Abstract The motion of blades relative to the disk wing at the extension and retraction modes is defined. The general solution is obtained including the fuselage motion under the action of control or external disturbance.
A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)
Russian Aeronautics ; 59 , 4 ; 507-516
2016-10-01
10 pages
Article (Journal)
Electronic Resource
English
Mathematical model of balancing for a vertical takeoff and landing disk-wing aircraft
Springer Verlag | 2010
|Mathematical model of balancing for a vertical takeoff and landing disk-wing aircraft
Online Contents | 2010
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