Abstract
In this paper, fault-tolerant active control of the rotational motion of the satellite has been applied. Satellite mathematical models are introduced, and the nontraditional Kalman filter is designed with the presented control algorithms. Re-adjustment control procedure has been established taking into account the identified control distribution matrix. If there are three-axis reaction wheels on the satellite, the failure of one actuator, control setting is carried out using control distribution matrix diagnostics. Extended Kalman Filter has been introduced to control the distribution estimation of matrix elements, so check back adjustment rule is applied by the fault tolerant attitude control.
| Original language | English |
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| Title of host publication | Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017 |
| Editors | M.F. Unal, A. Hacioglu, M.S. Yildiz, O. Altan, M. Yorukoglu |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 349-353 |
| Number of pages | 5 |
| ISBN (Electronic) | 9781538616031 |
| DOIs | |
| Publication status | Published - 4 Aug 2017 |
| Event | 8th International Conference on Recent Advances in Space Technologies, RAST 2017 - Istanbul, Turkey Duration: 19 Jun 2017 → 22 Jun 2017 |
Publication series
| Name | Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017 |
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Conference
| Conference | 8th International Conference on Recent Advances in Space Technologies, RAST 2017 |
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| Country/Territory | Turkey |
| City | Istanbul |
| Period | 19/06/17 → 22/06/17 |
Bibliographical note
Publisher Copyright:© 2017 IEEE.
Keywords
- attitude
- estimation
- fault tolerant control
- nanosatellite
- reconfigurable control