Modal control approach to the test maneuver design for aircraft flight tests

• Autorzy: Brusov V. , Ovcharenko V.
• 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

A problem of test maneuver design is discussed in the case of statically unstable aircraft. The results obtained can be applied to formulation of the control laws for an aircraft within a predetermined frequency range. There appears a kind of duality for such control laws, namely, an input signal stabilizes and disturbs the dynamic system states at the same time.

Słowa kluczowe

EN

aircrafts; maneuver aircraft; modal control

PL

samoloty; manewry samolotu; sterowanie modalne

• 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: 2001
• Tom: nr 11
• Strony: 25--28
• Opis fizyczny: Bibliogr. 3 poz., wykr.

Twórcy

autor

Brusov V.

autor

Ovcharenko V.

• Rzeszów University of Technology, Poland