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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Bibliografski detalji
Glavni autor: Muhyi Yaakop (Autor)
Autor kompanije: Universiti Malaysia Perlis
Format: Disertacija Knjiga
Jezik:English
Izdano: Perlis, Malaysia School of Mechatronic Engineering 2011.
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Opis
Sažetak: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 phase nominal mode controller which uses an adaptive method to smooth the discontinuity is used to adapt the systems to inherent noise.
Opis:x, 166 pages illustrations 30 cm.
Bibliografija:Includes bibliographical references (pages 128-132).