Jan 28, 2020   1:59 p.m. Alfonz
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Ing. Martin Garan, PhD.
Identification number: 10008
University e-mail: martin.garan [at] stuba.sk
Odborný asistent CSc.,PhD. - Institute of applied mechanics and mechatronics (FME)

Contacts     Graduate     Lesson     Final thesis     Supervised theses     Conferences     

Basic information

Basic information about a final thesis

Type of thesis: Bachelor thesis
Thesis title:Modeling and simulation of basic physical models of dynamic systems
Written by (author): Ing. Bence Nagy
Department: Institute of applied mechanics and mechatronics (FME)
Thesis supervisor: Ing. Martin Garan, PhD.
Opponent:Ing. Miroslav Šulko, 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:English

Slovak        English

Title of the thesis:Modeling and simulation of basic physical models of dynamic systems
Summary:The aim of this thesis was to discuss the problematics of creat- ing simple physical and dynamical models and show the process of simulating these models using various software and to develop the dynamical model of a suborbital rocket _ying in the Earth's atmosphere. The basics of model- ing of simple physical systems were described in the _rst chapter and were illustrated on a spring-mass-damper system. In the second chapter, we de- scribed the fundamentals of the simulation of dynamic systems. Here, the spring-mass-damper system was used as a reference, and it was shown that how can we build and simulate a dynamic system in Matlab/Simulink. The third chapter deals with _ight mechanics and shows the derivation of the equations of motion of an aircraft _ying in the Earth's atmosphere. First, the equations were derived for a general aircraft and later were applied to a suborbital rocket. The last chapter discussed the problematics of suborbital rockets and the mathematical model of a suborbital rocket was built. It was also shown that how we can simulate the _ight of a suborbital rocket using Simulink. The last topic of the thesis was the creation of an animation that visualizes the simulation and makes the whole thesis complete.
Key words:sounding rocket, physical model, mathematical model, simulation

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Parts of thesis with postponed release:

Final thesis (final thesis appendices) unlimited
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