Study on roll angle control for hovering tilt rotor aircraft on one side thrust reduction

Abstract

In this study a synthesis of flight control system which is able to control the roll angle of hovering Tilt Rotor Aircraft (TRA) on one side thrust reduction, which seriously affects the stability of TRA motion, is proposed. Basically this flight control system is constructed with roll angle feedback as stability augmentation method and P or PI control as controllability augmentation method.