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:: 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: 3.

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: 4.

Tytuł:: Helmet-mounted display and cueing systems as pilot aids for aviation/maritime search and rescue missions
Autorzy:: Lewitowicz, J.
Szelmanowski, A.
Pazur, A.
Michalak, S.
Janik, P.
Powiązania:: https://bibliotekanauki.pl/articles/135533.pdf
Data publikacji:: 2017
Wydawca:: Akademia Morska w Szczecinie. Wydawnictwo AMSz
Tematy:: integrated avionics systems
helmet-mounted display systems
SAR/CSAR systems
SWPL1 “Cyklop” system
NSC1 “Orion” system
TOPLITE system
RSC-125G system
Opis:: The paper presents selected results of analytical and construction works executed at the Air Force Institute of Technology (AFIT) in the context of possibilities of supporting the actions of a helicopter crew, i.e., pilot-crew commander, pilot-operator of on-board systems, and on-board technician participating in aviation/maritime search and rescue missions. Such support is based on using the helmet-mounted display systems SWPL1 “Cyklop” and NSC1 “Orion” for information from the observation-targeting heads and verbal communication with the survivor. Selected imaging and verbal communication devices installed on aircraft operated by the Polish Armed Forces, which are used in aviation/maritime search and rescue actions, are discussed. Particular attention is drawn to the problems associated with the integrated avionics systems of helmet-mounted imaging of piloting-navigation parameters and the helmet-mounted imaging of information from the observation-targeting heads, i.e., the on-board radio direction finder system and emergency radio, which are part of the integrated communication system. Sample structural solutions for such systems and the possibilities of their application in search and rescue missions are presented.
Źródło:: Zeszyty Naukowe Akademii Morskiej w Szczecinie; 2017, 52 (124); 112-119
1733-8670
2392-0378
Pojawia się w:: Zeszyty Naukowe Akademii Morskiej w Szczecinie
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 5.

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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