Guidance law implementation with performance recovery using an extended high-gain observer

Kemao Ma; Hassan K. Khalil; Yu Yao

doi:10.1016/j.ast.2011.11.005

Guidance law implementation with performance recovery using an extended high-gain observer

Kemao Ma^*
, Hassan K. Khalil
, Yu Yao

^*Corresponding author for this work

School of Astronautics, Harbin Institute of Technology
Michigan State University

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

35 Scopus citations

Abstract

Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input-multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance.

Original language	English
Pages (from-to)	177-186
Number of pages	10
Journal	Aerospace Science and Technology
Volume	24
Issue number	1
DOIs	https://doi.org/10.1016/j.ast.2011.11.005
State	Published - 2013
Externally published	Yes

Keywords

Guidance law
High-gain observer
Performance recovery
Target maneuver

Access to Document

10.1016/j.ast.2011.11.005

Cite this

@article{659899aa9cbc4fe29e961f6ed5862977,

title = "Guidance law implementation with performance recovery using an extended high-gain observer",

abstract = "Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input-multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance.",

keywords = "Guidance law, High-gain observer, Performance recovery, Target maneuver",

author = "Kemao Ma and Khalil, \{Hassan K.\} and Yu Yao",

year = "2013",

doi = "10.1016/j.ast.2011.11.005",

language = "英语",

volume = "24",

pages = "177--186",

journal = "Aerospace Science and Technology",

issn = "1270-9638",

publisher = "Elsevier Masson s.r.l.",

number = "1",

}

TY - JOUR

T1 - Guidance law implementation with performance recovery using an extended high-gain observer

AU - Ma, Kemao

AU - Khalil, Hassan K.

AU - Yao, Yu

PY - 2013

Y1 - 2013

N2 - Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input-multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance.

AB - Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input-multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance.

KW - Guidance law

KW - High-gain observer

KW - Performance recovery

KW - Target maneuver

UR - https://www.scopus.com/pages/publications/84875521364

U2 - 10.1016/j.ast.2011.11.005

DO - 10.1016/j.ast.2011.11.005

M3 - 文章

AN - SCOPUS:84875521364

SN - 1270-9638

VL - 24

SP - 177

EP - 186

JO - Aerospace Science and Technology

JF - Aerospace Science and Technology

IS - 1

ER -

Guidance law implementation with performance recovery using an extended high-gain observer

Abstract

Keywords

Access to Document

Other files and links

Fingerprint

Cite this