Development of an attitude control system for InnoSAT satellite /

The purpose of this work was to develop control scheme for one, two and three axis stabilization of a magnetic actuated satellite for InnoSAT. This was achieved by a combination of a two mode system theory. The de-tumbling mode by means of a passive 1st phase controller for quick response and 2nd ph...

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Bibliographic Details
Main Author: Muhyi Yaakop (Author)
Corporate Author: Universiti Malaysia Perlis
Format: Thesis Book
Language:English
Published: Perlis, Malaysia School of Mechatronic Engineering 2011.
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