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Návrh mechanického a elektrického subsystému bezpilotního letounu / Design of UAV hardware - mechanical and electrical subsystem

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.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:231203
Date January 2014
CreatorsKraus, David
ContributorsHrbáček, Jan, Krejsa, Jiří
PublisherVysoké učení technické v Brně. Fakulta strojního inženýrství
Source SetsCzech ETDs
LanguageCzech
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/masterThesis
Rightsinfo:eu-repo/semantics/restrictedAccess

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