Receding horizon guidance laws for constrained missiles with autopilot lags

Ki Baek Kim; Tae Woong Yoon; Wook Hyun Kwon

doi:10.1016/S0967-0661(01)00084-3

Receding horizon guidance laws for constrained missiles with autopilot lags

Ki Baek Kim, Tae Woong Yoon, Wook Hyun Kwon

School of Electrical Engineering

Research output: Contribution to journal › Article › peer-review

5 Citations (Scopus)

Abstract

In this paper, a new stabilizing receding horizon control (RHC) scheme is proposed for linear continuous time-invariant systems with input and state constraints. The control scheme is based on the minimization of the finite horizon cost with a finite terminal weighting matrix subject to constraints. A new algorithm is suggested to implement the RHC scheme for a constrained receding horizon guidance law (CRHG). The proposed CRHG, which does not use information on the time-to-go, is obtained by using linear matrix inequality (LMI) optimization. Through simulation examples, the performance of the proposed CRHG is illustrated.

Original language	English
Pages (from-to)	1107-1115
Number of pages	9
Journal	Control Engineering Practice
Volume	9
Issue number	10
DOIs	https://doi.org/10.1016/S0967-0661(01)00084-3
Publication status	Published - 2001 Oct

Keywords

Autopilots lags
Constraints
Guidance laws
LMI
RHC
Time-to-go

ASJC Scopus subject areas

Control and Systems Engineering
Computer Science Applications
Electrical and Electronic Engineering
Applied Mathematics

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10.1016/S0967-0661(01)00084-3

Cite this

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title = "Receding horizon guidance laws for constrained missiles with autopilot lags",

abstract = "In this paper, a new stabilizing receding horizon control (RHC) scheme is proposed for linear continuous time-invariant systems with input and state constraints. The control scheme is based on the minimization of the finite horizon cost with a finite terminal weighting matrix subject to constraints. A new algorithm is suggested to implement the RHC scheme for a constrained receding horizon guidance law (CRHG). The proposed CRHG, which does not use information on the time-to-go, is obtained by using linear matrix inequality (LMI) optimization. Through simulation examples, the performance of the proposed CRHG is illustrated.",

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AU - Yoon, Tae Woong

AU - Kwon, Wook Hyun

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N2 - In this paper, a new stabilizing receding horizon control (RHC) scheme is proposed for linear continuous time-invariant systems with input and state constraints. The control scheme is based on the minimization of the finite horizon cost with a finite terminal weighting matrix subject to constraints. A new algorithm is suggested to implement the RHC scheme for a constrained receding horizon guidance law (CRHG). The proposed CRHG, which does not use information on the time-to-go, is obtained by using linear matrix inequality (LMI) optimization. Through simulation examples, the performance of the proposed CRHG is illustrated.

AB - In this paper, a new stabilizing receding horizon control (RHC) scheme is proposed for linear continuous time-invariant systems with input and state constraints. The control scheme is based on the minimization of the finite horizon cost with a finite terminal weighting matrix subject to constraints. A new algorithm is suggested to implement the RHC scheme for a constrained receding horizon guidance law (CRHG). The proposed CRHG, which does not use information on the time-to-go, is obtained by using linear matrix inequality (LMI) optimization. Through simulation examples, the performance of the proposed CRHG is illustrated.

KW - Autopilots lags

KW - Constraints

KW - Guidance laws

KW - LMI

KW - RHC

KW - Time-to-go

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ER -

Receding horizon guidance laws for constrained missiles with autopilot lags

Abstract

Keywords

ASJC Scopus subject areas

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