Spacecraft attitude control via mixed H2/H method

碩士 === 國立交通大學 === 電機與控制工程學系 === 86 === This thesis investigates the attitude control design problem of spacecraft systems considering external disturbances based on the linear , , and mixed / approach. It has been shown by Limebeer [33]...

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Bibliographic Details
Main Authors:	Wu, Yuan Long, 吳元龍
Other Authors:	Yung-Chun Wu
Format:	Others
Language:	zh-TW
Published:	1998
Online Access:	http://ndltd.ncl.edu.tw/handle/71716477433372698115

id	ndltd-TW-086NCTU0591054
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spelling	ndltd-TW-086NCTU05910542015-10-13T11:06:15Z http://ndltd.ncl.edu.tw/handle/71716477433372698115 Spacecraft attitude control via mixed H2/H method 以混合H2/H的方法做衛星姿態控制 Wu, Yuan Long 吳元龍碩士國立交通大學電機與控制工程學系 86 This thesis investigates the attitude control design problem of spacecraft systems considering external disturbances based on the linear , , and mixed / approach. It has been shown by Limebeer [33] that these problems are special cases of the so- called two-player Nash differential game problem. The resulting controller is a constant state-feedback law, characterized by the solution to a pair of cross-coupled Riccati equations, which can be solved by using a numerical integration procedure. The design ob Yung-Chun Wu 吳永春 1998 學位論文 ; thesis 2 zh-TW
collection	NDLTD
language	zh-TW
format	Others
sources	NDLTD
description	碩士 === 國立交通大學 === 電機與控制工程學系 === 86 === This thesis investigates the attitude control design problem of spacecraft systems considering external disturbances based on the linear , , and mixed / approach. It has been shown by Limebeer [33] that these problems are special cases of the so- called two-player Nash differential game problem. The resulting controller is a constant state-feedback law, characterized by the solution to a pair of cross-coupled Riccati equations, which can be solved by using a numerical integration procedure. The design ob
author2	Yung-Chun Wu
author_facet	Yung-Chun Wu Wu, Yuan Long 吳元龍
author	Wu, Yuan Long 吳元龍
spellingShingle	Wu, Yuan Long 吳元龍 Spacecraft attitude control via mixed H2/H method
author_sort	Wu, Yuan Long
title	Spacecraft attitude control via mixed H2/H method
title_short	Spacecraft attitude control via mixed H2/H method
title_full	Spacecraft attitude control via mixed H2/H method
title_fullStr	Spacecraft attitude control via mixed H2/H method
title_full_unstemmed	Spacecraft attitude control via mixed H2/H method
title_sort	spacecraft attitude control via mixed h2/h method
publishDate	1998
url	http://ndltd.ncl.edu.tw/handle/71716477433372698115
work_keys_str_mv	AT wuyuanlong spacecraftattitudecontrolviamixedh2hmethod AT wúyuánlóng spacecraftattitudecontrolviamixedh2hmethod AT wuyuanlong yǐhùnhéh2hdefāngfǎzuòwèixīngzītàikòngzhì AT wúyuánlóng yǐhùnhéh2hdefāngfǎzuòwèixīngzītàikòngzhì
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Spacecraft attitude control via mixed H2/H method

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