1 articles published in Asrel Aerospace Research Letters with the keyword "Yunuslama Açısı": Comparison of PID Coefficients Determination Methods for Aircraft Pitch Angle Control
Saliha Köprücü, MUHAMMET ÖZTÜRK
Asrel Aerospace Research Letters, 2024, Vol 3, Issue 1, Page 15-26
In this study, the pitch angle of an aircraft is controlled using 4 different methods found in the literature. The linearized longitudinal equations of motion of the aircraft selected to be controlled in this study were obtained from the sources in the literature and the control application was...
Tyreus-LuybenZiegler-NicholsAstrom ve HagglundModifiye Edilmiş Ziegler-NicholsPID KontrolcüsüUzunlamasına HareketAstrom and HagglundLongitudinal MotionModified Ziegler-NicholsPID ControllerPitch Angle
