Kopytova K. Complex Control of the Aircraft with the Distributed System of Aerodynamic Forces

The object of research is the process of compensation of disturbed atmosphere actions in a conflict situation using the automatic control system. The aim of the thesis is to improve the quality of the aircraft evasion maneuver in a conflict situation which is complicated by the influence of the disturbed atmosphere. The theory of automatic control was used to create the mathematical model of automatic control system of the aircraft mass center. Method of the absolute invariance was used to create the block diagram of the compensation actions of disturbed atmosphere. The data of Clark Y and NACA 23012 airfoils which were blown in the wind tunnel were used to calculate the change of aerodynamic forces and moments at the deviation of wing mechanization components. Software development methods are based on the use of environment MATLAB of Simulink package. Analysis of the results of experiments was conducted using the methods of mathematical statistics. The theoretical significance of the results are in the development of the concept of integrated flight control of the aircraft, which is different from existing distributed system of aerodynamic forces (protected by 3 patents). The results of the thesis research are of great practical importance for the design of modern aviation technology. The method of distributed aerodynamic compensation of the disturbed atmosphere actions on the aircraft flight path was developed. The method of integrated control of aircraft flight altitude was improved. Implementation of the work was done in the scientific work of the International Research and Training Center of Information Technologies and Systems NAS and MES of Ukraine. The methods, mathematical models and algorithms can be used in the design and engineering institutions in the design of modern aircraft and in the training courses of specialist training in the field of systems and processes control.