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http://hdl.handle.net/11375/9151
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.advisor | Sinha, N.K. | en_US |
dc.contributor.author | Yau, Yiu Joe | en_US |
dc.date.accessioned | 2014-06-18T16:45:51Z | - |
dc.date.available | 2014-06-18T16:45:51Z | - |
dc.date.created | 2009-06-25 | en_US |
dc.date.issued | 1976-04 | en_US |
dc.identifier.other | opendissertations/430 | en_US |
dc.identifier.other | 1184 | en_US |
dc.identifier.other | 880911 | en_US |
dc.identifier.uri | http://hdl.handle.net/11375/9151 | - |
dc.description.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> | en_US |
dc.subject | Electrical and Electronics | en_US |
dc.subject | Electrical and Electronics | en_US |
dc.title | Decoupling Orbital and Attitude Control of Communications Technology Satellite | en_US |
dc.type | thesis | en_US |
dc.contributor.department | Electrical Engineering | en_US |
dc.description.degree | Master of Engineering (ME) | en_US |
Appears in Collections: | Open Access Dissertations and Theses |
Files in This Item:
File | Size | Format | |
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fulltext.pdf | 1.93 MB | Adobe PDF | View/Open |
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