Temat: Expert System - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Aircraft docking guidance system to the gate using fuzzy logic
Autorzy:: Żurawski, P.
Grzesik, N.
Kuźma, K.
Powiązania:: https://bibliotekanauki.pl/articles/243957.pdf
Data publikacji:: 2018
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: fuzzy logic
fuzzy expert system
aircraft taxiing
aircraft steering
Opis:: The article presents the concept of automated final process of aircraft taxiing to the gate at the terminal. On the basis of an analysis of the possibilities of aircraft taxiing in civil airports, the authors attempted at optimizing this process. The main objective of the project is to reduce the taxiing time, consequently reducing fuel consumption as well as the rotation time. As a result of the work, the authors designed a controller based on fuzzy logic, which, depending on the initial parameters, calculates the set values for the execution system of aircraft control in the horizontal plane and for the taxi speed. The controller receives two input signals, which determine two output signals. The designed controller allows comprehensive and fully automated aircraft steering. The project relies on data with regard to the apron class D, suited to handle aircraft with a wingspan of up to 52 m and the characteristics of a Boeing 767-200 in speed taxiing and the maximum turn of the nose gear. The measurements of the apron have been adopted in accordance with international regulations in the ICAO DOC 9157 “Aerodrome Design Manual”. The maximum deviation of the nose gear from the centre line was assumed 2.5 m in each direction and a safe distance behind the immobile aircraft equal to 25 m. The length of the Boeing aircraft 767-200 is below 48 m, therefore the input boundary parameters are equal to +/- 2.5 m from the centre line and 80 m from the designated aircraft stand (nose gear). The article presents the project of the controller and its optimization. The authors simulated the controller operation in the package MATLAB “Simulink”. The article ends with data analysis and final conclusions.
Źródło:: Journal of KONES; 2018, 25, 3; 549-556
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 2.

Tytuł:: The use of fuzzy expert system for an automatic control of the propulsion system in the aircraft ZLIN 143LSi
Autorzy:: Krok, B.
Grzesik, N.
Kuźma, K.
Powiązania:: https://bibliotekanauki.pl/articles/242523.pdf
Data publikacji:: 2018
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: fuzzy logic
fuzzy expert system
propulsion system
aircraft Zlin 143LSi
Opis:: The article discusses the manner of controlling the propulsion system in the aircraft Zlin 143LSi, which is equipped with a piston engine driving a variable-pitch propeller. All the operating procedures are carried out manually by the pilot in accordance with the flight manual. The authors attempted at developing the project of a controller based on fuzzy logic, whose main goal was automating the control system of the propulsion unit, thus lowering the level of difficulty of pilotage, and increasing the economics of the operation. The project was made in an interactive environment FuzzyLogic Toolbox of the MATLAB programme. In the analysis, three input parameters were taken into account, exerting an impact on changing the rotational speed of the propeller: the charging pressure of the propulsion unit expressed in inches of mercury, the speed of the aircraft (TAS) in knots and the angle of attack, at which the flight is made, expressed in degrees. On the basis of the above-mentioned input signals, the rotation speed of the propeller was determined, by changing the blade pitch and the recommended angle of attack for the parameters in order to make an optimal use of the data of the flight conditions. The article presents the project of the controller and its optimization. The authors simulated the controller operation in the package MATLAB “Simulink”. The article ends with data analysis and final conclusions.
Źródło:: Journal of KONES; 2018, 25, 3; 307-314
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 3.

Tytuł:: Using fuzzy logic expert system for the estimation of the probability of armour penetration by PGU-14 shells fired from the GAU-8/A CA
Autorzy:: Opala, P.
Grzesik, N.
Kuźma, K.
Powiązania:: https://bibliotekanauki.pl/articles/245144.pdf
Data publikacji:: 2017
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: fuzzy logic
fuzzy expert system
armour penetration
GAU-8/A cannon
PGU 14 API shells
Opis:: The article discusses the possibility of armour penetration by PGU 14 API shells fired from the GAU-8/A cannon. The considerations focus on questions with regard to the probability of armour penetration with the initially established conditions in the project. In the analysis, the authors took into account three parameters: armour thickness, armour slope and target distance. Based on the initial parameters, the authors estimated the probability of armour penetration. The designed a fuzzy expert system in the MATLAB software as well as conducting simulation of its performance in the Simulink programmes. The authors presented the performance of the system based on twenty samples for research, which simulate different thickness of the target armour, different distance from the target and different slope of the armour. The authors presented control surfaces, due to which it is possible to analyse the system performance. They also show the simulation process in the Simulink software package with the preset values. On the basis of the created controller, it is clear that a well-developed system, which had undergone testing and optimization, is capable of calculating near reality probability values. The designed system might improve fire effectiveness of ground targets during air training and combat tasks, as well as optimizing the consumption of air-to-ground armour piercing (AP) shells.
Źródło:: Journal of KONES; 2017, 24, 4; 211-218
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 4.

