Autor: Borowski, J - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Study of the noncommutativity of submitting aircraft rotation in high-manoeuvring flights
Autorzy:: Szelmanowski, A.
Borowski, J.
Garbacz, M.
Powiązania:: https://bibliotekanauki.pl/articles/244401.pdf
Data publikacji:: 2017
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: transport
aviation
inertial navigation system
coning motion
noncommutativity rate vector
lotnictwo
Inercyjny system nawigacji
Opis:: The article presents selected results of the analytical work carried out in the Air Force Institute of Technology and the Polish Air Force Academy by means of a computer simulation of noncommutativity phenomena submitting aircraft turnover on high-manoeuvrability flights. The results of these simulations allowed to define the guidelines for the method of “production” of noncommutativity phenomenon in specialized rotating positions for strapdown inertial navigation systems (to evaluate the errors of determining spatial orientation). Also, it analysed the possibility of “production” noncommutativity rotational movement in mobile flight simulator used for testing pilots and candidates for pilots (to test the sensitivity of the pilot’s vestibular system in terms of feeling the impact of this phenomenon). The results of the assessment of “greatness” noncommutativity angular velocity vector, occurring in some parts of the high-manoeuvrability flight of aircraft on the example of a fighter-bomber airplane Su-22 were discussed as well.
Źródło:: Journal of KONES; 2017, 24, 1; 325-332
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

Artykuł

Zmień widok

na półce

Skocz do pozycji: 2.

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

Artykuł

Zmień widok

na półce

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

Artykuł

Zmień widok

na półce

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

Artykuł

Zmień widok

na półce

Skocz do pozycji: 5.

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

Artykuł

Zmień widok

na półce

Informacja

Wyszukujesz frazę "Borowski, J" wg kryterium: Autor

Źródło danych

Dostawca treści

Kolekcja

Rok wydania

Wydawca

Temat

Autor

Typ dokumentu

Język