Finite Element Software Development of a Flexible Satellite Orbiting in Space
A computer code to simulate dynamics of flexible satellites orbiting the earth is developed. As the particular model, the satellite consisting of a rigid main body and two symmetrical flexible solar panels is observed. The motion of the solar panels is discretized by using finite element method. For...
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| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
2009
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| Online Access: | http://scholars.utp.edu.my/id/eprint/1089/ http://scholars.utp.edu.my/id/eprint/1089/1/75-59916-review.pdf |
| _version_ | 1848659075739418624 |
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| author | Parman, Setyamartana |
| author_facet | Parman, Setyamartana |
| author_sort | Parman, Setyamartana |
| building | UTP Institutional Repository |
| collection | Online Access |
| description | A computer code to simulate dynamics of flexible satellites orbiting the earth is developed. As the particular model, the satellite consisting of a rigid main body and two symmetrical flexible solar panels is observed. The motion of the solar panels is discretized by using finite element method. For this purpose the solar panels are supposed as a number of rectangular plate elements. The natural frequencies are then studied in order to determine the important modes during its operation. |
| first_indexed | 2025-11-13T07:24:40Z |
| format | Conference or Workshop Item |
| id | oai:scholars.utp.edu.my:1089 |
| institution | Universiti Teknologi Petronas |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-13T07:24:40Z |
| publishDate | 2009 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | oai:scholars.utp.edu.my:10892017-01-19T08:25:14Z http://scholars.utp.edu.my/id/eprint/1089/ Finite Element Software Development of a Flexible Satellite Orbiting in Space Parman, Setyamartana TL Motor vehicles. Aeronautics. Astronautics A computer code to simulate dynamics of flexible satellites orbiting the earth is developed. As the particular model, the satellite consisting of a rigid main body and two symmetrical flexible solar panels is observed. The motion of the solar panels is discretized by using finite element method. For this purpose the solar panels are supposed as a number of rectangular plate elements. The natural frequencies are then studied in order to determine the important modes during its operation. 2009-10 Conference or Workshop Item PeerReviewed application/pdf en http://scholars.utp.edu.my/id/eprint/1089/1/75-59916-review.pdf Parman, Setyamartana (2009) Finite Element Software Development of a Flexible Satellite Orbiting in Space. In: International Conference on APPLICATIONS AND DESIGN IN MECHANICAL ENGINEERING (ICADME) 2009, 11-13 October 2009, Batu Feringhi, Pulau Pinang. |
| spellingShingle | TL Motor vehicles. Aeronautics. Astronautics Parman, Setyamartana Finite Element Software Development of a Flexible Satellite Orbiting in Space |
| title | Finite Element Software Development of a Flexible
Satellite Orbiting in Space |
| title_full | Finite Element Software Development of a Flexible
Satellite Orbiting in Space |
| title_fullStr | Finite Element Software Development of a Flexible
Satellite Orbiting in Space |
| title_full_unstemmed | Finite Element Software Development of a Flexible
Satellite Orbiting in Space |
| title_short | Finite Element Software Development of a Flexible
Satellite Orbiting in Space |
| title_sort | finite element software development of a flexible
satellite orbiting in space |
| topic | TL Motor vehicles. Aeronautics. Astronautics |
| url | http://scholars.utp.edu.my/id/eprint/1089/ http://scholars.utp.edu.my/id/eprint/1089/1/75-59916-review.pdf |