可變結構系統理論在飛彈導引律設計上之應用

完整後設資料紀錄

DC 欄位	值	語言
dc.contributor.author	陳永平	en_US
dc.contributor.author	CHEN YON-PING	en_US
dc.date.accessioned	2014-12-13T10:34:15Z	-
dc.date.available	2014-12-13T10:34:15Z	-
dc.date.issued	2002	en_US
dc.identifier.govdoc	NSC91-CS-7009-004	zh_TW
dc.identifier.uri	http://hdl.handle.net/11536/92622	-
dc.identifier.uri	https://www.grb.gov.tw/search/planDetail?id=696768&docId=132064	en_US
dc.description.sponsorship	行政院國家科學委員會	zh_TW
dc.language.iso	zh_TW	en_US
dc.subject	可變結構系統理論	zh_TW
dc.subject	飛彈	zh_TW
dc.subject	導引律	zh_TW
dc.subject	軌跡	zh_TW
dc.subject	Variable structure system theory	en_US
dc.subject	Missile	en_US
dc.subject	Guidance law	en_US
dc.subject	Trajectory	en_US
dc.title	可變結構系統理論在飛彈導引律設計上之應用	zh_TW
dc.title	Variable Structure System Theory Applied to the Design of Guidance Laws for Missile	en_US
dc.type	Plan	en_US
dc.contributor.department	交通大學電機與控制工程系	zh_TW
顯示於類別：	研究計畫