PDF-Nonlinear Attitude Contro l for a Rigid Spacecraft by Feedback Linearization Hyochoong Bang J ngShin Lee unJu Eun Division of Aerospace Engineering KAIST Kuson Dong usongGu Daejon Abstract Att
Th e attitu on y ou tpu fu tio t erefore lead s a st cl ose l sy st em fol wi e gi ven re fe rence t aj ect or The p ci adva nt age of t op ed m th is t at it is
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