SCALABLE DESIGN APPROACH TO ANALYZE FLIGHT MECHANICAL PERFORMANCE OF TILT-WING UAVS
International Council of the Aeronautical Sciences
01.01.2018
13 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Design and Flight Testing of Inflatable Wing UAVs with Ailerons
British Library Conference Proceedings | 2011
|Flight testing experiments with tilt-wing aircraft
Engineering Index Backfile | 1959
|Design of flight control system for quad tilt-wing UAV
IEEE | 2015
|