Tytuł artykułu
Autorzy
Identyfikatory
Warianty tytułu
Konferencja
Proceedings of the Third Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(III; 23-25.11.1998; Warszawa, Polska)
Języki publikacji
Abstrakty
A new approach to the problem of aircraft motion mathematical model structural-parametrical identification is proposed by using spectral analysis. By applying the Finite Fourier Transform to flight test data, a family of frequency characteristics and then mathematical model parameters estimation are derived. Modeling transients are executed for the purpose of comparison with flight test data. The usefulness of this algorithm is illustrated by applying to real flight test records. Finally, research into the applicability of the developed algorithm in predicting the handling qualities levels ofrotorcraft (ADS-33 C) was conducted.
Czasopismo
Rocznik
Tom
Strony
53--58
Opis fizyczny
Bibliogr. 7 poz., rys., wykr.
Twórcy
autor
- Moscow State Aviation Institute (Technological University), Russia, tium@dynamics.mainet.mks.su
Bibliografia
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-PWA3-0037-0006