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Stability Control of Quadrocopter
Nejedlý, Jakub ; Luža, Radim (referee) ; Rozman, Jaroslav (advisor)
This work deals with physical laws affecting behavior of a quadcopter as a mobile robot. It describes methods of controlling movements and stability. The result of the theoretical analysis is creation of simulation model. Moreover it depicts practical software developement of a real machine controller unit with its own conclusion, comparison between simulation and practical experiments and the workflow of the physical system construction.
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Multicopter Attitude Estimation Using Dynamic Model
Baránek, R.
The paper is focused on attitude estimation of multicopters. Specifically the use of dynamic model of multicopter in the attitude estimation algorithm is investigated. The examined algorithm is compared to the standard algorithm GPS-INS, which do not need any information of the vehicle dynamics. Both algorithms are tested in simulations. The use of dynamic model provides bounded errors of attitude estimates even without GPS measurements. The drawback is the need for a good dynamic model of the multicopter and its parameters.
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Multicopter - dynamical model
Musil, Filip ; Němeček, Jakub (referee) ; Kraus, David (advisor)
Bachelor's thesis Multicopter - dynamic model deals with basic principles of multicopter flight and determining the position in space. Next part of the thesis is dedicated to the search of possible methods of compilation of dynamic model and implementation in Matlab/Simulink environment. The aim of this work is compilation of simplified dynamic model of multicopter which aims approximate real behavior in space.
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Control system of exploration flying robot design and realization
Šnajder, Patrik ; Zuth, Daniel (referee) ; Marada, Tomáš (advisor)
This bachelor’s thesis describes wide range of multirotors systems and to become familiar with mlutirotors flying systems as well as the design and practical implementation of the control system. The control system should be in the air to determine the tilt and rotation of multicpter and thus ensure it‘s stabilization. Introduction to the electronic componentes necessary to fly multirotors. Practiacal measurement of actuators and for this purpose to create experimental apparatus.
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