Mathematical Modeling and Investigation of Angle-of-Attack and Load Factor Limiting Systems for Combat Aircraft using Matlab Simulink

This paper presents the results of a survey on the effectiveness of a system for limiting the critical parameters of an aircraft during vertical maneuvering. The aircraft's motion model, combined with the critical parameter limiting system model, was constructed using Matlab Simulink software. The paper presents the results of the survey on the effectiveness of the critical parameter limiting system on the model and compares them with experimental results in the aircraft user manuals of the Air Force Officer School. Using this method, it is possible to determine the corresponding parameters in the system, calculate the system's efficiency, and then apply it in the practical use of this type of aircraft.