The Proceedings of the Transportation and Logistics Conference
Online ISSN : 2424-3175
2007.16
Session ID : 3211
Conference information
3211 Transportation system of QTW (Quad Tilt Wing)-UAV (Unmanned Aerial Vehicle)
Gaku KIMURADaisuke HIRABAYASHIMitsuhiro FURUYAKenta YASUDA
Author information
CONFERENCE PROCEEDINGS FREE ACCESS

Details
Abstract
QTW (Quad Tilt Wing)-UAV (Unmanned Aerial Vehicle) can realize the vertical takeoff and landing, and hovering flight that seems to be the helicopter, and the high cruising speed that seems to be the fixed-wing aircraft by changing an angle of a rotors and wings by using tilt mechanism. We develop the original QTW-UAV, PFCS (Primary Flight Control System) and experimental method for flight test. The result of the flight test shows the proper flight through the helicopter mode to the fixed-wing aircraft mode is realized by using our thought.
Content from these authors
© 2007 The Japan Society of Mechanical Engineers
Previous article Next article
feedback
Top