제어로봇시스템학회:학술대회논문집

Institute of Control, Robotics and Systems (제어로봇시스템학회)
권호 표지

SYNTHESIS OF DISCRETE TIME FLIGHT CONTROL SYSTEM USING NONLINEAR MODEL MATCHING

  • Aoi, Kazunari (Dept. of Mechanical Eng.,Kobe City College of Technology) ;
  • Osa, Yasuhiro (Dept. of Mechanical Eng.,Kobe City College of Technology) ;
  • Uchikado, Shigeru (School of Science and Engineering, Tokyo Denski University)
  • Published : 2000.10.01
Download PDF
⟨ Previous Next ⟩

Abstract

Until now various model matching systems have been proposed for linear system, but very little has been done for nonlinear system In this paper, a design method of discrete time flight control system using nonlinear model matching is proposed. This method is based on Hirschorn's algorithm and facilitates easy determination of the control law using the relationship, between the output and the input, which is obtained by the time shift of the output. Also as a result, this method is the extension of the linear model matching control system proposed by Wolovich, in which the control law is obtained by left-multiplying the output by the interactor matrix. At the end of paper, the proposed control system is applied to CCV flight control system of an aircraft and the feasibility of the proposed approach is shown by the numerical simulations.

Keywords