Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data
Small satellite builders frequently encounter many different types of problems in testing different satellite subsystems at ground based laboratories. Full-scale testing can only be performed in orbit with actual flight systems, where critical errors sometimes cannot be resolved. Unlike huge budget...
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| Format: | Monograph |
| Language: | English |
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s.n
2012
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| Online Access: | http://irep.iium.edu.my/33698/1/EDW_A_11-193-0984.pdf |
| _version_ | 1796878428577726464 |
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| author | Abdelrahman, Mohammad |
| author_facet | Abdelrahman, Mohammad |
| author_sort | Abdelrahman, Mohammad |
| collection | IIUM |
| description | Small satellite builders frequently encounter many different types of problems in testing different satellite subsystems at ground based laboratories. Full-scale testing can only be performed in orbit with actual flight systems, where critical errors sometimes cannot be resolved. Unlike huge budget missions, small satellite programs are supposed to have severe limitation in time, financial, and manpower resources. The future target of the project is to design, build, and test the mission software programs for spacecraft systems i.e., the ground control station computer and the on board computer. |
| first_indexed | 2024-03-05T23:21:20Z |
| format | Monograph |
| id | oai:generic.eprints.org:33698 |
| institution | International Islamic University Malaysia |
| language | English |
| last_indexed | 2024-03-05T23:21:20Z |
| publishDate | 2012 |
| publisher | s.n |
| record_format | dspace |
| spelling | oai:generic.eprints.org:336982014-01-22T00:28:07Z http://irep.iium.edu.my/33698/ Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data Abdelrahman, Mohammad TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General) Small satellite builders frequently encounter many different types of problems in testing different satellite subsystems at ground based laboratories. Full-scale testing can only be performed in orbit with actual flight systems, where critical errors sometimes cannot be resolved. Unlike huge budget missions, small satellite programs are supposed to have severe limitation in time, financial, and manpower resources. The future target of the project is to design, build, and test the mission software programs for spacecraft systems i.e., the ground control station computer and the on board computer. s.n 2012-10-31 Monograph NonPeerReviewed application/pdf en http://irep.iium.edu.my/33698/1/EDW_A_11-193-0984.pdf Abdelrahman, Mohammad (2012) Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data. Research Report. s.n. (Unpublished) EDW A11-193-0984 |
| spellingShingle | TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General) Abdelrahman, Mohammad Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data |
| title | Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data |
| title_full | Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data |
| title_fullStr | Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data |
| title_full_unstemmed | Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data |
| title_short | Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data |
| title_sort | development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data |
| topic | TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General) |
| url | http://irep.iium.edu.my/33698/1/EDW_A_11-193-0984.pdf |
| work_keys_str_mv | AT abdelrahmanmohammad developmentofathreedimensionalvisualizationtoolforspacecraftattitudeandorbitaldynamicsusingtelemetrydata |