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	Stress, deformation and safety analysis of the generator stator loaded by nonhomogeneous temperature Majdič, Petr ; Dobeš, Martin (referee) ; Vrbka, Jan (advisor) This thesis deals with stress, strain and reliability analysis of synchronous generator stator including an inhomogeneous temperature field. Using the finite element method, stress and strain are calculated, and from these values safety against yield strength is determined, which is followed by the life calculation of the most stressed weld joint and the determination of its possible damage during the period required by the customer. Detailed record
	Quadrocopter - Sensory Subsytem Bradáč, František ; Šolc, František (referee) ; Žalud, Luděk (advisor) This diploma thesis deals with processing of measured data from inertial navigation system in order these could be used for stabilization. There is general information about aerial vehicles called copters with emphasis on four-rotor construction called quadrocopter at first. Then mathematical model of quadrocopter in state space form is derived, the particular implementation of university developed quadrocopter is described and the design of data processing algorithm is presented with measured results. Finally achieved results are discussed. Detailed record
	Stress, deformation and safety analysis of the generator stator loaded by nonhomogeneous temperature Majdič, Petr ; Dobeš, Martin (referee) ; Vrbka, Jan (advisor) This thesis deals with stress, strain and reliability analysis of synchronous generator stator including an inhomogeneous temperature field. Using the finite element method, stress and strain are calculated, and from these values safety against yield strength is determined, which is followed by the life calculation of the most stressed weld joint and the determination of its possible damage during the period required by the customer. Detailed record
	Quadrocopter - Sensory Subsytem Bradáč, František ; Šolc, František (referee) ; Žalud, Luděk (advisor) This diploma thesis deals with processing of measured data from inertial navigation system in order these could be used for stabilization. There is general information about aerial vehicles called copters with emphasis on four-rotor construction called quadrocopter at first. Then mathematical model of quadrocopter in state space form is derived, the particular implementation of university developed quadrocopter is described and the design of data processing algorithm is presented with measured results. Finally achieved results are discussed. Detailed record

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