Receding horizon guidance laws for constrained missiles with autopilot lags

Ki Baek Kim, Tae Woong Yoon, Wook Hyun Kwon

Research output: Contribution to journalArticle

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 languageEnglish
Pages (from-to)1107-1115
Number of pages9
JournalControl Engineering Practice
Volume9
Issue number10
DOIs
Publication statusPublished - 2001 Oct 1

Fingerprint

Autopilot
Guidance Law
Electronic guidance systems
Missile
Missiles
Receding Horizon Control
Horizon
Input Constraints
Continuous time systems
Finite Horizon
Information use
State Constraints
Linear matrix inequalities
Weighting
Matrix Inequality
Linear Time
Continuous Time
Linear Inequalities
Invariant
Optimization

Keywords

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

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Industrial and Manufacturing Engineering

Cite this

Receding horizon guidance laws for constrained missiles with autopilot lags. / Kim, Ki Baek; Yoon, Tae Woong; Kwon, Wook Hyun.

In: Control Engineering Practice, Vol. 9, No. 10, 01.10.2001, p. 1107-1115.

Research output: Contribution to journalArticle

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