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|Title:||Decoupling Orbital and Attitude Control of Communications Technology Satellite|
|Authors:||Yau, Yiu Joe|
|Keywords:||Electrical and Electronics;Electrical and Electronics|
|Abstract:||<p>Based on Altman's model, a state model and a measurement model are obtained. Both models are linearized and the linear state variable feedback method is then applied to decouple the linearized system.</p> <p>Computer programmes for decoupling are written and the results are then discussed.</p> <p>Suggestions for future work are proposed.</p>|
|Appears in Collections:||Open Access Dissertations and Theses|
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