Synthesizing the control system of a small gliding unmanned aerial vehicle with high-aspect ratio wing

Synthesizing the control system of a small gliding unmanned aerial vehicle with high-aspect ratio wing

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...

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Veröffentlicht in:Russian aeronautics 2012-07, Vol.55 (3), p.251-258
Hauptverfasser: Grumondz, V. T., Polishchuk, M. A., Chertoryzhskaya, S. S., Krivoguz, A. S.
Format: Artikel
Sprache:eng
Schlagworte:
Aerials
Automotive Engineering
Control systems
Engineering
Flight Dynamics and Control of Flight Vehicles
Gliding
Unmanned aerial vehicles
Vehicles
Wings (aircraft)
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Beschreibung
Zusammenfassung: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.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799812030051