CONTROL ALGORITHM AIRCRAFT UNDER SUDDEN STEERING SURFACE DAMAGE

Authors

  • В. М. Казак National Aviation University
  • Т. В. Будзинська National Aviation University
  • В. Ю. Міщерякова National Aviation University

DOI:

https://doi.org/10.18372/2310-5461.1.5193

Keywords:

control of the aircraft, steering damage, flight, aviation, aircraft, airframe, aerodynamics, wing, flight control

Abstract

An analysis of damage influenece on control surfaces was made. The mathematic model of such influence and methods of aircraft’s controllability resumption were developed.

References

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Зарубежное военное обозрение. — М.: Воениздат, 1992. — № 9.

Казак В. М. Методика вибору алгоритму планування експерименту для проведення досліджень впливу ушкоджень поверхні ЛА на його керованість // Вісник НАУ. — 2003. — № 1. — С. 87—90.

Комаров А. А. Надежность воздушных судов. — К. : КМУГА, 1995. — 416 с.

Симонов М. П. Из истории создания СУ-27// Крылья Родины. — М. : МО, 1999. — № 7. — С. 3—7.

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How to Cite

Казак, В. М., Будзинська, Т. В., & Міщерякова, В. Ю. (2009). CONTROL ALGORITHM AIRCRAFT UNDER SUDDEN STEERING SURFACE DAMAGE. Science-Based Technologies, 1(1), 9–12. https://doi.org/10.18372/2310-5461.1.5193

Issue

Vol. 1 No. 1 (2009)

Section

Engineering

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