MATHEMATICAL MODELING OF THE TERMINATION FLIGHT CONTROL ALGORITHM FOR UNMANNED AERIAL VEHICLE

Authors

  • Ya. Kondrashov National Aviation University
  • A. Arutyunyan National Aviation University
  • I. Kravchyshyn National Aviation University

DOI:

https://doi.org/10.18372/2310-5461.5.5028

Keywords:

termination control, landing, mathematical modeling, unmanned aerial vehicles

Abstract

The efficiency of the algorithm of control synthesis is evaluated by means of mathematical modeling by a methodicalerror of the guidance of the gliding aircraft descending to the omnidirectional radio beacon. It’s shown,that the control synthesis results in formation of convergent stable process of motion parameters variation, andthe guidance error is generally determined by navigational errors of current phase coordinates determination.

References

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Кринецкий Е. И. Системы самонаведения/ Е.И.Кринецкий. — М. : Машиностроение, 1970. — 236 с.

Каменков Е. Ф. Маневрирование спускаемых систем/ Е. Ф. Каменков. — М. : Машиностроение, 1983. — 184 с.

Kondrashov Ya., Arutyunyan A., Kravchyshyn I. The method of prediction of unmanned aerial vehicle motion parameters. Матеріали IХ міжнар. наук.-техн. конф. «АВІА-2009». —Т. 2. — К. :НАУ, 2009. — С. 9.29—9.32.

Kondrashov Ya., Arutyunyan A., Kravchyshyn I. Principles of termination control of unmanned aerial vehicles flight path/ Наукоємні технології. — К. : НАУ, 2009. — С. 45—48.

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Published

2010-05-11

How to Cite

Kondrashov, Y., Arutyunyan, A., & Kravchyshyn, I. (2010). MATHEMATICAL MODELING OF THE TERMINATION FLIGHT CONTROL ALGORITHM FOR UNMANNED AERIAL VEHICLE. Science-Based Technologies, 5(1), 44–48. https://doi.org/10.18372/2310-5461.5.5028

Issue

Vol. 5 No. 1 (2010)

Section

Aeronautical systems

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