Title :
Study on roll angle control for hovering tilt rotor aircraft on one side thrust reduction
Author :
Osa, Yasuhiro ; Uchikado, Shigeru ; Tanaka, Kanya
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.
Keywords :
PI control; aircraft control; control system synthesis; controllability; feedback; motion control; stability; PI control; TRA motion stability; controllability augmentation method; flight control system synthesis; roll angle control; roll angle feedback; stability augmentation method; tilt rotor aircraft; Aerospace control; Aircraft; Mathematical model; Numerical stability; Pi control; Stability analysis;
Conference_Titel :
Automatic Control Conference (CACS), 2014 CACS International
Print_ISBN :
978-1-4799-4586-3
DOI :
10.1109/CACS.2014.7097175
