31th Congress of the International Council of the Aeronautical Sciences

06.1 - Flight Dynamics and Control (Control & Modelling)

APPLICATION OF THE DISTURBANCE VALUE MEASURED DURING THE REAL FLIGHT TO THE FLIGHT CONTROL SYSTEM SYNTHESIS

T. Rogalski╣, A. Tomczyk╣; ╣Rzeszˇw University of Technology, Poland

The essence of the proposed method is to separate the measurement noise and the effects of external disturbances from the of registered in-flight onboard sensor signals. In this way, in the design process we can take into consideration the real disturbances causes on aircraft.


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