Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/46907
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dc.contributor.authorLuo, Wenchengen
dc.date.accessioned2011-12-27T05:43:55Zen
dc.date.available2011-12-27T05:43:55Zen
dc.date.copyright2005en
dc.date.issued2005en
dc.identifier.citationLuo, W. (2005). Attitude control of microsatellite. Doctoral thesis, Nanyang Technological University, Singapore.en
dc.identifier.urihttps://hdl.handle.net/10356/46907en
dc.description176 p.en
dc.description.abstractIn this thesis, we study the robust optimal attitude control problem of microsatellites with disturbances and an uncertain inertia matrix. This is a nonlinear control problem. As the emphasis is on the development of state-feedback attitude controllers that achieve optimality as well as disturbance attenuation, a brief survey is made of the Lyapunov stability and the disturbance attenuation problems of nonlinear systems.en
dc.rightsNanyang Technological Universityen
dc.subjectDRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineeringen
dc.titleAttitude control of microsatelliteen
dc.typeThesisen
dc.contributor.supervisorChu Yun Chungen
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen
dc.description.degreeDOCTOR OF PHILOSOPHY (EEE)en
dc.identifier.doi10.32657/10356/46907en
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