Robust guidance law for space interception

Di Zhou; Fulian Duan

Robust guidance law for space interception

Di Zhou^*
, Fulian Duan

^*Corresponding author for this work

School of Astronautics

Harbin Normal University

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

1 Scopus citations

Abstract

In space interception, a linear time-varying model is established to describe the missile-target relative line-of-sight (LOS) motion, where guidance parameters' variations and target maneuvers are regarded as gain bounded disturbances. From this model, a robust guidance law of homing-missile is derived and its robustness against the gain bounded uncertainty is proved by Lyapunov-like approach. Simulation results also demonstrates the effectiveness of the presented guidance method.

Original language	English
Pages	3389-3393
Number of pages	5
State	Published - 2000
Event	Proceedings of the 3th World Congress on Intelligent Control and Automation - Hefei, China Duration: 28 Jun 2000 → 2 Jul 2000

Conference

Conference	Proceedings of the 3th World Congress on Intelligent Control and Automation
Country/Territory	China
City	Hefei
Period	28/06/00 → 2/07/00

Cite this

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title = "Robust guidance law for space interception",

abstract = "In space interception, a linear time-varying model is established to describe the missile-target relative line-of-sight (LOS) motion, where guidance parameters' variations and target maneuvers are regarded as gain bounded disturbances. From this model, a robust guidance law of homing-missile is derived and its robustness against the gain bounded uncertainty is proved by Lyapunov-like approach. Simulation results also demonstrates the effectiveness of the presented guidance method.",

author = "Di Zhou and Fulian Duan",

year = "2000",

language = "英语",

pages = "3389--3393",

note = "Proceedings of the 3th World Congress on Intelligent Control and Automation ; Conference date: 28-06-2000 Through 02-07-2000",

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TY - CONF

T1 - Robust guidance law for space interception

AU - Zhou, Di

AU - Duan, Fulian

PY - 2000

Y1 - 2000

N2 - In space interception, a linear time-varying model is established to describe the missile-target relative line-of-sight (LOS) motion, where guidance parameters' variations and target maneuvers are regarded as gain bounded disturbances. From this model, a robust guidance law of homing-missile is derived and its robustness against the gain bounded uncertainty is proved by Lyapunov-like approach. Simulation results also demonstrates the effectiveness of the presented guidance method.

AB - In space interception, a linear time-varying model is established to describe the missile-target relative line-of-sight (LOS) motion, where guidance parameters' variations and target maneuvers are regarded as gain bounded disturbances. From this model, a robust guidance law of homing-missile is derived and its robustness against the gain bounded uncertainty is proved by Lyapunov-like approach. Simulation results also demonstrates the effectiveness of the presented guidance method.

UR - https://www.scopus.com/pages/publications/0034591345

M3 - 论文

AN - SCOPUS:0034591345

SP - 3389

EP - 3393

T2 - Proceedings of the 3th World Congress on Intelligent Control and Automation

Y2 - 28 June 2000 through 2 July 2000

ER -

Robust guidance law for space interception

Abstract

Conference

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