Satellite attitude performance during the momentum dumping mode.
In this paper, the active magnetic control technique is applied for controlling the attitude and nutation of roll/yaw ares as well as unloading the excess wheel angular momentum for a small biased-momentum satellite in a nominal operation. Two control structures are configured using 2 and 3 magnetic...
| Main Authors: | , |
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| Format: | Article |
| Language: | English English |
| Published: |
Praise Worthy Prize
2009
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| Online Access: | http://psasir.upm.edu.my/id/eprint/16620/ http://psasir.upm.edu.my/id/eprint/16620/1/Satellite%20attitude%20performance%20during%20the%20momentum%20dumping%20mode.pdf |
| _version_ | 1848843012265738240 |
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| author | Mohd Suhadis, Nurulasikin Varatharajoo, Renuganth |
| author_facet | Mohd Suhadis, Nurulasikin Varatharajoo, Renuganth |
| author_sort | Mohd Suhadis, Nurulasikin |
| building | UPM Institutional Repository |
| collection | Online Access |
| description | In this paper, the active magnetic control technique is applied for controlling the attitude and nutation of roll/yaw ares as well as unloading the excess wheel angular momentum for a small biased-momentum satellite in a nominal operation. Two control structures are configured using 2 and 3 magnetic torquers. The proportional controller is used for the attitude and nutation control of roll/yaw ares while the proportional-integral controller is used for the wheel momentum unloading task Both systems are evaluated through numerical treatments and compared particularly during the momentum unloading process. The performance from simulations exhibits that both systems fulfill the mission requirements. However, the system that uses 3 magnetic lorquers gives a better attitude performance. |
| first_indexed | 2025-11-15T08:08:15Z |
| format | Article |
| id | upm-16620 |
| institution | Universiti Putra Malaysia |
| institution_category | Local University |
| language | English English |
| last_indexed | 2025-11-15T08:08:15Z |
| publishDate | 2009 |
| publisher | Praise Worthy Prize |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | upm-166202015-10-23T01:27:40Z http://psasir.upm.edu.my/id/eprint/16620/ Satellite attitude performance during the momentum dumping mode. Mohd Suhadis, Nurulasikin Varatharajoo, Renuganth In this paper, the active magnetic control technique is applied for controlling the attitude and nutation of roll/yaw ares as well as unloading the excess wheel angular momentum for a small biased-momentum satellite in a nominal operation. Two control structures are configured using 2 and 3 magnetic torquers. The proportional controller is used for the attitude and nutation control of roll/yaw ares while the proportional-integral controller is used for the wheel momentum unloading task Both systems are evaluated through numerical treatments and compared particularly during the momentum unloading process. The performance from simulations exhibits that both systems fulfill the mission requirements. However, the system that uses 3 magnetic lorquers gives a better attitude performance. Praise Worthy Prize 2009 Article PeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/16620/1/Satellite%20attitude%20performance%20during%20the%20momentum%20dumping%20mode.pdf Mohd Suhadis, Nurulasikin and Varatharajoo, Renuganth (2009) Satellite attitude performance during the momentum dumping mode. International Review of Aerospace Engineering, 2 (3). pp. 133-138. ISSN 1973 - 7459 English |
| spellingShingle | Mohd Suhadis, Nurulasikin Varatharajoo, Renuganth Satellite attitude performance during the momentum dumping mode. |
| title | Satellite attitude performance during the momentum dumping mode. |
| title_full | Satellite attitude performance during the momentum dumping mode. |
| title_fullStr | Satellite attitude performance during the momentum dumping mode. |
| title_full_unstemmed | Satellite attitude performance during the momentum dumping mode. |
| title_short | Satellite attitude performance during the momentum dumping mode. |
| title_sort | satellite attitude performance during the momentum dumping mode. |
| url | http://psasir.upm.edu.my/id/eprint/16620/ http://psasir.upm.edu.my/id/eprint/16620/1/Satellite%20attitude%20performance%20during%20the%20momentum%20dumping%20mode.pdf |