Naslov
Aerodynamic model development for general aviation aircraft based on flight test data

Autori
Đeverlija, Jan Juraj

Vrsta, podvrsta i kategorija rada
Ocjenski radovi, diplomski rad, diplomski

Fakultet
Fakultet strojarstva i brodogradnje

Mjesto
Zagreb

Datum
16.12

Godina
2021

Stranica
67

Mentor
Vrdoljak, Milan

Neposredni voditelj
Capone, Pierluigi

Ključne riječi
Piper PA-28, parameter estimation, aerodynamic coefficients, flight path reconstruction, sensor error model, linear regression, output-error method

Sažetak
This master thesis is a continuation of the work on a project of aerodynamic model development for a general aviation airplane, Piper PA-28, conducted by Centre for aviation at the Zürich University of Applied Sciences. After previous flight test data processing and organizing, a basic linear model was introduced. In this thesis its improvement was made, but before improvement itself, using flight path reconstruction it is necessary to develop sensor error model, as precisely as possible. Great attention is dedicated exactly to this part. Completion of the flight path reconstruction, with corrected sensor values, using linear regression aerodynamic parameters are estimated with ordinary least square method. Focus is put on longitudinal motion, such as stall, phugoid and short period manoeuvres.

Izvorni jezik
Engleski

Znanstvena područja
Zrakoplovstvo, raketna i svemirska tehnika

POVEZANOST RADA