Synthesis of Nonlinear Model Matching Flight Control System for Tilt Rotor Aircraft

  • Asada, Yasuhiro (The Advanced Course of Mechanical Systems Engineering, Kobe City College of Technology) ;
  • Osa, Yasuhiro (Department of Mechanical Engineering, Kobe City College of Technology) ;
  • Uchikado, Shigeru (School of Science and Engineering, Tokyo Denki University) ;
  • Tanaka, Kanya (Faculty of Engineering, Yamaguchi University)
  • Published : 2005.06.02

Abstract

In this study, we suggest a tilt rotor aircraft and attempt to apply a nonlinear model matching control method for its maneuver. The proposed method is very simple and useful to construct the control law for the complicated nonlinear system such as aircraft motion.

Keywords