Abstract In this paper, we consider a problem of synthesizing the control system of a small gliding (unpowered) aerial vehicle (GAV) with a high-aspect ratio wing (λ ≈ 10). This wing makes it possible to increase significantly the flight range and improve the maneuvering characteristics of the aerial vehicle itself.
Synthesizing the control system of a small gliding unmanned aerial vehicle with high-aspect ratio wing
Russian Aeronautics (Iz VUZ) ; 55 , 3 ; 251-258
2012-07-01
8 pages
Article (Journal)
Electronic Resource
English
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