Diagnostics of typical faults that cause extra situation in flight

Authors

  • Василий Николаевич Казак National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058, Ukraine
  • Дмитрий Олегович Шевчук National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058, Ukraine
  • Михаил Андреевич Васильев National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058, Ukraine

DOI:

https://doi.org/10.15587/2313-8416.2014.33560

Keywords:

aircraft, extra situation, faults, control system, reconfiguration, control surfaces, diagnostics

Abstract

This article is about typical aircraft system and components faults that cause to extra situation in flight. It is given statistic data about common control surfaces faults. It is analyzed three main types of faults: sensors faults, actuators, components faults and diagnostic how these faults affect on aircraft control system. It is developed fault diagnostics methodic in flight.

Author Biographies

Василий Николаевич Казак, National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058

Doctor of Technical Sciences, Professor

Automation and Energy Management Department

Дмитрий Олегович Шевчук, National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058

PhD

Automation and Energy Management Department

Михаил Андреевич Васильев, National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058

Postgraduate student

References

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Skripchenko, V. G. (2005). Primeneniye matematicheskogo modelirovaniya I teoretycheskych metodov pri analyze osobich sluchayev vzleta I posadki vozdushnih sudov [Mathematical modeling and theoretical methods usage for extra situation analyze on aircraft take off and landing stage]. Moscow, 483.

Published

2014-12-22

Issue

Section

Technical Sciences