H∞ guidance law with maneuvering targets

Ciann-Dong Yang, Hsin Yuan Chen

Research output: Contribution to journalArticle

2 Citations (Scopus)

Abstract

In this paper we propose an H robust guidance law for homing missiles with maneuvering targets. The nonlinear H suboptimal control design governed by the Hamilton-Jacobi PDE inequality associated with this guidance problem is solved analytically. Based on the existing nonlinear H techniques, we synthesize an H guidance law which can pursue a class of maneuvering targets with acceptable energy consumption and miss distance.

Original languageEnglish
Pages (from-to)2549-2550
Number of pages2
JournalProceedings of the IEEE Conference on Decision and Control
Volume3
Publication statusPublished - 1997

Fingerprint

Guidance Law
Electronic guidance systems
Missiles
Energy utilization
Suboptimal Control
Target
Hamilton-Jacobi
Missile
Control Design
Energy Consumption
Guidance
Class

All Science Journal Classification (ASJC) codes

  • Chemical Health and Safety
  • Control and Systems Engineering
  • Safety, Risk, Reliability and Quality

Cite this

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abstract = "In this paper we propose an H∞ robust guidance law for homing missiles with maneuvering targets. The nonlinear H∞ suboptimal control design governed by the Hamilton-Jacobi PDE inequality associated with this guidance problem is solved analytically. Based on the existing nonlinear H∞ techniques, we synthesize an H∞ guidance law which can pursue a class of maneuvering targets with acceptable energy consumption and miss distance.",
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H∞ guidance law with maneuvering targets. / Yang, Ciann-Dong; Chen, Hsin Yuan.

In: Proceedings of the IEEE Conference on Decision and Control, Vol. 3, 1997, p. 2549-2550.

Research output: Contribution to journalArticle

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AB - In this paper we propose an H∞ robust guidance law for homing missiles with maneuvering targets. The nonlinear H∞ suboptimal control design governed by the Hamilton-Jacobi PDE inequality associated with this guidance problem is solved analytically. Based on the existing nonlinear H∞ techniques, we synthesize an H∞ guidance law which can pursue a class of maneuvering targets with acceptable energy consumption and miss distance.

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