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Design of flight test laboratory for ballistic recovery systems testing
Chadima, Bedřich ; Pejchar, Jan (referee) ; Popela, Robert (advisor)
This thesis is focussed on designing of the air drop labradory for testing the balistic recovery systems. The first part of the thesis describes balistic recovery systems, their parts as well as methods of testing this devices. In the second charter there is a description of older vision of a testing device and simple test with the electronics of the testing device. The next step is designing of the new koncept of testing device and the structure analysis of the frame. The product of the thesis is a modular automated testing device, which is able to test balistic recovery systems for aicrafts with the weights between 230 and 1700 kilograms.
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Design of robotic arm module
Machala, Lukáš ; Kočiš, Petr (referee) ; Szabari, Mikuláš (advisor)
Robots of modular concept have each module functionally independent. They are continuously getting bigger representation on the market nowadays. This thesis contains research in the field of robotic arms and modular concepts. In the next part of the thesis, based on the calculations of structural nodes, were created modules in three sizes, which can be assembled into robotic arm.
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Design of robotic arm module
Machala, Lukáš ; Kočiš, Petr (referee) ; Szabari, Mikuláš (advisor)
Robots of modular concept have each module functionally independent. They are continuously getting bigger representation on the market nowadays. This thesis contains research in the field of robotic arms and modular concepts. In the next part of the thesis, based on the calculations of structural nodes, were created modules in three sizes, which can be assembled into robotic arm.
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Design of flight test laboratory for ballistic recovery systems testing
Chadima, Bedřich ; Pejchar, Jan (referee) ; Popela, Robert (advisor)
This thesis is focussed on designing of the air drop labradory for testing the balistic recovery systems. The first part of the thesis describes balistic recovery systems, their parts as well as methods of testing this devices. In the second charter there is a description of older vision of a testing device and simple test with the electronics of the testing device. The next step is designing of the new koncept of testing device and the structure analysis of the frame. The product of the thesis is a modular automated testing device, which is able to test balistic recovery systems for aicrafts with the weights between 230 and 1700 kilograms.
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