Constrained nonlinear receding horizon control and its application to a thrust vectored aircraft

Author

Lee, Y.I. ; Kouvaritakis, B. ; Cannon, M.

Author_Institution

Div. of Electr. & Electron. Eng., Gyeongsang Nat. Univ., Jinju Gyeong-Nam, South Korea

Volume

2

fYear

2001

fDate

2001

Firstpage

1186

Abstract

This paper presents a receding horizon control method for input constrained nonlinear systems. The optimization procedure is based on predictions made by incremental models at points made by linearized incremental models set points of a given seed trajectory and the effect of linearization error are taken into account to give a bound on the predicted tracking error. The results of the algorithm are illustrated by applying the proposed algorithm to a simplified model of a thrust vectored aircraft

Keywords

aerospace propulsion; aircraft control; linearisation techniques; nonlinear control systems; predictive control; stability; constrained nonlinear receding horizon control; input constrained nonlinear systems; linearization error; linearized incremental models set points; optimization procedure; predicted tracking error; predictive control; receding horizon control method; seed trajectory; stability; thrust vectored aircraft; Aerospace control; Aerospace electronics; Aerospace engineering; Aircraft propulsion; Dynamic programming; Nonlinear systems; Predictive models; Quadratic programming; Trajectory; Upper bound;

fLanguage

English

Publisher

ieee

Conference_Titel

Industrial Electronics, 2001. Proceedings. ISIE 2001. IEEE International Symposium on

Conference_Location

Pusan

Print_ISBN

0-7803-7090-2

Type

conf

DOI

10.1109/ISIE.2001.931647

Filename

931647