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Design of UAV hardware - mechanical and electrical subsystem
Kraus, David ; Hrbáček, Jan (referee) ; Krejsa, Jiří (advisor)
Main topic of this thesis is creation of platform for testing stabilization and control algorithms for UAV. For chosen suitable model plane was designed a structure of control and power electronics. Research of suitable algorithms was made and some of them were implemented. For this algorithms gains were designed, using simulation. The whole system was tested and validated in flight.
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Development of aircraft systems
Sokol, Filip ; Kaddour, Mirvat (referee) ; Trefilová, Helena (advisor)
The bachelor thesis with the name „Development of aircraft systems“ deals with development of flight control, electrical, hydraulic and fuel systems of aircraft type CS-23 and CS-25. The thesis is divided into particular chapters; each one concerns with description of particular system. The development is always mentioned at the beginning of each chapter and the rest is dedicated to basic description. There are mentioned the latest trends in flying control of the aircraft and a description of gradual transition into concepts More Electric Aircraft and More Electric Engine in the end of the thesis. The very end is comprised of comparison of aircrafts according to the aircraft systems they use.
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Design of UAV hardware - mechanical and electrical subsystem
Kraus, David ; Hrbáček, Jan (referee) ; Krejsa, Jiří (advisor)
Main topic of this thesis is creation of platform for testing stabilization and control algorithms for UAV. For chosen suitable model plane was designed a structure of control and power electronics. Research of suitable algorithms was made and some of them were implemented. For this algorithms gains were designed, using simulation. The whole system was tested and validated in flight.
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Development of aircraft systems
Sokol, Filip ; Kaddour, Mirvat (referee) ; Trefilová, Helena (advisor)
The bachelor thesis with the name „Development of aircraft systems“ deals with development of flight control, electrical, hydraulic and fuel systems of aircraft type CS-23 and CS-25. The thesis is divided into particular chapters; each one concerns with description of particular system. The development is always mentioned at the beginning of each chapter and the rest is dedicated to basic description. There are mentioned the latest trends in flying control of the aircraft and a description of gradual transition into concepts More Electric Aircraft and More Electric Engine in the end of the thesis. The very end is comprised of comparison of aircrafts according to the aircraft systems they use.
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