Helicopter flight controller design using nonlinear transformation

Author

Hamidi, H. Ebneddin ; Ohta, H.

Author_Institution

Dept. of Aerosp. Eng., Nagoya Univ., Japan

fYear

1995

fDate

26-28 Jul 1995

Firstpage

1481

Lastpage

1486

Abstract

In this study synthesis of a helicopter trajectory controller is described. Nonlinear transformation theory has been used in the design of the control system to represent nonlinearities in the model of the system. The singular perturbation theory is used to simplify control system structure and a new algorithm has been synthesized for the inverse nonlinear transformation of the control terms. Problem of modeling errors in the system with nonlinear inverse dynamics theory is investigated. The results of simulation show that the control system could track commanded values under the presence of modeling errors and disturbances

Keywords

aircraft control; control system synthesis; dynamics; helicopters; inverse problems; nonlinear control systems; transforms; disturbances; helicopter flight controller design; helicopter trajectory controller; inverse nonlinear transformation; modeling errors; nonlinear inverse dynamics theory; nonlinear transformation; singular perturbation theory; Adaptive control; Control system synthesis; Error correction; Helicopters; Inverse problems; Nonlinear control systems; Nonlinear dynamical systems; Nonlinear equations; Uncertain systems; Velocity control;

fLanguage

English

Publisher

ieee

Conference_Titel

SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers

Conference_Location

Hokkaido

Print_ISBN

0-7803-2781-0

Type

conf

DOI

10.1109/SICE.1995.526733

Filename

526733