Analysis and Design of Control Systems for Aircraft and Missiles

標題:	Analysis and Design of Control Systems for Aircraft and Missiles
作者:	韓光渭 K. W. Han
公開日期:	Apr-1966
出版社:	交大學刊編輯委員會
摘要:	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.
URI:	http://hdl.handle.net/11536/137437
期刊:	交大學刊 science bulletin national chiao-tung university
Volume:	1
Issue:	2
起始頁:	12
結束頁:	28
Appears in Collections:	Science Bulletin National Chiao-Tung University

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