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超音速飛機之飛行控制系統設計(總計畫)子計畫三:可變結構系統原理在飛行控制上之應用

dc.contributor.author陳永平 zh_TW
dc.contributor.department交通大學控制工程研究所 zh_TW
dc.date.accessioned2016-12-20T03:57:07Z
dc.date.available2016-12-20T03:57:07Z
dc.date.issued1993en_US
dc.description.abstract zh_TW
dc.description.abstract en_US
dc.description.sponsorship行政院國家科學委員會 zh_TW
dc.identifier.govdocNSC82-0424-E009-327 zh_TW
dc.identifier.urihttps://www.grb.gov.tw/search/planDetail?id=55459&docId=8141en_US
dc.identifier.urihttps://ir.lib.nycu.edu.tw/handle/11536/132178
dc.language.isozh_TWen_US
dc.subject zh_TW
dc.subject en_US
dc.title超音速飛機之飛行控制系統設計(總計畫)子計畫三:可變結構系統原理在飛行控制上之應用zh_TW
dc.titleTheory of Variable Structure System Appied in the Fight Control Systemen_US
dc.typePlanen_US

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