Research and measuring capabilities of the system-integration laboratory equipment to optimize integrated avionics systems

• Autorzy: Michalak S. , Szelmanowski A. , Cieślik A.
• Języki publikacji: EN

Abstrakty

EN

The paper has been intended to present research tools used at ITWL to activate and test hardware and software implemented in the integrated avionics systems. Particular attention has been paid to the research stand (built under the R&D project of the Ministry of Science and Higher Education) intended to optimize avionics systems integrated with digital data buses employed (according to, among other things, MIL-1553B and ARINC-429 standards). Specialized research equipment/test devices used to test software, including - apart from other things - test-patterns generators (within the range of display capability of the secondary head-up display (SHUD)) and Information efficiency tester s (for the SHUD andup-front control panel (UFCP) thereof) have also been presented. The architecture of a Sextant Avionique's STRATUS-type navigation system, engineering accomplishment of the laboratory stand, the laboratory equipment to optimise integrated avionics systems on the digital data bus A4IL-STD-1553B, research capabilities of the laboratory stand and equipment to optimize the integrated avionics system, laboratory stand's panels used in the process of integration, additional research tools for the optimisation of the integrated avionics system, exemplary research tools used to optimise software of the integrated avionics system: the SHUD/UFCP tester), and the Multi-function Display (MFD) tester are presented in the paper.

Słowa kluczowe

EN

integrated avionics systems; research and measuring equipment; optimization of functionality

• 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: 2009
• Tom: Vol. 16, No. 2
• Strony: 323--328
• Opis fizyczny: Bibliogr. 6 poz., rys.

Twórcy

autor

Michalak S.

autor

Szelmanowski A.

autor

Cieślik A.

• Air Force Institute of Technology Księcia Bolesława Street 6, 01-494 Warszawa, Poland phone: [phone],fax: [phone],

Bibliografia

• [1] Szelmanowski, A., et al., Stanowisko integracyjne systemów awionicznych na bazie cyfrowych szyn danych, Sprawozdanie z pracy, BT ITWL, Warszawa 2004.
• [2] The Sextant Avionique advertising materials, Navigation Systems – Laser Gyro Attitude and Navigation Hybrid Inertial Reference System STRATUS, Cedex, 1997.
• [3] Endsley, M., Flight crews and modern aircraft in search of Situation Awareness, Materiały konferencyjne Royal Aeronautical Society, London 2000.
• [4] Skrzyniarz, T., Dokumentacja opisowa stanowiska laboratoryjnego awioniki, Warszawa, BT ITWL 2008.
• [5] Frask, P., Instrukcja użytkowania stanowiska laboratoryjnego awioniki, Warszawa, BT ITWL 2008.
• [6] Szelmanowski, A., et al., Możliwości testowania poprawności przetwarzania informacji w systemach awionicznych zintegrowanych na bazie szyny MIL-1553B, Journal of Aeronautica Integra, ISSN 1896-8856, No. 1/2008 (3), pp. 73-78, Oficyna Wydawnicza Politechniki Rzeszowskiej, Rzeszów 2008.