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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spelling ndltd-TW-076NCTU23270152015-10-13T11:08:30Z http://ndltd.ncl.edu.tw/handle/70232108609551980911 Attitude controller design of an aircraft using Q-parametization method 使用Q參數化方法之飛機姿態控制器設計 ZHANG, ZHENG-LIN 章正麟 碩士 國立交通大學 控制工程研究所 76 LIN, GING-AN 林清安 1988 學位論文 ; thesis 94 zh-TW
collection NDLTD
language zh-TW
format Others
sources NDLTD
description 碩士 === 國立交通大學 === 控制工程研究所 === 76 ===
author2 LIN, GING-AN
author_facet LIN, GING-AN
ZHANG, ZHENG-LIN
章正麟
author ZHANG, ZHENG-LIN
章正麟
spellingShingle ZHANG, ZHENG-LIN
章正麟
Attitude controller design of an aircraft using Q-parametization method
author_sort ZHANG, ZHENG-LIN
title Attitude controller design of an aircraft using Q-parametization method
title_short Attitude controller design of an aircraft using Q-parametization method
title_full Attitude controller design of an aircraft using Q-parametization method
title_fullStr Attitude controller design of an aircraft using Q-parametization method
title_full_unstemmed Attitude controller design of an aircraft using Q-parametization method
title_sort attitude controller design of an aircraft using q-parametization method
publishDate 1988
url http://ndltd.ncl.edu.tw/handle/70232108609551980911
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AT zhāngzhènglín attitudecontrollerdesignofanaircraftusingqparametizationmethod
AT zhangzhenglin shǐyòngqcānshùhuàfāngfǎzhīfēijīzītàikòngzhìqìshèjì
AT zhāngzhènglín shǐyòngqcānshùhuàfāngfǎzhīfēijīzītàikòngzhìqìshèjì
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