Wszystkie pola: helmet - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Methods of flight parameters indications matching in helmet-mounted display systems
Autorzy:: Michalak, S.
Borowski, J.
Szelmanowski, A.
Powiązania:: https://bibliotekanauki.pl/articles/243670.pdf
Data publikacji:: 2017
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: transport
aviation
aircraft helmet-mounted display systems
joint helmet-mounted cueing systems
lotnictwo
Opis:: The article presents selected results of the analytical work carried out in the Air Force Institute of Technology regarding the possibility of computer matching systems, digital display and analogue devices, both in the static states and in dynamic states while manoeuvring the aircraft. On the example of parameter of vertical speeds provided a method of matching the indications for the helicopter Mi-17-1V with built helmet-mounted display system of flight data SWPL-1 Cyclops (developed by the Air Force Institute of Technology and cooperating with analogue avionics). Adjusting the display of vertical speed achieved by an inertial element of first row, implemented programmatically in the computer graphics KG-1. On the other hand, method of adjusting of indications on the information presented in the helmet-mounted cueing system NSC-1 Orion (built in the Air Force Institute of Technology for helicopter W-3PL Capercaillie) and obtained from the integrated avionics system (with digital avionics), exemplified by magnetic heading (obtained from heading layout KCS-305) and geographic heading (obtained from inertial navigation system EGI-3000). Adjusting of indications realized by introducing amendments to the indications of the multifunctional monitor MW-1, translucent display HUD and helmet-mounted display WDN-1 (in the form of elected declination, implemented programmatically on the computer mission KM-1) and the amendments to the magnetic deviation (introduced periodically to heading compensator layout KCS-305).
Źródło:: Journal of KONES; 2017, 24, 1; 255-263
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 2.

Tytuł:: Possibility of upgrading fighter aircraft MiG-29 in the field of helmet-mounted display systems
Autorzy:: Pazur, A.
Borowski, J.
Kowalczyk, H.
Szelmanowski, A.
Powiązania:: https://bibliotekanauki.pl/articles/244909.pdf
Data publikacji:: 2017
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: transport
aviation
aircraft glass cockpit systems
helmet mounted display systems
lotnictwo
Opis:: The article presents selected results of the analytical work carried out in the Air Force Institute of Technology in the field of information visualization capabilities of helmet-mounted guidance and navigation in fighter aircraft MiG- 29. There is presented the SzCz-3UM headset system of target’s indication, currently used on-board of MiG-29, which is directly cooperating with the pilot during the combat flight. There was presented that the information from the onboard systems of this aircraft containing analogue devices must be computer-processed into digital form in order to present flight data in the helmet-mounted display system. However, MiG-29 aircraft, used in the Polish Air Force, are equipped with modern digital avionics (integrated avionics system) based on the MIL-1553B digital data buses, which gives the possibility of the new helmet-mounted imaging of flight parameters via the computer data processing from aircraft’s devices and on-board installations. To develop guidelines for the construction of the helmet-mounted system for the MiG-29, the SWPL-1 Cyklop flight data-displaying system was adopted (system developed in the Air Force Institute of Technology as avionics system modernization for Mi-17 military helicopters). There are discussed the main problems of scientific and specialist research positions used in the Air Force Institute of Technology to assess the accuracy of the selected equipment components of avionics systems and determine credibility of information provided to the pilot during the flight.
Źródło:: Journal of KONES; 2017, 24, 1; 291-298
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 3.

Tytuł:: Ato choose variants of hardware architecture for the SWPL-1 helmet-mounted display system
Autorzy:: Michalak, S.
Kowalczyk, H.
Szelmanowski, A.
Borowski, J.
Powiązania:: https://bibliotekanauki.pl/articles/241745.pdf
Data publikacji:: 2018
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: transport
avionics
helmet-mounted display systems
hardware architecture
multi-criteria optimization
Opis:: 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.
Źródło:: Journal of KONES; 2018, 25, 4; 285-292
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 4.

Tytuł:: Modelling of physical phenomena in the vertical velocity measuring circuit for process of designing the SWPL-1 helmet-mounted display system
Autorzy:: Michalak, S.
Żyluk, A.
Szelmanowski, A.
Borowski, J.
Powiązania:: https://bibliotekanauki.pl/articles/243481.pdf
Data publikacji:: 2018
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: transport
avionics
helmet-mounted display systems
error
vertical velocity measurement
Opis:: The article presents the selected methods of identifying static and dynamic properties of the measuring paths to the extent necessary for the proper integration of on-board systems with the helmet-mounted flight parameter display system. It presents the methods of identifying static and dynamic properties of the WR-10MK on board variometer as one of more difficult identification elements. Its identification was carried out on the basis of the basic dependencies of the International Standard Atmosphere and the instruments construction’s parameters. It built a mathematical model describing the physical phenomena associated with vertical speed measurement. This model differs from the models found in the literature in terms of detail and description accuracy. On this basis, in the Simulink environment, it built a simulation model corresponding to its mathematical model. The non-linear model was the starting point for the construction of the linearized model based on the operator transmittance. The developed models were evaluated for errors of vertical speed’s dynamic indications. This allowed assessing the usefulness of the individual models for further works on ensuring the correlation of indications of the on-board variometer and the SWPL-1 helmet-mounted flight parameter display system. The presented simulation models include design details, as well as the characteristics of technological errors and disturbances of a stochastic nature. Another approach to the issue of identification is to use the characteristics provided by the manufacturer in the form of approximate characteristics of a module.
Źródło:: Journal of KONES; 2018, 25, 4; 277-284
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 5.

