Spacecraft Attitude Control: A Nonlinear Robust Control Approach

博士 === 國立成功大學 === 電機工程學系碩博士班 === 90 === In this dissertation, nonlinear control , mixed and LMI control design methods are proposed to solve large-angle robust attitude control and tracking of spacecraft. The robust attitude control problem is formulated as thruster control and wheels control wher...

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Bibliographic Details
Main Authors: Long-Life Show, 壽鶴年
Other Authors: Jyh-Ching Juang
Format: Others
Language:en_US
Published: 2002
Online Access:http://ndltd.ncl.edu.tw/handle/m8wwcm

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