Guidance scheme for operating multiple ship defense missiles with dual seekers

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This paper proposes a guidance scheme to operate ship defense missiles using dual seekersradio frequency and strapdown imaging infrared seekersagainst the threat of antiship missiles. Key challenges associated with considered operational concept such as the multipath error of an radio frequency seeker, the narrow field of view of an strapdown imaging infrared seeker, and the interference between the target and defense missiles are identified. A guidance scheme that can address these challenges is proposed by combining an optimal guidance law for the midcourse phase and the proportional navigation guidance for the terminal phase. A relationship among interceptor/target velocity, minimum line-of-sight angle for the radio frequency seeker, and the field of view of the strapdown imaging infrared seeker for a successful intercept is analytically derived and graphically presented. Numerical simulations for the engagements between ship defense missiles and an antiship missile demonstrate the validity of the proposed guidance scheme.
Publisher
SAGE PUBLICATIONS LTD
Issue Date
2016-03
Language
English
Article Type
Article
Keywords

OF-VIEW LIMITS; ANTISHIP MISSILES; IMPACT-TIME; LAW; ANGLE

Citation

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.230, no.4, pp.601 - 614

ISSN
0954-4100
DOI
10.1177/0954410015594637
URI
http://hdl.handle.net/10203/208334
Appears in Collection
AE-Journal Papers(저널논문)
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