Performance Evaluation of Automatic Control Systems in Commercial and Private Aircraft Using the FSX Flight Simulator

Abstract

This study aims to evaluate the performance of automatic heading and altitude control systems in commercial and private aircraft using the FSX flight simulator. The research employs an experimental methodology involving the creation of various simulated flight scenarios under different weather and operational conditions. Data obtained from these simulations are analyzed to assess the behavior of the automatic systems, focusing on key parameters such as error, settling time, and response time. The main findings indicate that the aircraft category and weather conditions, such as precipitation, wind speed, and wind direction, have a significant impact on the performance of automatic control systems. These variables affect the error signal and settling time, which are crucial for determining the aircraft's stability under various operating conditions. The analysis of the transient response and error signal reveals that the transfer function is unique and specific to each type of aircraft. This finding highlights the importance of developing and optimizing automatic control systems that are robust, reliable, and adaptable to the particular characteristics of each aircraft and the simulated flight conditions. In conclusion, this study provides essential information for the design and evaluation of automatic control systems in commercial aviation. The results highlight the need to integrate these considerations into the development of technologies that enhance stability, safety, and operational efficiency in air transport. This comprehensive approach is crucial for improving safety and reliability in air operations, particularly in challenging environments.