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Graphical Interface for Flight Displays
Tabášek, Michal ; Vlk, Jan (referee) ; Chudý, Peter (advisor)
Tato bakalářská práce se zabývá vizualizací letových dat. Obsahuje popis matematicko fyzikálního modelu letadla, přístrojů používaných při zobrazování letových veličin a proces vývoje primálního letového displeje pro letecký simulátor. Displej je implementován s využitím jazyka C++ a grafické knihovny OpenGLTato bakalářská práce se zabývá vizualizací letových dat. Obsahuje popis matematicko fyzikálního modelu letadla, přístrojů používaných při zobrazování letových veličin a proces vývoje primálního letového displeje pro letecký simulátor. Displej je implementován s využitím jazyka C++ a grafické knihovny OpenGL.
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Aircraft's Engine Data Recorder
Vrána, Michal ; Šebesta, Ondřej (referee) ; Červenka, Miroslav (advisor)
This thesis deals with aircraft engine monitoring system. In the first part a study of current solutions, available on the market is made. Next is the description of test airplane, where the prototype of the instrument will be tested. Description of prototype instrument, it’s data handling and graphical solution are all analysed in the next chapter, with pros and cons of possible solutions. Last chapter deals with further instrument development and possible data postprocessing.
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Radar Altimeter for Ultramicro Airplanes
Imrich, Marek ; Maršík, Lukáš (referee) ; Zemčík, Pavel (advisor)
Radar equipment is an integral part of the aviation sector. It is very important to use a suitable module to guide ultralight aircraft during landing. The bachelor thesis is focused on the use of altitude radar based on the microwave sensor IWR6843ISK manufactured by TEXAS Instruments and its application in practice for ultralight aircraft. Its ability in conjunction with a computer is the altitude guidance of an ultralight aircraft to the runway by generating sound tones to indicate to the pilot the distance above the terrain. The main goal of this work is to design a model for the use of a microwave module in conjunction with a computer and its subsequent testing of the suitability for use in performing a landing maneuver. The aim of this work is to design a system that works with millimeter radar and its evaluation of usability in practice. The proposed module generates point clouds, which are then parsed, then the output data are suitably correlated, further transformed to the exact height of the aircraft above the terrain with subsequent sound interpretation to the pilot.
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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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Futuristic Aircraft Cockpit Design
Hlipala, Martin ; Vlk, Jan (referee) ; Chudý, Peter (advisor)
This thesis is analysing the historical evolution of flight instruments and aims at the design of a new, enhanced cockpit that includes basic flight instruments supplemented by data from selected aircraft subsystems. The design is based on currently available electronic instruments, known as EFIS, presently used onboard Boeing 737-800 cockpit. The proposed design aims at improvements to graphic style of EFIS, and accomodation of new data into newly designed displays. As a result of this effort, a set of design concepts is created. Those are then implemented as fully functional set of displays using custom made user interface system design tool.
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Radar Altimeter for Ultralight Aircraft
Zahradník, Jiří ; Zemčík, Pavel (referee) ; Maršík, Lukáš (advisor)
In this bachelor thesis author designs a radar altimeter. In this thesis the emphasis is placed onto modular architecture and that is why this altimeter is designed as a group of independent modules communicating through BSD sockets. Software implementation is made in C++ and for sound generator is used library PulseAudio. Next topic is multithreading safety implementation of queue and stack which was made by template class to keep simplicity and generality.
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Graphical Interface for Flight Displays
Tabášek, Michal ; Vlk, Jan (referee) ; Chudý, Peter (advisor)
Tato bakalářská práce se zabývá vizualizací letových dat. Obsahuje popis matematicko fyzikálního modelu letadla, přístrojů používaných při zobrazování letových veličin a proces vývoje primálního letového displeje pro letecký simulátor. Displej je implementován s využitím jazyka C++ a grafické knihovny OpenGLTato bakalářská práce se zabývá vizualizací letových dat. Obsahuje popis matematicko fyzikálního modelu letadla, přístrojů používaných při zobrazování letových veličin a proces vývoje primálního letového displeje pro letecký simulátor. Displej je implementován s využitím jazyka C++ a grafické knihovny OpenGL.
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Graphical Interface for Flight Displays
Brumovský, Vít ; Dittrich, Petr (referee) ; Chudý, Peter (advisor)
This work aims to familiarize the reader with the evolution of avionics, techniques and possibility to display the flight quantity and describe the making of primary flight displays for flight simulator. The text also contains implementation details and testing methods. The display is created using C ++ and OpenGL graphics library. Created solution provides two display modes - classic and monochromatic. The final display is possible to configure for a specific type of aircraft.
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Control unit for turbofan jet engine TFE731
Slavotínek, Jan ; Mikuláštík, Jiří (referee) ; Macho, Tomáš (advisor)
This thesis is classified as an internal experimental project whose aim is to design HW and low level SW of simplified version of the controller for TFE731 turbofan engine according to defined requirements. The expected outputs in addition to the system design is also information about possible technical problems and difficulties arising during the analysis and development of the system. The work covers a brief look into the history of aviation and avionics, theoretical analysis turbofan engine, analysis of measured and controlled variables. Based on the requirements analysis and I/O values is made circuit design (HW) and design of the low level control software.
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