Title :
Design of a nonlinear flight controller based on dynamic inversion
Author :
Baba, Yoriaki ; Takano, Hiroyuki ; Sano, Masaki
Author_Institution :
Dept. of Aerosp. Eng., Nat. Defense Acad., Yokosuka, Japan
Abstract :
This paper deals with a synthesis for a nonlinear flight controller using a nonlinear state feedback. This method is called a dynamic inversion theory and is widely used to design a nonlinear flight controller. We show how to choose the control gains for the controller designed by a dynamic inversion theory when inversion is not exact due to the actuator lags
Keywords :
aircraft control; control system synthesis; nonlinear control systems; state feedback; control gains; dynamic inversion; nonlinear flight controller design; nonlinear state feedback; Actuators; Aerodynamics; Aerospace engineering; Aircraft; Ear; Nonlinear equations; Proportional control; Robustness; State estimation; State feedback;
Conference_Titel :
SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers
Conference_Location :
Hokkaido
Print_ISBN :
0-7803-2781-0
DOI :
10.1109/SICE.1995.526734
