Ato choose variants of hardware architecture for the SWPL-1 helmet-mounted display system

• Autorzy: Michalak S. , Kowalczyk H. , Szelmanowski A. , Borowski J.

Identyfikatory

DOI

10.5604/01.3001.0012.4802

• Języki publikacji: EN

Abstrakty

EN

The paper presents the structure and basic properties of the SWPL-1 helmet-mounted flight parameter display system, constructed for the Mi-17 helicopter with analogue systems and on-board instruments. It describes the basic components of the SWPL-1 system and on board components cooperating with the SWPL-1 system necessary to ensure the imaging system’s operation (including the ADU-3200 central unit for aerodynamic data and the GPS-155XL satellite signals receiver). It presents the architecture, the principle of operation, and the main constituents of the SWPL-1 helmet-mounted flight parameter system, as well as the standards of data transmission used in digital communication between the SWPL-1 system and on-board systems (installed on the Mi-17 helicopter). It describes the scope and manner of pilot and navigation data presentation as well as control of drive unit operation parameters in detail. It presents selected optimization methods for tasks executed in the helmet mounted system’s life cycle. The particular stages of the life cycle were described in detail, from the earliest stages of needs identification, through the analytic and conceptual phase, then the implementation stage, and ending with the operation stage. It introduces tasks for optimization and related methods into the process of creating the new system at every stage of its implementation. It presents one of the methods of multi-criteria optimization based on the experts’ assessment of choice of a variant of the helmet-mounted flight parameter display system’s hardware architecture in detail.

Słowa kluczowe

EN

transport; avionics; helmet-mounted display systems; hardware architecture; multi-criteria optimization

• 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: 285--292
• Opis fizyczny: Bibliogr. 6 poz., rys.

Twórcy

autor

Michalak S.

• Air Force Institute of Technology Ksiecia Boleslawa Street 6, 01-494 Warsaw, Poland tel.: [phone] [phone], [phone], fax: [phone]

autor

Kowalczyk H.

• Air Force Institute of Technology Ksiecia Boleslawa Street 6, 01-494 Warsaw, Poland tel.: [phone] [phone], [phone], fax: [phone]

autor

Szelmanowski A.

• Air Force Institute of Technology Ksiecia Boleslawa Street 6, 01-494 Warsaw, Poland tel.: [phone] [phone], [phone], fax: [phone]

autor

Borowski J.

• Air Force Institute of Technology Ksiecia Boleslawa Street 6, 01-494 Warsaw, Poland tel.: [phone] [phone], [phone], fax: [phone]

Bibliografia

• [1] Michalak, S., Selected problems of designing the helmet-mounted flight parameter display systems, Monograph, Publishing and Printing House of the Air Force Institute of Technology, Warsaw 2016.
• [2] Michalak, S., Borowski, J., Szelmanowski, A., Applicability of the helmet-mounted data presentation system in modernisation of military helicopter, Chapter in the collective work edited by Jan Gruszecki, Selected issues of Avionics, Publishing House of Rzeszow University of Technology, pp. 81-92, Rzeszow 2011.
• [3] Płonka, S., Multi-criterion optimisation of manufacturing processes of machinery parts,Scientific Technical Publisher, WNT, Warsaw 2010.
• [4] Saaty, T. L., The Analytic Hierarchy Process, McGraw-Hill, New York 1980.
• [5] Saaty, T. L., Decision Making with Dependence and Feedback, The Analytic NetworkProcess, RWS Publications, Pittsburg 2001.
• [6] Yager, R. R., Multiple Obiective Decision – Machining Using Fuzzy Sets, InternationalJournal on Man – Machines Studies, pp. 375-382, 1977.

Uwagi

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