Titlebook: EuCoMeS 2018; Proceedings of the 7 Burkhard Corves,Philippe Wenger,Mathias Hüsing Conference proceedings 2019 Springer Nature Switzerland A

Inelasticity

Fuzzy Logic Controller and PID Controller Design for Aircraft Pitch Controlime domain. In the end, the performances of pitch control are looked into and examined with respect to evaluation criteria of step response so as to determine which control method exhibits better performance depending on pitch angle and pitch rate. It is determined thanks to simulation that FLC shows better performance than PID controller.