06.1 - Flight Dynamics and Control (Control & Modelling)
LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT
J. Vlkı, P. Chudyı, M. Prustomerskyı; ıBrno University of Technology, Czech Republic
The core of this work is aimed at flight control laws synthesis built around the optimal control theory. The researched flight control laws originating from the proposed design process were integrated into an experimental digital Flight Control System.The paper introduces the evaluation of the designed automatic Flight Control System in the real flight experiments.