prikaz prve stranice dokumenta Proračun putanje instrumentalnog prilaženja zrakoplova u nestandardnim atmosferskim uvjetima
  Download
PDF 1.9 MB
undergraduate thesis
Proračun putanje instrumentalnog prilaženja zrakoplova u nestandardnim atmosferskim uvjetima
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2020. urn:nbn:hr:119:199005
Bošnjak, Marko
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

Bošnjak, M. (2020). Proračun putanje instrumentalnog prilaženja zrakoplova u nestandardnim atmosferskim uvjetima (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:199005

Bošnjak, Marko. "Proračun putanje instrumentalnog prilaženja zrakoplova u nestandardnim atmosferskim uvjetima." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2020. https://urn.nsk.hr/urn:nbn:hr:119:199005

Bošnjak, Marko. "Proračun putanje instrumentalnog prilaženja zrakoplova u nestandardnim atmosferskim uvjetima." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2020. https://urn.nsk.hr/urn:nbn:hr:119:199005

Bošnjak, M. (2020). 'Proračun putanje instrumentalnog prilaženja zrakoplova u nestandardnim atmosferskim uvjetima', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 03 June 2024, https://urn.nsk.hr/urn:nbn:hr:119:199005

Bošnjak M. Proračun putanje instrumentalnog prilaženja zrakoplova u nestandardnim atmosferskim uvjetima [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2020 [cited 2024 June 03] Available at: https://urn.nsk.hr/urn:nbn:hr:119:199005

M. Bošnjak, "Proračun putanje instrumentalnog prilaženja zrakoplova u nestandardnim atmosferskim uvjetima", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2020. Available at: https://urn.nsk.hr/urn:nbn:hr:119:199005

Metadata
TitleProračun putanje instrumentalnog prilaženja zrakoplova u nestandardnim atmosferskim uvjetima
Title (english)Aircraft Instrument Approach Trajectory Calculation in Non-Standard Atmospheric Conditions
AuthorMarko Bošnjak
MentorDoris Novak (mentor)
Committee memberTomislav Radišić (predsjednik povjerenstva)
Committee memberTino Bucak (član povjerenstva)
Committee memberJurica Ivošević (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2020-07-14, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Instrumentalno prilaženje definirano je načinom elektroničkog vođenja zrakoplova u horizontalnoj i vertikalnoj ravnini. Visina se u zrakoplovu standardno mjeri barometarskim visinomjerom. Temperatura zraka važan je čimbenik u određivanju visine leta koji nije kompenziran barometarskim visinomjerom. Kada je temperatura zraka manja od standardne vrijednosti, zrakoplov će biti niže nego što pokazuje visinomjer. Za određenu vrstu instrumentalnog prilaženja koristi se isključivo barometarski visinomjer kao izvor podataka o visini leta za proračun vertikalnog profila prilaženja. Stoga je u ovom radu objašnjen utjecaj temperature zraka na visinu leta, navedena je jednadžba za korekciju indicirane visine pri niskim temperaturama zraka te su razrađeni postupci koje posada zrakoplova mora poduzeti prilikom proračuna visina u prilaženju kako bi se osiguralo sigurno nadvišavanje prepreka.
Abstract (english)
Instrument approach is defined by the method of electronic guidance of an aircraft in the lateral and vertical modes. The altitude of the aircraft is usually measured by a barometric altimeter. Air temperature is an important factor in determining the aircraft’s altitude which is not compensated by the barometric altimeter. When the air temperature is lower than the standard value, the aircraft will be lower than indicated by the altimeter. For a specific type of instrument approach, the barometric altimeter is used exclusively as the altitude source for the calculation of the vertical approach profile. Therefore, this paper explains the influence of air temperature on altitude, states the equation for the correction of indicated altitude at low air temperatures and describes the procedures that the flight crew must perform when calculating altitudes during approach to ensure safe obstacle clearance.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:199005
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
Terms of useLicence In copyright icon
Created on2020-08-21 10:36:39