Tytuł:: Different defuzzification methods in Guimbal Cabri G2 helicopter takeoff possibility evaluation
Autorzy:: Mendrek, M.
Grzesik, N.
Krzyżak, A.
Kuźma, K.
Powiązania:: https://bibliotekanauki.pl/articles/374121.pdf
Data publikacji:: 2018
Wydawca:: Politechnika Śląska. Wydawnictwo Politechniki Śląskiej
Tematy:: fuzzy logic
fuzzy expert system
helicopter take off
logika rozmyta
regułowe systemy ekspertowe
start helikoptera
Opis:: The article discusses the aerodynamic properties of the Guimbal Cabri G2 helicopter. The main considerations concern the helicopters ascending to the altitude under initial conditions, which were assumed in the project and how the change of the defuzzification method affects the work of the fuzzy controller. The authors analyzed the following: the aircraft, the crew and the payload. The authors assessed the altitude and the minimum time of the helicopter climb. In designing and the work simulation process, the authors used Matlab and Simulink software. A comparison of the influence of selected defuzzification methods on the work of the fuzzy controller was made.
Źródło:: Transport Problems; 2018, 13, 2; 27-38
1896-0596
2300-861X
Pojawia się w:: Transport Problems
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 5.

Tytuł:: Ocena możliwości wzniesienia się w powietrze śmigłowca Guimbal Cabri G2 z wykorzystaniem rozmytego systemu eksperckiego
Guimbal Cabri G2 helicopter take off possibility evaluation with use of fuzzy expert system
Autorzy:: Mendrek, M.
Grzesik, N.
Krzyżak, A.
Powiązania:: https://bibliotekanauki.pl/articles/315655.pdf
Data publikacji:: 2016
Wydawca:: Instytut Naukowo-Wydawniczy "SPATIUM"
Tematy:: śmigłowiec Guimbal Cabri G2
rozmyty system ekspercki
MATLAB/Simulink
Guimbal Cabri G2 helicopter
fuzzy expert system
Matlab/Simulink
Opis:: W artykule omówione zostały możliwości aerodynamiczne śmigłowca Guimbal Cabri G2. Rozważania oscylują wokół pytania na jaką wysokość maszyna będzie w stanie się wznieść biorąc pod uwagę warunki początkowe założone w projekcie. Analizowano masę śmigłowca, masę członków załogi oraz masę bagażu zabieranego przez załogę. Oceniano wysokość i minimalny czas w jakim śmigłowiec będzie się wznosił. Zaprojektowany układ mógłby zostać wykorzystany w praktyce podczas lotów szkoleniowych, rekreacyjnych, wykonywania różnorakich zadań lotniczych oraz znacząco ułatwić proces przygotowania się do lotu załogi, w aspekcie możliwości szybkiej analizy obciążenia masowego śmigłowca. Zaprojektowano rozmyty system ekspercki w oprogramowaniu Matlab oraz przeprowadzono symulację jego działania w programie Simulink.
The article discusses the Guimbal Cabri G2 aerodynamic properties. The main question is what is helicopter rising altitude under initial conditions assumed in the project. The aircraft, crew and baggage weight analysis were the scope. The altitude and the minimum time in which the helicopter ascends were assessed. The designed project can be used in the wide spectrum of the air tasks. It will provide improvements during crew pre-flight preparations in terms of heli-copter weight capacity. Matlab and Simulink software was used in designing and work simulation process.
Źródło:: Autobusy : technika, eksploatacja, systemy transportowe; 2016, 17, 12; 1212-1216
1509-5878
2450-7725
Pojawia się w:: Autobusy : technika, eksploatacja, systemy transportowe
Dostawca treści:: Biblioteka Nauki

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