Oct 20, 2020   1:46 a.m. Vendelín
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Ing. Juraj Slačka, PhD.
Identification number: 50837
University e-mail: juraj.slacka [at] stuba.sk
Odborný asistent CSc.,PhD. - Institute of Robotics and Cybernetics (FEEIT)

Final thesis     
Supervised theses

Basic information

Basic information about a final thesis

Type of thesis: Diploma thesis
Thesis title:
Flying model of bicopter
Written by (author): Ing. Lukáš Hrečko
Department: Institute of Robotics and Cybernetics (FEEIT)
Thesis supervisor: Ing. Juraj Slačka, PhD.
doc. Ing. Rudolf Andoga, PhD.
Final thesis progress:
Final thesis was successfully defended.

Additional information

Additional information about the final thesis follows. Click on the language link to display the information in the desired language.

Language of final thesis:Slovak

Slovak        English

Title of the thesis:
Flying model of bicopter
Summary:Due to the complexity of flying vehicles, which includes both construction and mathematical model, dealing with their control problems is usually not a trivial task. Typical control problems one needs to consider are related not only to control the vehicle's flight itself but also to control the process of its take off, landing, and stabilization during the flight. These problems significantly depend on the flying vehicle under consideration, and the corresponding control actions need to be chosen also with respect to the size and type of the vehicle. In this paper the respective vehicle we consider is the so-called bicopter, which can be described as a two-rotor flying machine without variable tilting propellers attached to it. Note that the rotors and the body of the bicopter are not firmly connected, and the whole construction is more pendulum-like. That is, the rotors can rotate around the common axis perpendicular to the body of the bicopter. This makes bicopter one of the least stable aircraft construction.
Key words:
bicopter, AHRS, filters, drone, IMU, MCU, process control, Kalman, tilt rotor

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