Određivanje parametara leta za avion Pilatus PC-9M tijekom prilaženja s konstantnim napadnim kutom

master's thesis

• Title (english): Determining the flight characteristics of the PC-9M during constant angle of attack approach
• Author: Antonio Sučić
• Mentor: Doris Novak (mentor)
• Committee member: Petar Andraši (predsjednik povjerenstva)
• Committee member: Tino Bucak (član povjerenstva)
• Committee member: Tomislav Radišić (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Aeronautics); (Department of Aeronautics); Zagreb
• Defense date and country: 2024-05-16, 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: Napadni kut; prilaženja; Pilatus; PC-9M; izračun; određivanje; tehnika pilotiranja; raspored pažnje
• Keywords (english): Angle-of-Attack; approach; Pilatus PC-9M; calculation; determining; piloting technique; onspeed
• Language: croatian
• URN:NBN: urn:nbn:hr:119:609003
• Study programme: Title: 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 resource: Text
• File origin: Born digital
• Access conditions: Open access
• Created on: 2024-12-09 13:14:15