Uçak eğim kontrol sistemi için ölüm oyunu optimizasyonuna dayalı PID-F denetleyicisi tasarımı.

In this article, PID-F controller is proposed for aircraft pitch control (APC) system in order to obtain a better dynamic system response. PID-F controller represents P proportional action with gain (kp), I integral action with gain (ki), D derivative action with gain (kd) and F derivative filter with gain (kf). Battle royale optimization (BRO) algorithm is used to find the optimal values of the independent parameters kp, ki, kd and kf. The performance of the BRO based PID-F controller has been verified by comparing with the BRO based PID controller. In addition, in order to make a more comprehensive performance evaluation, the BRO based PID-F controller is compared to the PID controllers existing in the literature for the same aircraft pitch control system, designed using harris hawks optimization (HHO) and atom search optimization (ASO). Transient response, frequency response and pole-zero analyses are used for comparative analysis. The results obtained from the simulations show that the proposed BRO/PID-F controller is superior to other controllers in terms of improving the transient and frequency responses of the APC system. [ABSTRACT FROM AUTHOR]