標題: Analysis and Design of Control Systems for Aircraft and Missiles
作者: 韓光渭
K. W. Han
公開日期: 四月-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
顯示於類別:交大學刊


文件中的檔案:

  1. HT001295-02.pdf