & System Tech. Dept. of Aerospace Information Engineering, Konkuk University, 1 Hwayang-dong, Gwangjin-Gu, Seoul, Korea September 19, 2007
We designed a small flying robot with co-axial rotary wings. It consists of two rotor blade sets, electronic speed controller, electronic motor, RF receiver, a gyroscope, and lithium polymer battery, etc. We chose a co-axial rotor system to solve anti-torque rotation problem. Also, small flying robot with about 470mm diameter rotors has a camera to capture and transmit video images. The total weight of the designed flying robot is about 450g and it can fly about 10 minutes.
1. System properties The Vehicle Name : KU-Loiter Weight : 450g Rotor Dia. : 470mm Propulsion : 2 Electric Brushless Motor Endurance : 10 minutes Transmission system -
2.4GHz analog transmitter for the video downlink. (80mW) 72MHz RC transmitter for safety RC Link. (100mW)
Small vehicles tend to have problems with penetration into wind coupled with ... âStructuralâ hydrogen fuel cell powered flight March 2003. AeroVironment Inc ...
proven both efficient and successful in the past, UF has developed a 30 cm autonomous. MAV which is capable of ... accurate sensor deployment, followed by a.
Traffic monitoring (long endurance). ⢠Counter-drug ... 20 minute hover endurance. ⢠25 g payload .... Enhanced control power that can be. Hiller Bar. Rotor.
Sep 4, 2007 - Figure 2: Functional overview of the flight control system (FCS). ... late EMI/ESI interference caused by the brushless electric motor on the battery ... Gyroscope and accelerometer MEMS are integrated on the MAVPilot3 board.
Development and construction of hardware system for sensor interfacing, control calculation ... A strain gauge force balance is mounted to the sliding platform.
Advisor - Micro and Nano Systems â National Design and. Research .... IC Engines. ⢠Electric Motors (Nd Fe B) .... (Integrated GPS, Control Data. Processing and ...
manual mode, the autopilot switches to a basic navigation, circling around the ... The planner monitors the video and uses a Google Earth editor connected to ...
Sep 17, 2004 - including the retina, the low and high-level visual cortical ... of retinal and cortical neurons. They do .... subsumption architecture [3] according to.
electric motor and lithium polymer cells. ... integrated piezo-ceramic gyro sensor. .... control system the tilt angle is calculated in such a way that the camera ...
Systems. 1st US-European Micro Air Vehicle Technology. Demonstration and Assessment. Garmisch-Partenkirchen ... 2 gram electric motor. ⢠Lithium battery ... Means to control stability and to navigate are non trivial. 8. ..... integrated organism.
Sep 1, 2007 - autopilot with navigation sensors, a GPS unit, computer vision hardware, and .... sending navigation commands and tuning PID controller gains.
the years the group has matured the capability to design, manufacture, maintain .... to Competition Rules a worse case scenario of âwind gusting up to 10 m/sâ is.
The company EURO MC, in partnership with the association AERODES, and the .... With a same mass Lithium-Polymer battery, we hope for a duration of 30 ...
Apr 27, 2005 - Flight Tests planning. A. M. J. J. A. S. O .... Airport compatibility checks : Frankfurt + Far East Tour ... Far East Tour â 10th - 18th November 2005 ...
Challenges: Autopilot Design + Obstacle Avoidance + Resource Allocation ... o Additional challenges: online resource allocation and path planning. Cooperating agents ... Two systems forming independent decisions have the potential for conflicting dec
Flapping MAV. Smart Robot Center. Dept. of Aerospace Information Eng. Konkuk University. Seoul, Korea. Park Joon Hyuk, Kim Hyung Jin,. Kwang Joon Yoon ...
The IG-500G combines in the same miniature package an IG-500A, a GPS and a barometric altimeter. It thus provides precise orientation, as well as a GPS ...
Sep 21, 2007 - Endurance requirement: 15 minutes of stationary flight and 30 minutes of .... second selection round was performed (based on these enhanced ...
R.J. Lipton. The reachability problem requires exponential space. Technical Report 63, Yale. University, 1976. 14. G. Memmi and G. Roucairol. Linear algebra in ...
