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Návrh a rozbor LQ-regulátoru pro podélný a stranový pohyb letadla / LQ-regulator design and its analysis for the aircraft's longitudinal and lateral motion

This diploma thesis is focused on designing and specifying a linear quadratic regulator for longitudinal and lateral motion of the aircraft. The regulator is designed for a linear system obtained from a linearization of our nonlinear dynamic dynamic model of aircraft around the basic reference state (trimmed state-and-level ight). To nd a complete description of this reference state, some optimality problem has to be solved and the solution of this problem is called a trimmed state.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:232106
Date January 2015
CreatorsPrešinský, Ján
ContributorsZatočilová, Jitka, Nechvátal, Luděk
PublisherVysoké učení technické v Brně. Fakulta strojního inženýrství
Source SetsCzech ETDs
LanguageSlovak
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/masterThesis
Rightsinfo:eu-repo/semantics/restrictedAccess

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