PARAMETRIC ANALYSIS OF LONGITUDINAL STABILITY UNMANNED AERIAL VEHICLE

Authors

  • Ievgen Udartsev National Aviation University
  • Alexandr Bondar National Aviation University
  • Ievgen Plakhotniuk National Aviation University

DOI:

https://doi.org/10.18372/2306-1472.56.5411

Keywords:

analysis, longitudinal static stability in overload, soot blowing propellers, Unmanned Aerial Vehicle

Abstract

We consider the aerodynamic characteristics of unmanned aircraft container type, which were obtained in a wind tunnel and refined amended by soot blowing elements propeller system and the influence of the earth's surface. The estimation of longitudinal static stability and its dependence on altitude, damping, coordinates of center of gravity, shoulder horizontal tail, wings rejection of mechanization. The variation of these parameters enables to optimize balancing system with minimal losses.

Author Biographies

Ievgen Udartsev, National Aviation University

Udartsev Ievgen. Doctor of Engineering. Professor.

National Aviation University, Kyiv, Ukraine.

Research area: unsteady aerodynamics.

Alexandr Bondar, National Aviation University

Bondar Alexandr. Research Assistant.

Department of Aerodynamics and Flight Safety of Aircraft, National Aviation University, Kyiv, Ukraine.

Education: National Aviation University, Kyiv, Ukraine (2010).

Research area: aerodynamics of aircraft.

Ievgen Plakhotniuk, National Aviation University

Plakhotniuk Ievgen. Postgraduate Student.

Department of Air Navigation Systems, National Aviation University, Kyiv, Ukraine.

Education: National Aviation University, Kyiv, Ukraine (2010).

Research area: unmanned aircraft.

References

Lebedev, A.A.; Chernobrovkyn, L.S. 1973. Flight dynamics of Unmanned Aerial Vehicles. Moscow, Engineering. 616 p. (in Russian).

Mikeladze, V.G. 1996. General aviation, recommendations for designers. Moscow, Aerokon. 298 p. (in Russian).

Mkhitaryan, A.M. 1976. Aerodynamics. Moscow, Mechanical Engineering. 446 p. (in Russian).

Ostoslavskyy, I.V.; Kalachev, G.S. 1951. Longitudinal Stability and upravlyaemost Airplane. Moscow, State Publishing House of Defense Industry. 367 p. (in Russian).

Ostoslavskyy, I.V.; Strazheva, I.V. 1965. Flight dynamics. Stability and control of aircraft. Moscow, Mechanical Engineering. 468 p. (in Russian).

Sylkova, V.I. 2009. Unmanned aerial vehicles. Methods of approximate calculations of the main parameters and characteristics. Kyiv, CSRI AF UKRAINE, 2009. 302 p. (in Russian).

How to Cite

Udartsev, I., Bondar, A., & Plakhotniuk, I. (2013). PARAMETRIC ANALYSIS OF LONGITUDINAL STABILITY UNMANNED AERIAL VEHICLE. Proceedings of National Aviation University, 56(3), 22–28. https://doi.org/10.18372/2306-1472.56.5411

Issue

Section

AEROSPACE SYSTEMS FOR MONITORING AND CONTROL