Application of the non-linear filtering method to determination an optimal control of aircraft manoeuvres

• Autorzy: Goetzendorf-Grabowski T.
• 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 an application of the non-linear filtering method to determination the optimal control function of the aircraft manoeuvres. Theoretical grounds of the filtering problem and the main idea of its application for the identification problem were shown. The method, originally applied to a parametrical identification was adapted to determination a control function. A mathematical model of an aircraft flight was developed for considered case. Paper shows the results of a numerical example for a fire fighting aircraft. The calculation results concern control function determination and parametrical identification as well.

Słowa kluczowe

EN

filtering method; optimal control; aircraft manoeuvres

PL

metoda filtracyjna; kontrola optymalna; manewry samolotu

• 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: 95--98
• Opis fizyczny: Bibliogr. 10 poz., rys., wykr.

Twórcy

autor

Goetzendorf-Grabowski T.

• Warsaw University of Technology, Warsaw, Poland