The continuation framework for nonlinear dynamics of an agike aircraft

• Autorzy: Sibilski K. , Żyluk A.

Warianty tytułu

PL

Kontynuacyjna metoda badania nieliniowej dynamiki samolotu supermanewrowego

• Języki publikacji: EN

Abstrakty

EN

This paper describes the implementation of continuation methods and bifurcation analysis in the "global" identification of an agile aircraft dynamics. In the examples presented, it integrates features of eigenstructure methods within the nonlinear state-parameter environment. The basis of the continuation analysis is outlined and demonstrated using a highly nonlinear aircraft model.

PL

W pracy opisano zastosowanie metod kontynuacyjnych i analizy bifurkacyjnej do "globalnej" identyfikacji dynamiki lotu samolotu supermanewrowego. Przedstawiono cechy sprzężeń zwrotnych pozwalających na osiągnięcie założonej struktury wartości własnych, w zakresie nieliniowości parametrów stanu.

Słowa kluczowe

PL

samolot supermanewrowy; dynamika lotu

• Wydawca: Warsaw University of Technology, Faculty of Transport
• Czasopismo: Archives of Transport
• Rocznik: 2006
• Tom: Vol. 18, iss. 1
• Strony: 71--86
• Opis fizyczny: Bibliogr. 19 poz., rys.

Twórcy

autor

Sibilski K.

autor

Żyluk A.

• Instytut Techniczny Wojsk Lotniczych, 01-494 Warszawa, ul. Księcia Bolesława 6

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