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undergraduate thesis
Analiza jednadžbe gibanja zrakoplova za različite režime leta
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2015. urn:nbn:hr:119:145417
Fujs, David
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics

Institutional repository: Faculty of Transport and Traffic Sciences

Cite this document

Fujs, D. (2015). Analiza jednadžbe gibanja zrakoplova za različite režime leta (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:145417

Fujs, David. "Analiza jednadžbe gibanja zrakoplova za različite režime leta." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2015. https://urn.nsk.hr/urn:nbn:hr:119:145417

Fujs, David. "Analiza jednadžbe gibanja zrakoplova za različite režime leta." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2015. https://urn.nsk.hr/urn:nbn:hr:119:145417

Fujs, D. (2015). 'Analiza jednadžbe gibanja zrakoplova za različite režime leta', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 25 July 2024, https://urn.nsk.hr/urn:nbn:hr:119:145417

Fujs D. Analiza jednadžbe gibanja zrakoplova za različite režime leta [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2015 [cited 2024 July 25] Available at: https://urn.nsk.hr/urn:nbn:hr:119:145417

D. Fujs, "Analiza jednadžbe gibanja zrakoplova za različite režime leta", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2015. Available at: https://urn.nsk.hr/urn:nbn:hr:119:145417

Metadata
TitleAnaliza jednadžbe gibanja zrakoplova za različite režime leta
Title (english)Analysis of Equation of Motion for Various Flight Regimes
AuthorDavid Fujs
MentorDavor Franjković (mentor)
Committee memberAnita Domitrović (predsjednik povjerenstva)
Committee memberKarolina Krajček Nikolić (član povjerenstva)
Committee memberŽeljko Marušić (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2015-09-01, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Gibanje zrakoplova može se promatrati u više koordinatnih sustava. Iz lokalnog koordinatnog sustava, koji je vezan za Zemlju, pomoću matričnih transformacija prelazi se u ostale koordinatne sustave. Primjenom drugog Newtonovog zakona na gibanje zrakoplova, izvode se jednadžbe gibanja zrakoplova za šest stupnjeva slobode gibanja, koje se dijele na jednadžbe translacijskog i rotacijskog gibanja. Iako zrakoplov nastoji ostati u ravnotežnom položaju, na njega utječu male sile poremećaja, koje dodatno otežavaju izračun. Komponente gibanja, s obzirom na ravninu u kojoj djeluju, opisuju longitudinalno i laterelno gibanje. Također, nakon zapisivanja jednadžbi u linearnom obliku i proširivanjem pomoću Taylorovih redova, moguće je promatrati gibanje za specifične slučajeve. U jednolikim režimima leta, gibanje zrakoplova je idealizirano, a jednadžbe koje opisuju takve režime, iako pojednostavljene, imaju bolju primjenu od općenitih izraza. Alternativni zapisi jednadžbi gibanja su jednadžbe stanja i izlaza. Izražavanjem linearnih sustava u frekvencijskoj domeni, moguće je dobiti funkciju prijenosa.
Abstract (english)
Motion of an aircraft can be examined in several coordinate systems. Using transformation matrices, it is possible to transfer from Earth-fixed coordinate system into other ones. By application of Newton's second law, equations of motion of an aircraft for its six degrees of freedom, which are divided into the equations of translational and rotational motion, are derived. An aircraft strives to remain in equilibrium, although small perturbation forces act on it, which additionally complicate the calculation. Components of motion, considering the plane in which they act, describe longitudinal and lateral motion. Also, after linearization of equations and expansion of terms using Taylor series, it is possible to examine motion for specific cases. Motion of an aircraft is idealized in steady maneuvering flight conditions and equations which describe those conditions, although simplified, are of greater practical use than general expressions. Alternative forms of equations of motions are state and output equation. By expressing linear systems in the frequency domain, it is possible to obtain transfer function.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:145417
Study programmeTitle: Aeronautics
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike (sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike)
Type of resourceText
File originBorn digital
Access conditionsOpen access
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Created on2015-09-16 12:43:25