SOKOL Unmanned Aerial System

Authors

  • Jiri Kuzdas Department of UAS, Air Force and Air Defence Technical Institute, Praha, Czech Republic
  • Z. Pátek VZLU Aerospace Research and Test Establishment, Praha, Czech Republic

Keywords:

Unmanned aerial system, unmanned aerial vehicle

Abstract

The SOKOLunmanned aerial system is intended for the military, police and the integrated rescue system operations. The system consists of the light small SOKOLunmanned airplane, the catapult launcher with the rubber bungee cords and the control system whose main part is the ruggedized PC tablet. The system features versatility, compactness and robustness that allow performing different missions at adverse weather and terrain conditions. The SOKOLmeets the actual status of the Czech legislation of the UAV operations.

Author Biography

  • Jiri Kuzdas, Department of UAS, Air Force and Air Defence Technical Institute, Praha, Czech Republic

    USZaBS, Director

References

PÁTEK, Z. Zkušební proud vzduchu v aerodynamickém tunelu ø 3 m (in Czech) [VZLÚ Report R-3401/02]. Praha: VZLÚ, 2002.

ČERVINKA, J. Metodika měření v tunelu 3m LSWT - parametry zkušebního proudu (in Czech) [VZLÚ Report R-5022]. Praha: VZLÚ, 2010.

ČERVINKA, J., ZABLOUDIL, M. Metodika měření modelů letadel v tunelu 3m LSWT (in Czech) [VZLÚ Report R-5031]. Praha: VZLÚ, 2010.

BITTNER, M.: Návod k použití programu Tunel pro tenzometrické váhy (in Czech) [VZLÚ Directive PI-ANR-22]. Praha: VZLÚ, 2006.

ČERVINKA, J. Metodika simulace vrtulových pohonných jednotek (in Czech) [VZLÚ Report R-5199]. Praha: VZLÚ, 2011.

BARLOW, JB., RAE, WH. and POPE, A. Low-Speed Wind Tunnel Testing. New York: Wiley, 1999.

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Published

05-11-2015

Issue

Section

Technical Information

Categories

How to Cite

SOKOL Unmanned Aerial System. (2015). Advances in Military Technology, 10(1), 99-109. https://www.aimt.cz/index.php/aimt/article/view/1057

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