Analysis and Design of Control Systems for Aircraft and Missiles

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DC Field	Value	Language
dc.contributor.author	韓光渭	zh_TW
dc.contributor.author	K. W. Han	en_US
dc.date.accessioned	2017-10-06T06:17:37Z	-
dc.date.available	2017-10-06T06:17:37Z	-
dc.date.issued	1966-04	en_US
dc.identifier.uri	http://hdl.handle.net/11536/137437	-
dc.description.abstract	In this paper, control systems for aircraft and missiles are analyzed and designed using a "stability curve" method which is particularily suitable for testing stability and adjusting parameters for complex control systems. Design procedures are given along with examples.	en_US
dc.language.iso	en_US	en_US
dc.publisher	交大學刊編輯委員會	zh_TW
dc.title	Analysis and Design of Control Systems for Aircraft and Missiles	en_US
dc.type	Campus Publications	en_US
dc.identifier.journal	交大學刊	zh_TW
dc.identifier.journal	science bulletin national chiao-tung university	en_US
dc.citation.volume	1	en_US
dc.citation.issue	2	en_US
dc.citation.spage	12	en_US
dc.citation.epage	28	en_US
Appears in Collections:	Science Bulletin National Chiao-Tung University

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