Interceptor guidance law based on relative heading error angle

Naiming Qi; Yunqian Li; Xing Cheng

doi:10.1109/ICMA.2009.5245088

Interceptor guidance law based on relative heading error angle

Naiming Qi^*
, Yunqian Li
, Xing Cheng

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

2 Scopus citations

Abstract

This paper presents a new guidance law based on relative heading error angle (RHEA) for endo-atmospheric interception. RHEA is the angle between the relative velocity vector and the line-of-sight (LOS). Driving it to zero can ensure a head-on engagement. Sliding mode control theory is employed to design this new guidance law. The performance of the proposed guidance law is studied through simulation for different engagement scenarios, and compared with sliding mode guidance law based on LOS rate.

Original language	English
Title of host publication	2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009
Pages	567-571
Number of pages	5
DOIs	https://doi.org/10.1109/ICMA.2009.5245088
State	Published - 2009
Event	2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009 - Changchun, China Duration: 9 Aug 2009 → 12 Aug 2009

Publication series

Name	2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009

Conference

Conference	2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009
Country/Territory	China
City	Changchun
Period	9/08/09 → 12/08/09

Keywords

Guidance law
Interception
Sliding mode control

Access to Document

10.1109/ICMA.2009.5245088

Cite this

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title = "Interceptor guidance law based on relative heading error angle",

abstract = "This paper presents a new guidance law based on relative heading error angle (RHEA) for endo-atmospheric interception. RHEA is the angle between the relative velocity vector and the line-of-sight (LOS). Driving it to zero can ensure a head-on engagement. Sliding mode control theory is employed to design this new guidance law. The performance of the proposed guidance law is studied through simulation for different engagement scenarios, and compared with sliding mode guidance law based on LOS rate.",

keywords = "Guidance law, Interception, Sliding mode control",

author = "Naiming Qi and Yunqian Li and Xing Cheng",

year = "2009",

doi = "10.1109/ICMA.2009.5245088",

language = "英语",

isbn = "9781424426935",

series = "2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009",

pages = "567--571",

booktitle = "2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009",

note = "2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009 ; Conference date: 09-08-2009 Through 12-08-2009",

}

Qi, N, Li, Y & Cheng, X 2009, Interceptor guidance law based on relative heading error angle. in 2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009., 5245088, 2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009, pp. 567-571, 2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009, Changchun, China, 9/08/09. https://doi.org/10.1109/ICMA.2009.5245088

Interceptor guidance law based on relative heading error angle. / Qi, Naiming; Li, Yunqian; Cheng, Xing.
2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009. 2009. p. 567-571 5245088 (2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009).

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

TY - GEN

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AU - Qi, Naiming

AU - Li, Yunqian

AU - Cheng, Xing

PY - 2009

Y1 - 2009

N2 - This paper presents a new guidance law based on relative heading error angle (RHEA) for endo-atmospheric interception. RHEA is the angle between the relative velocity vector and the line-of-sight (LOS). Driving it to zero can ensure a head-on engagement. Sliding mode control theory is employed to design this new guidance law. The performance of the proposed guidance law is studied through simulation for different engagement scenarios, and compared with sliding mode guidance law based on LOS rate.

AB - This paper presents a new guidance law based on relative heading error angle (RHEA) for endo-atmospheric interception. RHEA is the angle between the relative velocity vector and the line-of-sight (LOS). Driving it to zero can ensure a head-on engagement. Sliding mode control theory is employed to design this new guidance law. The performance of the proposed guidance law is studied through simulation for different engagement scenarios, and compared with sliding mode guidance law based on LOS rate.

KW - Guidance law

KW - Interception

KW - Sliding mode control

UR - https://www.scopus.com/pages/publications/77449147099

U2 - 10.1109/ICMA.2009.5245088

DO - 10.1109/ICMA.2009.5245088

M3 - 会议稿件

AN - SCOPUS:77449147099

SN - 9781424426935

T3 - 2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009

SP - 567

EP - 571

BT - 2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009

T2 - 2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009

Y2 - 9 August 2009 through 12 August 2009

ER -

Interceptor guidance law based on relative heading error angle

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