Numerical analysis of the sensivity of aircraft flight control at high angles of attack

• Autorzy: Złocka M.
• Konferencja: Proceedings of the Fourth Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(IV; 30.11-02.12.2000; Warszawa, Polska)
• Języki publikacji: EN

Abstrakty

EN

The paper presents the results of numerical analysis of the sensitivity of aircraft flight control carried out on a mathematical model chosen. The control is designed using the non-linear inverse dynamics method. Non-linear control laws have been synthesised for wing rock stabilisation. As an example the numerical simulation of a controlled motion is carried out employing the aerodynamic and mass data of the F-16 aircraft.

Słowa kluczowe

EN

aircrafts; numerical analysis; flight control

PL

samoloty; analiza numeryczna; kontrola lotu

• Wydawca: Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology
• Czasopismo: Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics
• Rocznik: 2000
• Tom: nr 10
• Strony: 225--230
• Opis fizyczny: Bibliogr. 18 poz., rys., wykr.

Twórcy

autor

Złocka M.

• Warsaw University of Technology, Warsaw, Poland