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Control moment gyro actuator for small satellite applications
Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005.
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| Other Authors: | |
| Format: | Thesis |
| Language: | English |
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Stellenbosch : University of Stellenbosch
2006
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| _version_ | 1867613837353549824 |
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| access_status_str | Open Access |
| author | Berner, Reimer |
| author2 | Steyn, W. H. |
| author_browse | Berner, Reimer Steyn, W. H. |
| author_facet | Steyn, W. H. Berner, Reimer |
| author_sort | Berner, Reimer |
| collection | Thesis |
| dc_rights_str_mv | University of Stellenbosch |
| description | Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005. |
| format | Thesis |
| id | oai:scholar.sun.ac.za:10019.1/2144 |
| institution | Stellenbosch University (South Africa) |
| language | English |
| last_indexed | 2026-06-10T12:42:28.529Z |
| license_str | Other — see source repository |
| provenance_str_mv | Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository |
| publishDate | 2006 |
| publishDateRange | 2006 |
| publishDateSort | 2006 |
| publisher | Stellenbosch : University of Stellenbosch |
| publisherStr | Stellenbosch : University of Stellenbosch |
| record_format | dspace |
| source_str | SUNScholar — Stellenbosch University Repository |
| spelling | oai:scholar.sun.ac.za:10019.1/2144 Control moment gyro actuator for small satellite applications Berner, Reimer Steyn, W. H. University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering. Actuators Artificial satellites -- Automatic control Artificial satellites -- Control systems Dissertations -- Electronic engineering Theses -- Electronic engineering Electrical and Electronic Engineering Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005. The aim of the thesis is to design a Control Moment Gyro (CMG) actuator which can be used in small satellite applications. The hardware and software of the CMG has to be designed according to specifications given. A satellite fitted with these CMGs has to be able to do a 30 degree rotation within 10 seconds. 2006-11-01T06:00:00Z 2010-06-01T08:41:24Z 2006-11-01T06:00:00Z 2010-06-01T08:41:24Z 2005-03 Thesis http://hdl.handle.net/10019.1/2144 en University of Stellenbosch 2558800 bytes application/pdf application/pdf Stellenbosch : University of Stellenbosch |
| spellingShingle | Actuators Artificial satellites -- Automatic control Artificial satellites -- Control systems Dissertations -- Electronic engineering Theses -- Electronic engineering Electrical and Electronic Engineering Berner, Reimer Control moment gyro actuator for small satellite applications |
| title | Control moment gyro actuator for small satellite applications |
| title_full | Control moment gyro actuator for small satellite applications |
| title_fullStr | Control moment gyro actuator for small satellite applications |
| title_full_unstemmed | Control moment gyro actuator for small satellite applications |
| title_short | Control moment gyro actuator for small satellite applications |
| title_sort | control moment gyro actuator for small satellite applications |
| topic | Actuators Artificial satellites -- Automatic control Artificial satellites -- Control systems Dissertations -- Electronic engineering Theses -- Electronic engineering Electrical and Electronic Engineering |
| url | http://hdl.handle.net/10019.1/2144 |
| work_keys_str_mv | AT bernerreimer controlmomentgyroactuatorforsmallsatelliteapplications |