prikaz prve stranice dokumenta Parameters sensitivity analysis for generic helicopter flight model
Embargo period 2026-05-13
master's thesis
Parameters sensitivity analysis for generic helicopter flight model
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. urn:nbn:hr:235:551254
Matić, Filip
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

Institutional repository: Repository of Faculty of Mechanical Engineering and Naval Architecture University of Zagreb

Cite this document

Matić, F. (2024). Parameters sensitivity analysis for generic helicopter flight model (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:551254

Matić, Filip. "Parameters sensitivity analysis for generic helicopter flight model." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:551254

Matić, Filip. "Parameters sensitivity analysis for generic helicopter flight model." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:551254

Matić, F. (2024). 'Parameters sensitivity analysis for generic helicopter flight model', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 02 October 2024, https://urn.nsk.hr/urn:nbn:hr:235:551254

Matić F. Parameters sensitivity analysis for generic helicopter flight model [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2024 [cited 2024 October 02] Available at: https://urn.nsk.hr/urn:nbn:hr:235:551254

F. Matić, "Parameters sensitivity analysis for generic helicopter flight model", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2024. Available at: https://urn.nsk.hr/urn:nbn:hr:235:551254

Metadata
TitleParameters sensitivity analysis for generic helicopter flight model
Title (croatian)Analiza senzitivnosti parametara generičkog modela leta helikoptera
AuthorFilip Matić
MentorMilan Vrdoljak (mentor)
MentorPierluigi Capone https://orcid.org/0009-0006-5395-5670 (komentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2024-05-14, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Control
Abstract
This thesis presents a comprehensive approach to developing and tuning a helicopter flight model for simulation of flight performance, with a focus on a prototype helicopter under development. Conducted at Zürich University of Applied Sciences (ZHAW), the research involves several key tasks aimed at refining the model to achieve satisfactory similarity with real-flight data. The thesis begins with a description of the helicopter flight model and its relevant sub-models, including aerodynamics, propulsion, controls, and dynamics. Subsequently, potential tunable parameters for the model are identified through analysis of its components. These parameters are then subjected to sensitivity analysis to understand their impact on stability and overall flight characteristics. Based on the sensitivity analysis results, recommendations are made for a list of parameters deemed suitable for tuning the helicopter flight model. The criteria for evaluation encompass the significance of each parameter in influencing flight performance and the feasibility of adjusting them to match real-flight behavior. This research contributes to the advancement of helicopter flight modeling by providing a systematic methodology for parameter identification, sensitivity analysis, and model tuning. The findings offer insights into enhancing the fidelity of helicopter simulation models, with implications for various applications including training, research, and development.
Abstract (croatian)
Ovaj rad predstavlja sveobuhvatan pristup razvoju i podešavanju modela leta helikoptera za simulaciju leta, s fokusom na prototip helikoptera u razvoju. Provedeno na Zurich University of Applied Science (ZHAW), istraživanje uključuje nekoliko ključnih zadataka s ciljem usavršavanja modela kako bi se postigla zadovoljavajuća sličnost s podacima stvarnog leta. Rad započinje opisom modela leta helikoptera i pripadajućih podmodela, uključujući aerodinamiku, pogon, upravljanje i dinamiku. Naknadno, potencijalni prilagodljivi parametri za model identificiraju se kroz analizu njegovih komponenti. Ti parametri potom su podvrgnuti analizi osjetljivosti kako bi se razumio njihov utjecaj na stabilnost i ukupne karakteristike leta. Na temelju rezultata analize osjetljivosti, donosi se popis parametara koji se smatraju prikladnima za podešavanje modela leta helikoptera. Kriteriji za ocijenjivanje obuhvaćaju značaj utjecaja svakog parametra na dinamiku leta i letnih performansi te provedbu prilagodbe usklađivanja s ponašanjem u stvarnom letu. Ovo istraživanje doprinosi napretku modeliranja leta helikoptera pružajući sustavnu metodologiju za identifikaciju parametara, analizu osjetljivosti i podešavanje modela. Dobiveni rezultati nude uvide u poboljšanje vjernosti modela simulacije helikoptera, s implikacijama za različite primjene, uključujući obuku, istraživanje i razvoj.
Keywords
Keywords (english)
Languageenglish
URN:NBNurn:nbn:hr:235:551254
Study programmeTitle: Aeronautical Studies
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva (magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsEmbargoed access
Embargo expiration date: 2026-05-13
Terms of useLicence In copyright icon
Created on2024-05-15 12:13:05