Tytuł:: Implementacja wymagań standardu DO-178C w procesie tworzenia oprogramowania awionicznego dedykowanego dla nahełmowego systemu zobrazowania SWPL-1 CYKLOP
Implementation of DO-178C standard requirements in the development process of avionic software dedicated to the SWPL-1 CYKLOP helmet-mounted flight parameter imaging system
Autorzy:: Pazur, A.
Szelmanowski, A.
Borowski, J.
Michałowski, P.
Powiązania:: https://bibliotekanauki.pl/articles/313301.pdf
Data publikacji:: 2017
Wydawca:: Instytut Naukowo-Wydawniczy "SPATIUM"
Tematy:: nahełmowy system zobrazowania
SWPL-1 CYKLOP
awionika
standard DO-178C
helmet-mounted imaging system
avionics
DO-178C standard
Opis:: W artykule przedstawiono wybrane wyniki prac analitycznych i konstrukcyjnych realizowanych w Instytucie Technicznym Wojsk Lotniczych (ITWL) w zakresie możliwości implementacji wymagań standardu DO-178C w procesie tworzenia oprogramowania awionicznego dedykowanego dla nahełmowego systemu zobrazowania SWPL-1 CYKLOP, zbudowanego w ITWL. Na przykładzie oprogramowania tworzonego dla komputera graficznego KG-1, zarządzającego trybami pracy systemu SWPL-1, oraz układu dopasowania sygnałów UDS-1, zilustrowano spełnienie wybranych wymagań standardu DO-178C.
The paper presents the selected results of analytical and construction works implemented in Air Force Institute of Technology in terms of possibilities of implementation of DO-178C standard requirements in the process of developing the avionic software dedicated to the SWPL-1 CYKLOP helmet-mounted imaging system, constructed in Air Force Institute of Technology (AFIT). In the general part of the paper, DO-178C requirements on the adopted safety level of software developed for the SWPL-1 system, were presented. In the detailed part, the methods for implementation of DO-178C requirements, applied in the development process of software for the SWPL-1 system, were discussed. On the basis of the software developed for KG-1 graphic computer, which manages operating modes of the SWPL-1 system and UDS-1 conditioning system of signals, the fullfilment of DO-178C standard requirements was illustrated.
Źródło:: Autobusy : technika, eksploatacja, systemy transportowe; 2017, 18, 12; 351-358, CD
1509-5878
2450-7725
Pojawia się w:: Autobusy : technika, eksploatacja, systemy transportowe
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 6.

Tytuł:: Możliwości nahełmowego zobrazowania informacji pilotażowo-nawigacyjnej w samolotach myśliwskich mig-29 z wykorzystaniem komputerowego przetwarzania danych
Possibilities concerning the helmet-mounted imaging of the flight and navigation information in the mig-29 aircraft with the use of computer data processing
Autorzy:: Pazur, A.
Michalak, S.
Borowski, J.
Szelmanowski, A.
Powiązania:: https://bibliotekanauki.pl/articles/250435.pdf
Data publikacji:: 2015
Wydawca:: Instytut Naukowo-Wydawniczy TTS
Opis:: W artykule przedstawiono wyniki prac analitycznych realizowanych w Instytucie Technicznym Wojsk Lotniczych w zakresie możliwości nahełmowego zobrazowania informacji pilotażowo-nawigacyjnej i celowniczej w samolotach myśliwskich MiG-29. Wykazano, że informacja z systemów pokładowych tego samolotu, zawierających urządzenia analogowe, musi być komputerowo przetwarzana do postaci cyfrowej, aby mogła być prezentowana w systemie nahełmowego wyświetlania parametrów lotu. Do opracowania założeń do budowy systemu nahełmowego dla samolotu MiG-29 przyjęto system wyświetlania parametrów lotu SWPL-1 Cyklop. Omówiono główne problemy naukowe i specjalistyczne stanowiska badawcze, wykorzystywane w Instytucie Technicznym Wojsk Lotniczych do oceny dokładności wskazań wybranych urządzeń składowych systemów awionicznych oraz określania wiarygodności informacji przekazywanej pilotowi podczas lotu.
The paper presents results of the analytical work carried out at the Air Force Institute of Technology (AFIT) in the field of possibilities concerning the helmet-mounted imaging of the flight, navigation and targeting information in the MiG-29 aircraft. It has been shown that the information from this aircraft’s on-board systems which contain analog devices, has to be processed by a computer into digital form in order to be presented in the helmet-mounted display system. To develop the guidelines for the construction of the helmet-mounted display system for the MiG-29 aircraft, the SWPL-1 flight data display system (Cyclops) has been adopted. The main scientific problems and specialist test benches used in the AFIT to assess the accuracy of selected devices of avionics systems and determine the reliability of information provided to the pilot during the flight are discussed.
Źródło:: TTS Technika Transportu Szynowego; 2015, 12; 2810-2815
1232-3829
2543-5728
Pojawia się w:: TTS Technika Transportu Szynowego
Dostawca treści:: Biblioteka Nauki

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