22nd Congress of International Council of the Aeronautical Sciences, Harrogate, UK, 28 August - 1st September, 2000
Paper ICAS 2000-P5.6

ROBUST CONTROL LAW SYNTHESIS FOR HIGH MANOEUVRABLE AIRCRAFT

R. Szabolcsi, L. Pokoradi, J. Bera
’Miklós Zrínyi’ National Defense University, Hungary

Keywords: controller, lqg, fighter aircraft, computer program

The purpose of the authors is to present a new design example for solution of the LQG controller synthesis problem for the high performance fighter aircraft. The closed loop time domain and the frequency domain behavior were tested. For the solution of the controller synthesis problem and for the control system time domain and frequency domain analysis a new computer program has been created by the authors.

view full paper