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

dc.contributor.author陳永平en_US
dc.contributor.authorCHEN YON-PINGen_US
dc.contributor.department國立交通大學控制工程研究所zh_TW
dc.date.accessioned2014-12-13T10:39:52Z
dc.date.available2014-12-13T10:39:52Z
dc.date.issued1995en_US
dc.description.sponsorship行政院國家科學委員會zh_TW
dc.identifier.govdocNSC84-2212-E009-045zh_TW
dc.identifier.urihttps://www.grb.gov.tw/search/planDetail?id=171035&docId=28900en_US
dc.identifier.urihttps://ir.lib.nycu.edu.tw/handle/11536/96904
dc.language.isozh_TWen_US
dc.title超音速飛機之飛行控制系統設計---子計畫三:可 變結構系統原理在飛行控制上之應用(II)zh_TW
dc.titleTheory of Variable Structure System Applied to the Flight Control(II)en_US
dc.typePlanen_US

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