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Thesis (M. Ing.) -- University of Stellenbosch, 1994.
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| Other Authors: | |
| Format: | Thesis |
| Language: | English |
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Stellenbosch : Stellenbosch University
2012
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| _version_ | 1867613941154185216 |
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| access_status_str | Open Access |
| author | De Swardt, Ian |
| author2 | Bakkes, P. J. |
| author_browse | Bakkes, P. J. De Swardt, Ian |
| author_facet | Bakkes, P. J. De Swardt, Ian |
| author_sort | De Swardt, Ian |
| collection | Thesis |
| dc_rights_str_mv | Stellenbosch University |
| description | Thesis (M. Ing.) -- University of Stellenbosch, 1994. |
| format | Thesis |
| id | oai:scholar.sun.ac.za:10019.1/58284 |
| institution | Stellenbosch University (South Africa) |
| language | English |
| last_indexed | 2026-06-10T12:44:08.546Z |
| license_str | Other — see source repository |
| provenance_str_mv | Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository |
| publishDate | 2012 |
| publishDateRange | 2012 |
| publishDateSort | 2012 |
| publisher | Stellenbosch : Stellenbosch University |
| publisherStr | Stellenbosch : Stellenbosch University |
| record_format | dspace |
| source_str | SUNScholar — Stellenbosch University Repository |
| spelling | oai:scholar.sun.ac.za:10019.1/58284 A telemetry system for SUNSAT De Swardt, Ian Bakkes, P. J. Stellenbosch University. Faculty of Engineering. Dept. of Electrical & Electronic Engineering. Artificial satellites Aerospace telemetry Telemeter Dissertations -- Electronic engineering Thesis (M. Ing.) -- University of Stellenbosch, 1994. SUNSAT will require a reliable telematry system which will enable the Ground Control Station to establish the status of the satellite under all operational conditions. Flexibility is required to adapt the telemetry system to the different needs and situations which may arise during the satellite's mission. Existing microsatellite telemetry systems were evaluated and a conceptual design was developed from the evaluation. A prototype model was developed and from the experienced gained, another conceptual design was developed. This led to the design and implementation of an engineering model of the hardware. The result is a telemetry system which was developed with reliability and flexibility as the two main design guidelines. Some of the main features of the engineering model is the decentralized implementation and the use of multiple on board processors which can collect the telemetry data. The system implements a hardware based telemetry function which is not dependant on any of the on board processors to transmit the telemetry data. Masters 2012-08-27T11:38:53Z 2012-08-27T11:38:53Z 1994 Thesis http://hdl.handle.net/10019.1/58284 en Stellenbosch University 144 pages : ill. application/pdf Stellenbosch : Stellenbosch University |
| spellingShingle | Artificial satellites Aerospace telemetry Telemeter Dissertations -- Electronic engineering De Swardt, Ian A telemetry system for SUNSAT |
| title | A telemetry system for SUNSAT |
| title_full | A telemetry system for SUNSAT |
| title_fullStr | A telemetry system for SUNSAT |
| title_full_unstemmed | A telemetry system for SUNSAT |
| title_short | A telemetry system for SUNSAT |
| title_sort | telemetry system for sunsat |
| topic | Artificial satellites Aerospace telemetry Telemeter Dissertations -- Electronic engineering |
| url | http://hdl.handle.net/10019.1/58284 |
| work_keys_str_mv | AT deswardtian atelemetrysystemforsunsat AT deswardtian telemetrysystemforsunsat |