Optimal sliding-mode guidance of a homing-missile

Di Zhou; Chundi Mu; Qiang Ling; Wenli Xu

Optimal sliding-mode guidance of a homing-missile

Di Zhou^*
, Chundi Mu
, Qiang Ling
, Wenli Xu

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Contribution to journal › Conference article › peer-review

32 Scopus citations

Abstract

An optimal guidance law based on missile-target LOS angular rate is presented for intercepting a nonmaneuvering target. It is then integrated with sliding-mode control theory to derive an optimal sliding-mode guidance law for intercepting a maneuvering target. The new guidance method's robustness against target maneuvers and good miss distance performance are proved by the second method of Lyapunov and simulation results. The presented guidance law is simple to implement in practical applications.

Original language	English
Pages (from-to)	5131-5136
Number of pages	6
Journal	Proceedings of the IEEE Conference on Decision and Control
Volume	5
State	Published - 1999
Event	The 38th IEEE Conference on Decision and Control (CDC) - Phoenix, AZ, USA Duration: 7 Dec 1999 → 10 Dec 1999

Cite this

@article{7309004b56c24022a8a030b43ec049b0,

title = "Optimal sliding-mode guidance of a homing-missile",

abstract = "An optimal guidance law based on missile-target LOS angular rate is presented for intercepting a nonmaneuvering target. It is then integrated with sliding-mode control theory to derive an optimal sliding-mode guidance law for intercepting a maneuvering target. The new guidance method's robustness against target maneuvers and good miss distance performance are proved by the second method of Lyapunov and simulation results. The presented guidance law is simple to implement in practical applications.",

author = "Di Zhou and Chundi Mu and Qiang Ling and Wenli Xu",

year = "1999",

language = "英语",

volume = "5",

pages = "5131--5136",

journal = "Proceedings of the IEEE Conference on Decision and Control",

issn = "0743-1546",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

note = "The 38th IEEE Conference on Decision and Control (CDC) ; Conference date: 07-12-1999 Through 10-12-1999",

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TY - JOUR

T1 - Optimal sliding-mode guidance of a homing-missile

AU - Zhou, Di

AU - Mu, Chundi

AU - Ling, Qiang

AU - Xu, Wenli

PY - 1999

Y1 - 1999

N2 - An optimal guidance law based on missile-target LOS angular rate is presented for intercepting a nonmaneuvering target. It is then integrated with sliding-mode control theory to derive an optimal sliding-mode guidance law for intercepting a maneuvering target. The new guidance method's robustness against target maneuvers and good miss distance performance are proved by the second method of Lyapunov and simulation results. The presented guidance law is simple to implement in practical applications.

AB - An optimal guidance law based on missile-target LOS angular rate is presented for intercepting a nonmaneuvering target. It is then integrated with sliding-mode control theory to derive an optimal sliding-mode guidance law for intercepting a maneuvering target. The new guidance method's robustness against target maneuvers and good miss distance performance are proved by the second method of Lyapunov and simulation results. The presented guidance law is simple to implement in practical applications.

UR - https://www.scopus.com/pages/publications/0033352201

M3 - 会议文章

AN - SCOPUS:0033352201

SN - 0743-1546

VL - 5

SP - 5131

EP - 5136

JO - Proceedings of the IEEE Conference on Decision and Control

JF - Proceedings of the IEEE Conference on Decision and Control

T2 - The 38th IEEE Conference on Decision and Control (CDC)

Y2 - 7 December 1999 through 10 December 1999

ER -

Optimal sliding-mode guidance of a homing-missile

Abstract

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