- Tytuł:
- Output Error Method for Tiltrotor Unstable in Hover
- Autorzy:
-
Lichota, P.
Szulczyk, J. - Powiązania:
- https://bibliotekanauki.pl/articles/140298.pdf
- Data publikacji:
- 2017
- Wydawca:
- Polska Akademia Nauk. Czytelnia Czasopism PAN
- Tematy:
-
flight dynamics
system identification
output error method
maximum likelihood
unstable system
tiltrotor
dynamika lotu
identyfikacja systemu
metoda błędu wyjścia
maksymalne prawdopodobieństwo
system niestabilny
zmiennopłat - Opis:
- This article investigates unstable tiltrotor in hover system identification from flight test data. The aircraft dynamics was described by a linear model defined in Body-Fixed-Coordinate System. Output Error Method was selected in order to obtain stability and control derivatives in lateral motion. For estimating model parameters both time and frequency domain formulations were applied. To improve the system identification performed in the time domain, a stabilization matrix was included for evaluating the states. In the end, estimates obtained from various Output Error Method formulations were compared in terms of parameters accuracy and time histories. Evaluations were performed in MATLAB R2009b environment.
- Źródło:
-
Archive of Mechanical Engineering; 2017, LXIV, 1; 23-36
0004-0738 - Pojawia się w:
- Archive of Mechanical Engineering
- Dostawca treści:
- Biblioteka Nauki
Artykuł