Pregled bibliografske jedinice broj: 1150862
Aerodynamic coefficients estimation of a general aviation airplane from flight test data
Aerodynamic coefficients estimation of a general aviation airplane from flight test data, 2021., diplomski rad, diplomski, Fakultet strojarstva i brodogradnje, Zagreb
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Naslov
Aerodynamic coefficients estimation of a general aviation airplane from flight test data
(Estimacija aerodinamičkih koeficijenata za avion opće avijacije iz podataka s testnih letova)
Autori
Haber-Zelanto, David
Vrsta, podvrsta i kategorija rada
Ocjenski radovi, diplomski rad, diplomski
Fakultet
Fakultet strojarstva i brodogradnje
Mjesto
Zagreb
Datum
21.01
Godina
2021
Stranica
82
Mentor
Vrdoljak, Milan ; Capone, Pierluigi
Neposredni voditelj
Monstein, Raphael
Ključne riječi
parameter estimation, Piper PA-28-161, flight test data, sensor error model, flight path reconstruction, aerodynamic coefficients, linear regression, moments of inertia, engine model, manoeuvre
Sažetak
In the summer of 2019 the Center for Aviation at the Zürich University of Applied Sciences conducted a flight test campaign on a Piper Pa-28-161 airplane. Since then, they have the goal of a self-made model of a Piper PA-28 which can be implemented in their Research and Didactics Simulator. This thesis is concerned with all the necessary data gathering and set up for a parameter estimation process determining aerodynamic coefficient models. Along with the basic introduction to the system identification and parameter estimation, this thesis provides an overview of the flight test data, instrumentation and test points together with some challenges and issues that have to be mentioned before the data can be used. After the processing procedure of the flight test data, it is shown how the estimation of the mass, balance and inertia of the aircraft is performed. Next, engine forces and moments needed for aerodynamic coefficient calculation are computed. Additional data corrections and sensor error model development with flight path reconstruction is presented as well. Finally, after all the data is gathered and assembled, parameter estimation with linear estimation is done using the ordinary least squares method. Exemplary models of the aerodynamic coefficients are offered as well.
Izvorni jezik
Engleski
Znanstvena područja
Zrakoplovstvo, raketna i svemirska tehnika
Napomena
In association with Center for Aviation at the Zürich University of Applied Sciences (ZHAW) for a flight test campaign on a Piper Pa-28-161 airplane. Dr. Pierluigi Capone was comentor.
POVEZANOST RADA
Ustanove:
Fakultet strojarstva i brodogradnje, Zagreb
Profili:
Milan Vrdoljak
(mentor)