Please use this identifier to cite or link to this item: http://hdl.handle.net/11455/48779
DC FieldValueLanguage
dc.contributor.author林俊良zh_TW
dc.contributor.other國立中興大學電機工程學系(所)zh_TW
dc.contributor.other行政院國家科學委員會zh_TW
dc.date2004zh_TW
dc.date.accessioned2014-06-06T08:31:49Z-
dc.date.available2014-06-06T08:31:49Z-
dc.identifierNSC92-2213-E005-025zh_TW
dc.identifier.urihttp://hdl.handle.net/11455/48779-
dc.language.isozh_TWzh_TW
dc.subject電子電機工程類zh_TW
dc.subject應用研究zh_TW
dc.title彈道飛彈軌跡估測及反飛彈控制系統設計(III)-子計畫IV:反飛彈導引律及側力控制系統研發zh_TW
dc.titleDevelopment of Anti-Missile Guidance Law and Side Force Control Systemen_US
dc.typeResearch Reportszh_TW
item.cerifentitytypePublications-
item.grantfulltextnone-
item.languageiso639-1zh_TW-
item.fulltextno fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.openairetypeResearch Reports-
Appears in Collections:電機工程學系所
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