Attitude controller design of an aircraft using Q-parametization method

Attitude controller design of an aircraft using Q-parametization method

碩士 === 國立交通大學 === 控制工程研究所 === 76 ===

Bibliographic Details
Main Authors:	ZHANG, ZHENG-LIN, 章正麟
Other Authors:	LIN, GING-AN
Format:	Others
Language:	zh-TW
Published:	1988
Online Access:	http://ndltd.ncl.edu.tw/handle/70232108609551980911

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