Basanets O. Synthesis of the Robust Control System for Guidance of the Rotating Uunmanned Aerial Vehicle by Laser Beam

The thesis is devoted to the robust system synthesis in a case of incomplete state space measurments, structure and unstructure uncertainties for guidance process of rotating UAV. The parametric robust optimization procedure with Н2/Нinf -norms of closed-loop system and constraints on system oscillativity is developed. The rotating UAV dynamic controller synthesis technique for guidance system is devoted. The dynamic controller is founded under linear matrix inequalities (LMI) approach. The unified technique which is basing on L2-gain design problem under LMI approach is devoted. The designed technique permits to synthesise systems with various control signal structure. The fuzzy type 2 PID-controller design technique is devoted. Key worlds: rotating UAV, H2/Hinf - robust optimization, static output feedback, linear matrix inequality, PID-controller, tracking system, fuzzy type 2 controller.