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

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

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

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

Dept. of Electrical and Information Engineering

Gyeongsang National University

Research output: Contribution to conference › Paper › peer-review

1 Scopus citations

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 eat 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 trust vectored aircraft.

Original language	English
Pages	1186-1191
Number of pages	6
State	Published - 2001
Event	2001 IEEE International Symposium on Industrial Electronics Proceedings (ISIE 2001) - Pusan, Korea, Republic of Duration: 12 Jun 2001 → 16 Jun 2001

Conference

Conference	2001 IEEE International Symposium on Industrial Electronics Proceedings (ISIE 2001)
Country/Territory	Korea, Republic of
City	Pusan
Period	12/06/01 → 16/06/01

Cite this

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title = "Constrained nonlinear receding horizon control and its application to a thrust vectored aircraft",

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 eat 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 trust vectored aircraft.",

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AU - Lee, Y. I.

AU - Kouvaritakis, B.

AU - Cannon, M.

PY - 2001

Y1 - 2001

N2 - 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 eat 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 trust vectored aircraft.

AB - 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 eat 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 trust vectored aircraft.

UR - https://www.scopus.com/pages/publications/0034856515

M3 - Paper

AN - SCOPUS:0034856515

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EP - 1191

T2 - 2001 IEEE International Symposium on Industrial Electronics Proceedings (ISIE 2001)

Y2 - 12 June 2001 through 16 June 2001

ER -

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

Abstract

Conference

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