Robust roll-pitch-yaw integrated autopilot for a high angle-of-attack missile

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dc.contributor.authorKang, S.-
dc.contributor.authorKim, H.J.-
dc.contributor.authorWon, D.-
dc.contributor.authorTahk, Min-Jea-
dc.contributor.authorLee, J.-I.-
dc.contributor.authorJun, B.-E.-
dc.date.accessioned2013-03-27T00:44:08Z-
dc.date.available2013-03-27T00:44:08Z-
dc.date.created2012-02-06-
dc.date.issued2008-08-18-
dc.identifier.citationAIAA Guidance, Navigation and Control Conference and Exhibit, v., no., pp. --
dc.identifier.urihttp://hdl.handle.net/10203/157594-
dc.languageENG-
dc.titleRobust roll-pitch-yaw integrated autopilot for a high angle-of-attack missile-
dc.typeConference-
dc.identifier.scopusid2-s2.0-78651065962-
dc.type.rimsCONF-
dc.citation.publicationnameAIAA Guidance, Navigation and Control Conference and Exhibit-
dc.identifier.conferencecountryUnited States-
dc.identifier.conferencecountryUnited States-
dc.contributor.localauthorTahk, Min-Jea-
dc.contributor.nonIdAuthorKang, S.-
dc.contributor.nonIdAuthorKim, H.J.-
dc.contributor.nonIdAuthorWon, D.-
dc.contributor.nonIdAuthorLee, J.-I.-
dc.contributor.nonIdAuthorJun, B.-E.-
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AE-Conference Papers(학술회의논문)
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