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AeroWorks: Graphic User Iterface for Autopilot
Duryagina, Viktoriya ; Dittrich, Petr (referee) ; Chudý, Peter (advisor)
The objective of the bachelor thesis is to design a graphical user interface for autopilot control system. The first chapter is dedicated to automatic flight control system theory overview. The next part discusses the user interface requirements and human-computer interaction problems. Subsequently, the design process and the development of new user interface are described. The final solution is implemented in the SimStar simulator.
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Stability and autopilot system for airplane RC model
Čamaj, Peter ; Republic), (SAAB Technologies Czech (referee) ; Šebesta, Jiří (advisor)
The master thesis deals with design and realization of stabilizing and autopilot system, which is used in radio controlled model planes. The thesis contains a proposal of hardware platform, which is able to control the plane model based on data measured from a sensor system. Moreover, this thesis describes a software implementation of individual modules, which is measured the onboard values. The basic principles of stabilization and autonomous flight control are also summarized. In conclusion, the system is subjected to flight tests.
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Evaluation of advantages and disadvantages of aircraft automatic systems
Vrána, Michal ; Koštial, Rostislav (referee) ; Horpatzká, Michaela (advisor)
This bachelor’s thesis deals with civil airplane automatic systems. The first part analyses historical development of flight control systems and automatic system together with philosophy, which is implemented in modern airliners. In the next part, we evaluate advantages and disadvantages together with list and description of modern avionic systems, which participate on automatic flight. In the last part, selected airplane incidents and accidents are analysed, focusing on influence of automation with incidental human factor.
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Small UAV parachute recovery system design
Pejchar, Jan ; Jebáček, Ivo (referee) ; Popela, Robert (advisor)
The thesis is focused on the small UAV’s rescue system design. The thesis is divided into related sections reflecting the design process. The first part deals with general problems of parachute equipment. Another part is evaluating critical situations in manual and autonomous control of the airplane. The deceleration device is based on this critical situations as well as the calculated structure loading. Next is the description and evaluation of experiments to verify the performance of modern parachutes. The thesis also includes a simplified proposal ejection mechanism designed in 3D software and documentation of the of model aircraft construction for testing and predicting behaviour in autonomous flight mode.
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Control and Position Stabilization of a Small Flying Drone
Martinec, Adrián ; Zamba, Martin (referee) ; Strnadel, Josef (advisor)
The goal of this thesis is to create a drone in a form of a plane, driven by autopilot. I have solved the selected issues using a theory of flight and regulators from an automatization area. The text describes a functional solution. Unfortunately because of an accident, no final tests were performed. A contribution of this work is in exploring a functionality of various parts that are used with a drone building process. That includes a use of regulators and creation of libraries driving those parts.
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Automatic Flight Control System Design for a Jet Aircraft
Krasňanský, Milan ; Vlk, Jan (referee) ; Chudý, Peter (advisor)
Tato bakalářská práce se zabýva modelováním letových vlastností proudového letadla a následným návrhem a implementací systému pro automatické řízení letu. Jejím cílem bylo na základě veřejně dostupných aerodynamických dat letounu F-16, který má sníženou podélnou stabilitu, implementovat model tohoto letounu a použít tento model jako platformu pro návrh a implementaci systému pro automatické řízení letu založeného na nelineární dynamické inverzi se soustředením se na řízení podélného pohybu letounu, pomocí nastavení požadovaného úhlu náběhu. Testy vytvořeného systému prokázali schopnost dosáhnout a udržet požadovaný úhel náběhu.
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Expansion of Skydog Aircraft Model Control System by Remote and Autonomous Control by Android Application
Boček, Michal ; Šimek, Václav (referee) ; Strnadel, Josef (advisor)
The thesis aims to design and implement an Android application with ability to control the autopilot of the Skydog aircraft model using the wireless telemetry. The application shall receive data from an aircraft model gathered from various installed sensors. These data shall be then processed and corresponding instructions for autopilot shall be sent back. When collision with terrain or obstacle is detected, the application shall send instructions to autopilot to avoid such collision. RRT algorithm is used to find collision-free flight trajectory. Database of known obstacles and digital terrain model are provided to application in formats XML and GeoTIFF respectively.
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AeroWorks: Mode Selection Panel for Autopilot
Cibula, Peter ; Dittrich, Petr (referee) ; Chudý, Peter (advisor)
This thesis deals with the implementation of the aplication for the autopilot mode selection panel. It describes automatic flight control systems from their origins to the present. It deals with the spacial model of aircraft motion. It also describes the hardware characteristics of the panel, the application in terms of implementation and functionality, testing on flight simulator SimStar and future plans.
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Methods for parameters setting of controller by plane with flight control with floating level centre in MATLAB-Simulink
Náglová, Katarína ; Burlak, Vladimír (referee) ; Pivoňka, Petr (advisor)
The thesis is focused on aircraft flight level control in case when the location of center of gravity changes during flight. The theoretical part of the thesis describes basics of aerodynamics, which are necessary to understand airplane's behavior and its control theory. Basics of state theory and stability of systems, as it is used for design of linear model. This part also mentions mathematical equations of nonlinear model of business jet and discusses conventional and adaptive methods used to design autopilot parameters. Several autopilots were designed in practical part of the thesis. The most important part is the logic used to determine location of center of gravity of the airplane. The models use nonlinear model of an airplane that better represents the real environment and conditions.
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