Modelling Of Aircraft Autopilot Using F-16.
Students Name: Yermolaiev Danylo Kyrylovych
Qualification Level: magister
Speciality: Aviation Information Systems and Complexes
Institute: Institute of Telecommunications, Radioelectronics and Electronic Engineering
Mode of Study: full
Academic Year: 2023-2024 н.р.
Language of Defence: ukrainian
Abstract: The work is dedicated to the development and analysis of autopilot modeling algorithms for an aircraft, using the parameters of the F-16 aircraft as an example. The study explores fundamental aspects of autopilots, including their structure, algorithms, and interaction with other aircraft systems. Specifically, attention is given to utilizing F-16 parameters to build and optimize mathematical models that enable the implementation of an effective autopilot. The research includes an analysis of aircraft dynamics and the determination of necessary control variables to achieve desired flight parameters using Matlab. The use of F-16 parameters allows for considering the characteristics of this specific type of aircraft, ensuring accuracy and stability of the autopilot under various flight conditions. The research results can be valuable for the development of improved autopilots for aircraft, particularly incorporating technological solutions that account for the unique characteristics of the F-16. The work contributes significantly to the understanding and optimization of autopilot systems, fostering further advancements in aviation technology. Study object: Autopilot. Scope of research: Autopilot model using F-16 parameters. Goal of research: Analyze the behavior of the aircraft autopilot with F-16 parameters. Keywords: aircraft, F-16, mathematical model, flight, F-16 parameters, analysis. During this work, a review of autopilot types, their development, and applications was conducted. A mathematical model of aircraft motion was developed, a Simulink model was constructed, and algorithms for simulation and linearization of the aircraft autopilot model with F-16 parameters were developed.References 1. В. Г. Воробьев, С. В. Кузнецов. Автоматическое управление полетом самолетов: Учеб. для вузов.-М.: Транспорт. 1995.-448 с. 2. Кузнецов С.В. Системы автоматического управления полетом. Самолет как объект управления [Текст] : учебное пособие / С.В. Кузнецов. – М. : ИД Академии Жуковского, 2018. – 52 с. 3. Остахов А. А., Первухин Д. А., Ляшенко А. Л., Ильюшин Ю.В., Кравцова А. Л. Системы автоматического управления летательными аппаратами. История и практика – Санкт-Петербург: издательство «СатисЪ», 2013 – 184с. 4. Синєглазов В.М. Філяшкін М.К. С382 Автоматизовані системи управління повітряних суден: Підручник – К.: НАУ, 2013. – 502 с. 5. Albert Farr ?e Gabernet, University Of California, Controllers for Systems with Bounded Actuators: Modeling and control of an F-16 aircraft 6. Eric H.K. Fung, Y.K. Wong, Hugh H.T. Liu and Y.C. Li, Multiple specification controller design for F-16 fighters, Aircraft Engineering and Aerospace Technolog. 7. General Dynamics F-16 Fighting Falcon. [ Електроний ресурс] – Режим доступу :URL: https://www.lockheedmartin.com/en-us/products/f16.html– Назва з екрана 8. How autopilot works[ Електроний ресурс] – Режим доступу :URL: https://science.howstuffworks.com/transport/flight/modern/autopilot5– Назва з екрана. 9. Richard S.Russel University of Minnesota. Non-Linear F-16 Simulation using Simulink and Matlab. 1/12/2014 10. Zeinab El-Sayegh, Aynour Deghidy, Auto Pilot Design for F-16 December 2014