The design and simulation of an automated de-icing control system in the aircraft diamond DA42

• Autorzy: Gliwa W. , Żyluk A. , Grzesik N. , Kuźma K.

Identyfikatory

DOI

10.5604/01.3001.0012.7850

• Języki publikacji: EN

Abstrakty

EN

The article discusses the automatic control system of the Diamond DA42 aircraft anti-icing system. In the analysis of the issue of icing, four parameters were taken into account: air temperature, cloud humidity, temperature of the aircraft and precipitation. On the basis of the initial parameters, the authors determined the icing intensity, which is likely to occur on the aircraft skin. By automating the activities related to the activation of the de-icing system, it is possible to significantly relieve the pilot and increase the safety of air operations, particularly in conditions, which are conducive to the formation of icing. The authors performed a thirty-minute electronic simulation of the flight in real atmospheric conditions. The article discusses the obtained results of the simulation. Designed system uses fuzzy logic. The system inputs and output were determined and fuzzy expert inference system was developed in MATLAB software and Fuzzy Logic Toolbox. The proper system work was verified with use of MATLAB/Simulink software. Use of that kind of systems can significantly relieve the pilot and increase the safety of air operations, particularly in conditions, which are conducive to the formation of icing.

Słowa kluczowe

EN

anti-icing installation; icing; Diamond DA42; aircraft; general aviation; MATLAB

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2018
• Tom: Vol. 25, No. 4
• Strony: 525--532
• Opis fizyczny: Bibliogr. 9 poz., rys.

Twórcy

autor

Gliwa W.

• Polish Air Force University in Deblin, Faculty of Aeronautics Dywizjonu 303/35 Street, 08-521 Deblin, Poland tel.: [phone], fax: [phone]

autor

Żyluk A.

• Polish Air Force Academy in Deblin, Faculty of Aeronautics Dywizjonu 303/35 Street, 08-521 Deblin, Poland tel.: [phone], fax: [phone]

autor

Grzesik N.

• Polish Air Force University in Deblin, Faculty of Aeronautics Dywizjonu 303/35 Street, 08-521 Deblin, Poland tel.: [phone], fax: [phone]

autor

Kuźma K.

• Polish Air Force University in Deblin, Faculty of Aeronautics Dywizjonu 303/35 Street, 08-521 Deblin, Poland tel.: [phone], fax: [phone]

Bibliografia

• [1] Diamond Aircraft. The Airplane flight manual, Austria 2016.
• [2] Diamond Aircraft. Supplement S02 to The Airplane flight manual DA42 NG Ice protection System, Austria 2016. 531
• [3] Domicz, J, Szutowski, L., Podręcznik pilota samolotowego, wydawnictwo Avia-Test, Poznan 2008.
• [4] Jeppesen., Meteorology JAA ATPL Training, Atlantic Flight Training Ltd, Germany 2004.
• [5] Scorer R., Clouds of the World, wydawnictwo Lothian, Melbourne 1972.
• [6] Szewczak, P., Meteorologia dla pilota samolotowego, Wydawnictwo Avia-Test, Poznan 2007. [7] Grzesik, N., Podstawy sterowania rozmytego, WSOSP, Deblin 2012.
• [8] http://www.mathworks.com/products/simulink/ (available on 2 May 2018).
• [9] https://www.caviceprotection.com/content/about-tks-ice-protection-systems (available on 2 May 2018).

Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).