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Wyszukujesz frazę "Adamski, A." wg kryterium: Autor


Wyświetlanie 1-4 z 4
Tytuł:
Study of the pilot’s attention in the cabin during the flight
Autorzy:
Adamski, M.
Adamski, A.
Powiązania:
https://bibliotekanauki.pl/articles/243850.pdf
Data publikacji:
2018
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
transport
battlefield environment
pilot reaction delay
device parameters
parameters reading time
Opis:
The pilot, while performing certain tasks or being in the battlefield environment works in a time lag. He is forced to properly interpret the information and quickly and correctly take action. Therefore, the instruments in the cabin should be arranged in such a way that they are legible and the operator have always-easy access to them. Due to the dynamics of the aircraft and the time needed to process the information by the pilot, a reaction delay occurs, resulting in the plane flying in an uncontrolled manner even up to several hundred meters. This article discusses the VFR and IFR flight characteristics, the pilot’s attention during flight, cabin ergonomics, and the placement of on-board instruments having a significant impact on the safety of the task performed in the air. In addition, tests have been carried out to determine exactly what the pilot’s eye is aimed at while completing the aerial task. Six basic devices were identified: altimeter, artificial horizon, speedometer, turn indicator with transverse gauge, variometer and heading indicator. They also started to think about how to position them in relation to each other in order to achieve the best results in terms of ergonomics, which include, minimizing time of reading individual parameters, grouping devices with parameters closely related to each other, reducing to a minimum the value of errors during reading and the smallest possible pilot’s effort.
Źródło:
Journal of KONES; 2018, 25, 3; 17-24
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Application of drones in protection of state border
Autorzy:
Adamski, M.
Mieżaniec, J.
Adamski, A.
Powiązania:
https://bibliotekanauki.pl/articles/242649.pdf
Data publikacji:
2018
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
Unmanned Aerial Vehicles
flying platform
drone
unmanned
UAV
Unmanned Aerial Vehicle
fly eye
Border Guard
operator
Opis:
An unmanned aerial vehicle is a flying apparatus that does not require a crewmember on board to complete a task. Its piloting is done by means of indirect control. UAVs also have the ability to perform autonomous flight on a pre-programmed flight path. The purpose of the study was to use the unmanned aircraft "Fly Eye" by WB Electronic used by the Border Guard to patrol the state border in 103 TRA zone on the section of the Republic of Poland with the Kaliningrad District of the Russian Federation. The TRA zones constitute a specially designated area for the use of the Border Guard and the army, in order to carry out flights there beyond the scope of the pattern for training purposes and to patrol the state border. The article also contains information of the Border Guard formation and the characteristics of the unmanned aerial vehicle “FlyEye”. In order to ensure the safety of the UAV flight, the test was carried out in the TRA zone, which is used for special use for the Border Guard formation and the army.
Źródło:
Journal of KONES; 2018, 25, 4; 9-15
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Algorithm for determining the angular position of the pilot’s helmet to control the on-board weapon’s control system
Autorzy:
Adamski, M.
Szelmanowski, A.
Powiązania:
https://bibliotekanauki.pl/articles/242876.pdf
Data publikacji:
2015
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
helmet-mounted cueing systems
modelling
research methods
Opis:
The following paper presents a method of determining the angular position of the pilot’s helmet based on the measurement of magnetic field components, artificially generated on board the aircraft (similarly to the helmet-mounted cueing systems of the F-16 aircraft). We presented a mathematical model, which describes determining of the angular position of the pilot's helmet, based on the measurement of the magnetic field components in various moments of powering orthogonally fixed magnetic coils. We also defined modelling capabilities of the helmet-mounted cueing system, which uses the magnetic method to determine the angular position of the pilot's helmet. It has been shown that the direction cosine matrix can be used for determining the angular position of the pilot's helmet, specified based on the matrix formed from the magnetic field components in various moments of powering orthogonal magnetic coils. The paper ends with an outline of simulation tests, which enable to identify the errors of the system, using such a method.
Źródło:
Journal of KONES; 2015, 22, 2; 7-16
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
The magnetic field curvature correction algorithm dedicated for helmet mounted cueing systems
Autorzy:
Adamski, M.
Szelmanowski, A.
Powiązania:
https://bibliotekanauki.pl/articles/949523.pdf
Data publikacji:
2018
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
transport
avionics
helmet-mounted cueing systems
errors of the angular positioning
magnetic field measurement
flat coil profile modelling
Opis:
The article presents the new built in Poland helmet mounted cueing system NSC-1 Orion with a magnetic method, dedicated to the multi-purpose helicopters W-3PL Gluszec. This system uses the magnetic field generated by the system of three mutually orthogonal electric coils. The principle of operation of this system is described and the method of determining the angular position of the pilot's helmet relative to the helicopter's cabin using the reference magnetic field and the directional cosines matrix are discussed. Electrical flat coils, constructed in the Polish Air Force Institute of Technology (AFIT), generating a magnetic field with curved symmetry axis characteristics, causing errors in determining the angular position of the pilot's helmet are shown. As a way to minimize these errors, an original proprietary algorithm for correcting the negative impact of the magnetic field curvature generated by the on-board system has been presented. Mathematical relations describing the presented correction process as well as selected results of simulation and experimental investigations in the area of inaccuracy of the "before" and "after" systems of applying the developed algorithm were given. Inaccuracies determined from computer simulations of the developed mathematical relations were compared with experimental data from magnetic field measurements using the integrated three-axis sensor ADIS-16405, used in the laboratory of the AFIT Avionics Division for helmet control of the angular position of the moving observation and sighting head and reflector-search light.
Źródło:
Journal of KONES; 2018, 25, 2; 15-30
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
    Wyświetlanie 1-4 z 4

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