Fault tolerant control for missile guidance laws with finite-time convergence

Zheng Zhu; Yuanqing Xia; Mengyin Fu; Shuo Wang

doi:10.1109/CCDC.2011.5968388

Fault tolerant control for missile guidance laws with finite-time convergence

Zheng Zhu^*, Yuanqing Xia, Mengyin Fu, Shuo Wang

^*Corresponding author for this work

School of Automation

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

9 Citations (Scopus)

Abstract

This paper aims to develop hit-to-kill guidance laws for missile interception with actuator faults. New fault-tolerant control schemes with sliding mode control and finite-time control are proposed for the design of guidance laws to achieve the interception in the presence of bounded target acceleration. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

Original language	English
Title of host publication	Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011
Pages	1288-1293
Number of pages	6
DOIs	https://doi.org/10.1109/CCDC.2011.5968388
Publication status	Published - 2011
Event	2011 Chinese Control and Decision Conference, CCDC 2011 - Mianyang, China Duration: 23 May 2011 → 25 May 2011

Publication series

Name	Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011

Conference

Conference	2011 Chinese Control and Decision Conference, CCDC 2011
Country/Territory	China
City	Mianyang
Period	23/05/11 → 25/05/11

Keywords

Fault tolerant control
Finite-time control
Guidance law
Sliding mode control

Access to Document

10.1109/CCDC.2011.5968388

Cite this

@inproceedings{33731efffc0c46adabe64b580dd034a6,

title = "Fault tolerant control for missile guidance laws with finite-time convergence",

abstract = "This paper aims to develop hit-to-kill guidance laws for missile interception with actuator faults. New fault-tolerant control schemes with sliding mode control and finite-time control are proposed for the design of guidance laws to achieve the interception in the presence of bounded target acceleration. Also, simulation results are presented to illustrate the effectiveness of the control strategies.",

keywords = "Fault tolerant control, Finite-time control, Guidance law, Sliding mode control",

author = "Zheng Zhu and Yuanqing Xia and Mengyin Fu and Shuo Wang",

year = "2011",

doi = "10.1109/CCDC.2011.5968388",

language = "English",

isbn = "9781424487363",

series = "Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011",

pages = "1288--1293",

booktitle = "Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011",

note = "2011 Chinese Control and Decision Conference, CCDC 2011 ; Conference date: 23-05-2011 Through 25-05-2011",

}

Zhu, Z, Xia, Y, Fu, M & Wang, S 2011, Fault tolerant control for missile guidance laws with finite-time convergence. in Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011., 5968388, Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011, pp. 1288-1293, 2011 Chinese Control and Decision Conference, CCDC 2011, Mianyang, China, 23/05/11. https://doi.org/10.1109/CCDC.2011.5968388

Fault tolerant control for missile guidance laws with finite-time convergence. / Zhu, Zheng; Xia, Yuanqing; Fu, Mengyin et al.
Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011. 2011. p. 1288-1293 5968388 (Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Fault tolerant control for missile guidance laws with finite-time convergence

AU - Zhu, Zheng

AU - Xia, Yuanqing

AU - Fu, Mengyin

AU - Wang, Shuo

PY - 2011

Y1 - 2011

N2 - This paper aims to develop hit-to-kill guidance laws for missile interception with actuator faults. New fault-tolerant control schemes with sliding mode control and finite-time control are proposed for the design of guidance laws to achieve the interception in the presence of bounded target acceleration. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

AB - This paper aims to develop hit-to-kill guidance laws for missile interception with actuator faults. New fault-tolerant control schemes with sliding mode control and finite-time control are proposed for the design of guidance laws to achieve the interception in the presence of bounded target acceleration. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

KW - Fault tolerant control

KW - Finite-time control

KW - Guidance law

KW - Sliding mode control

UR - http://www.scopus.com/inward/record.url?scp=80052197138&partnerID=8YFLogxK

U2 - 10.1109/CCDC.2011.5968388

DO - 10.1109/CCDC.2011.5968388

M3 - Conference contribution

AN - SCOPUS:80052197138

SN - 9781424487363

T3 - Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011

SP - 1288

EP - 1293

BT - Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011

T2 - 2011 Chinese Control and Decision Conference, CCDC 2011

Y2 - 23 May 2011 through 25 May 2011

ER -

Fault tolerant control for missile guidance laws with finite-time convergence

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this