Decoupling Orbital and Attitude Control of Communications Technology Satellite
| dc.contributor.advisor | Sinha, N.K. | en_US |
| dc.contributor.author | Yau, Yiu Joe | en_US |
| dc.contributor.department | Electrical Engineering | 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.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.description.degree | Master of Engineering (ME) | 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.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 |
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