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master's thesis
Određivanje parametara leta za avion Pilatus PC-9M tijekom prilaženja s konstantnim napadnim kutom
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2024. urn:nbn:hr:119:609003
Sučić, Antonio
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

Sučić, A. (2024). Određivanje parametara leta za avion Pilatus PC-9M tijekom prilaženja s konstantnim napadnim kutom (Master's thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:609003

Sučić, Antonio. "Određivanje parametara leta za avion Pilatus PC-9M tijekom prilaženja s konstantnim napadnim kutom." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2024. https://urn.nsk.hr/urn:nbn:hr:119:609003

Sučić, Antonio. "Određivanje parametara leta za avion Pilatus PC-9M tijekom prilaženja s konstantnim napadnim kutom." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2024. https://urn.nsk.hr/urn:nbn:hr:119:609003

Sučić, A. (2024). 'Određivanje parametara leta za avion Pilatus PC-9M tijekom prilaženja s konstantnim napadnim kutom', Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 28 December 2024, https://urn.nsk.hr/urn:nbn:hr:119:609003

Sučić A. Određivanje parametara leta za avion Pilatus PC-9M tijekom prilaženja s konstantnim napadnim kutom [Master's thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2024 [cited 2024 December 28] Available at: https://urn.nsk.hr/urn:nbn:hr:119:609003

A. Sučić, "Određivanje parametara leta za avion Pilatus PC-9M tijekom prilaženja s konstantnim napadnim kutom", Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2024. Available at: https://urn.nsk.hr/urn:nbn:hr:119:609003

Metadata
TitleOdređivanje parametara leta za avion Pilatus PC-9M tijekom prilaženja s konstantnim napadnim kutom
Title (english)Determining the flight characteristics of the PC-9M during constant angle of attack approach
AuthorAntonio Sučić
MentorDoris Novak (mentor)
Committee memberPetar Andraši (predsjednik povjerenstva)
Committee memberTino Bucak (član povjerenstva)
Committee memberTomislav Radišić (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2024-05-16, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Avion PC-9M je opremljen instrumentom s pomoću kojeg se leti s konstantnim napadnim kutom, ali takvo letenje ne ulazi u obuku učenika letača i nije obrađeno u priručnicima letenja istog aviona. U Sjedinjenim Američkim državama se takvo letenje koristi pri slijetanju na nosačima aviona i slijetanju višenamjenskim borbenim avionima. S obzirom na to da je Hrvatsko ratno zrakoplovstvo nabavilo višenamjenske borbene avione Dassault Rafale, PC-9M može služiti kao platforma za obuku učenika letača za prilaženje konstantnim napadnim kutom koji su kandidati za preobuku na tim avionima. U ovom radu se opisuje postupak izračunavanja parametara leta pri konstantnom napadnom kutu, podatci se uspoređuju sa stvarnim podatcima s probnog leta i definirat će se tehnika pilotiranja koja bi se mogla koristiti u budućoj obuci učenika letača. Probnim letovima su potvrđeni izračunati podatci te su mjereni dodatni podatci leta pri konstantnom napadnom kutu. Raspisana je tehnika pilotiranja i raspored pažnje za prilaženje konstantnim napadnim kutom iz školskog kruga, iz pravca i tijekom ILS prilaženja. Na drugom probnom letu se izvelo 6 školskih krugova sa prilaženjem konstantnim napadnim kutom kako bi potvrdili raspisanu tehniku pilotiranja i raspored pažnje.
Abstract (english)
The PC-9M is equipped with an instrument used while flying with a constant angle of attack (onspeed), but such is not included in the training of student pilots and is not covered in the flight manuals of the same aircraft. In the United States of America, such flying is used when landing on aircraft carriers and landing fighter aircraft. Given that the Croatian Air Force has acquired the Dassault Rafale, the PC-9M can serve as a platform for training student pilots for constant angle-of-attack flight. This thesis describes the procedure for calculating the flight characteristics at a constant angle of attack, compares them with data from a test flight, and defines a piloting technique that could be used in the training of student pilots. The calculated data was confirmed during a test flight and additional data during constant angle-of-attack flight was measured. The piloting technique for constant angle-of-attack approach from a traffic circuit, straight in and during ILS approach is defined. On the second test flight, 6 traffic circuits were performed with a constant angle of attack approach in order to confirm the prescribed piloting technique.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:609003
Study programmeTitle: Aeronautics
Study programme type: university
Study level: graduate
Academic / professional title: sveučilišni/a magistar/magistra inženjer/inženjerka aeronautike (sveučilišni/a magistar/magistra inženjer/inženjerka aeronautike)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2024-12-09 13:14:15