Detail publikace

Diagnostic parameters determination of aircraft hydraulic system

TŘETINA, K. CÄSAR, T.

Originální název

Diagnostic parameters determination of aircraft hydraulic system

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

The article presents methodology for application of information theory for selection of hydraulic system diagnostic parameters. Changes in technical state of the system are accompanied by a set of symptoms. Method of determining information value of each symptom by information theory is presented. A set of technical conditions and set of symptoms for a simple hydraulic system are determined. Matrix of technical state describing relations between technical conditions and symptoms is constructed. The four symptoms are determined by matrix analysis with use of information theory. These symptoms are chosen as diagnostic parameters and provide the most information about technical state of the hydraulic system.

Klíčová slova

hydraulic system, diagnostic symptom, technical condition, matrix of technical state, entropy, diagnostic parameter selection, information theory

Autoři

TŘETINA, K.; CÄSAR, T.

Vydáno

11. 1. 2019

ISBN

978-80-214-5696-9

Kniha

Research and Education in Aircraft Design 2018

Strany od

189

Strany do

196

Strany počet

8

BibTex

@inproceedings{BUT157733,
  author="Karel {Třetina} and Tomáš {Cäsar}",
  title="Diagnostic parameters determination of aircraft hydraulic system",
  booktitle="Research and Education in Aircraft Design 2018",
  year="2019",
  pages="189--196",
  doi="10.13164/conf.read.2018.18",
  isbn="978-80-214-5696-9"
}