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http://hdl.handle.net/11375/9151| Title: | Decoupling Orbital and Attitude Control of Communications Technology Satellite |
| Authors: | Yau, Yiu Joe |
| Advisor: | Sinha, N.K. |
| Department: | Electrical Engineering |
| Keywords: | Electrical and Electronics;Electrical and Electronics |
| Publication Date: | Apr-1976 |
| 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> |
| URI: | http://hdl.handle.net/11375/9151 |
| Identifier: | opendissertations/430 1184 880911 |
| Appears in Collections: | Open Access Dissertations and Theses |
Files in This Item:
| File | Size | Format | |
|---|---|---|---|
| fulltext.pdf | 1.93 MB | Adobe PDF | View/Open |
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