Integrated guidance and control with impact angle constraint

Wangkui Liu; Yiyin Wei; Guangren Duan

doi:10.1109/CAC.2017.8242887

Integrated guidance and control with impact angle constraint

Wangkui Liu^*
, Yiyin Wei
, Guangren Duan

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

4 Scopus citations

Abstract

In this paper, an adaptive integrated guidance and control(IGC) law is proposed for the missile intercepting the maneuvering target with impact angle constraint. Considering the parameter uncertainties, a new IGC model is established. Subsequently, the dynamic surface control and adaptive technique are combined to design the adaptive IGC law. Finally, the simulation results are provided to verify the effectiveness of the presented IGC law.

Original language	English
Title of host publication	Proceedings - 2017 Chinese Automation Congress, CAC 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	866-871
Number of pages	6
ISBN (Electronic)	9781538635247
DOIs	https://doi.org/10.1109/CAC.2017.8242887
State	Published - 29 Dec 2017
Event	2017 Chinese Automation Congress, CAC 2017 - Jinan, China Duration: 20 Oct 2017 → 22 Oct 2017

Publication series

Name	Proceedings - 2017 Chinese Automation Congress, CAC 2017
Volume	2017-January

Conference

Conference	2017 Chinese Automation Congress, CAC 2017
Country/Territory	China
City	Jinan
Period	20/10/17 → 22/10/17

Keywords

Adaptive
Dynamic surface control
Impact angle constraint
Integrated guidance and control(IGC)

Access to Document

10.1109/CAC.2017.8242887

Cite this

@inproceedings{5869c541ccc84c7aa1a84fb194d4ed29,

title = "Integrated guidance and control with impact angle constraint",

abstract = "In this paper, an adaptive integrated guidance and control(IGC) law is proposed for the missile intercepting the maneuvering target with impact angle constraint. Considering the parameter uncertainties, a new IGC model is established. Subsequently, the dynamic surface control and adaptive technique are combined to design the adaptive IGC law. Finally, the simulation results are provided to verify the effectiveness of the presented IGC law.",

keywords = "Adaptive, Dynamic surface control, Impact angle constraint, Integrated guidance and control(IGC)",

author = "Wangkui Liu and Yiyin Wei and Guangren Duan",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 2017 Chinese Automation Congress, CAC 2017 ; Conference date: 20-10-2017 Through 22-10-2017",

year = "2017",

month = dec,

day = "29",

doi = "10.1109/CAC.2017.8242887",

language = "英语",

series = "Proceedings - 2017 Chinese Automation Congress, CAC 2017",

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

pages = "866--871",

booktitle = "Proceedings - 2017 Chinese Automation Congress, CAC 2017",

address = "美国",

}

Liu, W, Wei, Y & Duan, G 2017, Integrated guidance and control with impact angle constraint. in Proceedings - 2017 Chinese Automation Congress, CAC 2017. Proceedings - 2017 Chinese Automation Congress, CAC 2017, vol. 2017-January, Institute of Electrical and Electronics Engineers Inc., pp. 866-871, 2017 Chinese Automation Congress, CAC 2017, Jinan, China, 20/10/17. https://doi.org/10.1109/CAC.2017.8242887

Integrated guidance and control with impact angle constraint. / Liu, Wangkui; Wei, Yiyin; Duan, Guangren.
Proceedings - 2017 Chinese Automation Congress, CAC 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 866-871 (Proceedings - 2017 Chinese Automation Congress, CAC 2017; Vol. 2017-January).

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

TY - GEN

T1 - Integrated guidance and control with impact angle constraint

AU - Liu, Wangkui

AU - Wei, Yiyin

AU - Duan, Guangren

PY - 2017/12/29

Y1 - 2017/12/29

N2 - In this paper, an adaptive integrated guidance and control(IGC) law is proposed for the missile intercepting the maneuvering target with impact angle constraint. Considering the parameter uncertainties, a new IGC model is established. Subsequently, the dynamic surface control and adaptive technique are combined to design the adaptive IGC law. Finally, the simulation results are provided to verify the effectiveness of the presented IGC law.

AB - In this paper, an adaptive integrated guidance and control(IGC) law is proposed for the missile intercepting the maneuvering target with impact angle constraint. Considering the parameter uncertainties, a new IGC model is established. Subsequently, the dynamic surface control and adaptive technique are combined to design the adaptive IGC law. Finally, the simulation results are provided to verify the effectiveness of the presented IGC law.

KW - Adaptive

KW - Dynamic surface control

KW - Impact angle constraint

KW - Integrated guidance and control(IGC)

UR - https://www.scopus.com/pages/publications/85050343585

U2 - 10.1109/CAC.2017.8242887

DO - 10.1109/CAC.2017.8242887

M3 - 会议稿件

AN - SCOPUS:85050343585

T3 - Proceedings - 2017 Chinese Automation Congress, CAC 2017

SP - 866

EP - 871

BT - Proceedings - 2017 Chinese Automation Congress, CAC 2017

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2017 Chinese Automation Congress, CAC 2017

Y2 - 20 October 2017 through 22 October 2017

ER -

Integrated guidance and control with impact angle constraint

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