Analysis and Design of Control Systems for Aircraft and Missiles

Title:	Analysis and Design of Control Systems for Aircraft and Missiles
Authors:	韓光渭 K. W. Han
Issue Date:	Apr-1966
Publisher:	交大學刊編輯委員會
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.
URI:	http://hdl.handle.net/11536/137437
Journal:	交大學刊 science bulletin national chiao-tung university
Volume:	1
Issue:	2
Begin Page:	12
End Page:	28
Appears in Collections:	Science Bulletin National Chiao-Tung University

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