Investigation of Aircraft Control Loop Characteristics

In this paper, we study the characteristics of the control loop of an aircraft. It can be used in the scientific research of control systems, aerodynamics, flight dynamics, simulation. The purpose and volume of the semi-real simulation are determined by the program of semi-real-time simulation on the IC. The main goals of the semi-realistic simulation are as follows: • verification of the correctness of the structure and parameters of the missile stabilization system; • assessment of the quality of processes and stability stocks on the flight trajectories to the starting points of autonomous flight tests; • checking the functioning of on-board equipment and software. Research in the work showed that the IMS allows you to fully assess the qualitative and quantitative characteristics of the contours of stabilization and control of the missile, to assess the impact on them of various disturbing effects.