Design of guidance law for passive homing missile using sliding mode control

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dc.contributor.authorLee, C.-H.-
dc.contributor.authorKim, T.-H.-
dc.contributor.authorTahk, Min-Jea-
dc.date.accessioned2013-03-28T12:42:30Z-
dc.date.available2013-03-28T12:42:30Z-
dc.date.created2012-02-06-
dc.date.issued2010-10-27-
dc.identifier.citationInternational Conference on Control, Automation and Systems, ICCAS 2010, v., no., pp.2380 - 2385-
dc.identifier.urihttp://hdl.handle.net/10203/165779-
dc.languageENG-
dc.titleDesign of guidance law for passive homing missile using sliding mode control-
dc.typeConference-
dc.identifier.scopusid2-s2.0-78751535826-
dc.type.rimsCONF-
dc.citation.beginningpage2380-
dc.citation.endingpage2385-
dc.citation.publicationnameInternational Conference on Control, Automation and Systems, ICCAS 2010-
dc.identifier.conferencecountrySouth Korea-
dc.identifier.conferencecountrySouth Korea-
dc.contributor.localauthorTahk, Min-Jea-
dc.contributor.nonIdAuthorLee, C.-H.-
dc.contributor.nonIdAuthorKim, T.-H.-
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AE-Conference Papers(학술회의논문)
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