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Decoupling Orbital and Attitude Control of Communications Technology Satellite

<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> / Master of Engineering (ME)

Identiferoai:union.ndltd.org:mcmaster.ca/oai:macsphere.mcmaster.ca:11375/9151
Date04 1900
CreatorsYau, Yiu Joe
ContributorsSinha, N.K., Electrical Engineering
Source SetsMcMaster University
Detected LanguageEnglish
Typethesis

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