The Use of a Fuzzy Logic to Eliminate an Error in Measuring the Flight Altitude of the W-3 „Sokół” Helicopter

Along with the growing technology, helicopters are equipped with increasingly complex avionics and operational control systems. Such devices use a variety of input signals in order to enhance their performance. Owing to the use of electronic control systems, modern helicopters have a wide range of p...

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Main Authors: Bujak Krystian, Grzesik Norbert, Kuźma Konrad
Format: Article
Language:English
Published: Sciendo 2018-03-01
Series:Journal of KONBiN
Subjects:
Online Access:https://doi.org/10.2478/jok-2018-0007
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spelling doaj-dcf30540ddc54a0abfc788ef45118fb72021-09-06T19:41:43ZengSciendoJournal of KONBiN2083-46082018-03-0145112514110.2478/jok-2018-0007jok-2018-0007The Use of a Fuzzy Logic to Eliminate an Error in Measuring the Flight Altitude of the W-3 „Sokół” HelicopterBujak Krystian0Grzesik Norbert1Kuźma Konrad2Air Force Academy in Dęblin; Wyższa Szkoła Oficerska Sił Powietrznych, Wydział LotnictwaAir Force Academy in Dęblin; Wyższa Szkoła Oficerska Sił Powietrznych, Wydział LotnictwaAir Force Academy in Dęblin; Wyższa Szkoła Oficerska Sił Powietrznych, Wydział LotnictwaAlong with the growing technology, helicopters are equipped with increasingly complex avionics and operational control systems. Such devices use a variety of input signals in order to enhance their performance. Owing to the use of electronic control systems, modern helicopters have a wide range of possibilities, both in terms of manoeuvrability and combat. The article presents a case study of designing equipment control systems on the example of a radio altimeter, which is mounted onboard the W-3 “Sokół” helicopter. The primary assumption was to design a fuzzy controller using FuzzyLogic Toolbox in the Matlab software package that will facilitate similar results, and, above all, will eliminate the altitude measurement error resulting from the bank of a helicopter.https://doi.org/10.2478/jok-2018-0007radio altimeterfuzzy logichelicopter w-3 „sokół”
collection DOAJ
language English
format Article
sources DOAJ
author Bujak Krystian
Grzesik Norbert
Kuźma Konrad
spellingShingle Bujak Krystian
Grzesik Norbert
Kuźma Konrad
The Use of a Fuzzy Logic to Eliminate an Error in Measuring the Flight Altitude of the W-3 „Sokół” Helicopter
Journal of KONBiN
radio altimeter
fuzzy logic
helicopter w-3 „sokół”
author_facet Bujak Krystian
Grzesik Norbert
Kuźma Konrad
author_sort Bujak Krystian
title The Use of a Fuzzy Logic to Eliminate an Error in Measuring the Flight Altitude of the W-3 „Sokół” Helicopter
title_short The Use of a Fuzzy Logic to Eliminate an Error in Measuring the Flight Altitude of the W-3 „Sokół” Helicopter
title_full The Use of a Fuzzy Logic to Eliminate an Error in Measuring the Flight Altitude of the W-3 „Sokół” Helicopter
title_fullStr The Use of a Fuzzy Logic to Eliminate an Error in Measuring the Flight Altitude of the W-3 „Sokół” Helicopter
title_full_unstemmed The Use of a Fuzzy Logic to Eliminate an Error in Measuring the Flight Altitude of the W-3 „Sokół” Helicopter
title_sort use of a fuzzy logic to eliminate an error in measuring the flight altitude of the w-3 „sokół” helicopter
publisher Sciendo
series Journal of KONBiN
issn 2083-4608
publishDate 2018-03-01
description Along with the growing technology, helicopters are equipped with increasingly complex avionics and operational control systems. Such devices use a variety of input signals in order to enhance their performance. Owing to the use of electronic control systems, modern helicopters have a wide range of possibilities, both in terms of manoeuvrability and combat. The article presents a case study of designing equipment control systems on the example of a radio altimeter, which is mounted onboard the W-3 “Sokół” helicopter. The primary assumption was to design a fuzzy controller using FuzzyLogic Toolbox in the Matlab software package that will facilitate similar results, and, above all, will eliminate the altitude measurement error resulting from the bank of a helicopter.
topic radio altimeter
fuzzy logic
helicopter w-3 „sokół”
url https://doi.org/10.2478/jok-2018-0007
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