Goel, P. S. ; Agrawal, V. K. ; Krishnan, A. ; Upadhyaya, J. S. (1985) Auto reconfiguration of reaction wheels in IRS IEEE Transactions on Aerospace and Electronic Systems, AES-21 (1). 160 - 163. ISSN 0018-9251
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Official URL: http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumb...
Related URL: http://dx.doi.org/10.1109/TAES.1985.310550
Abstract
The Indian remote sensing satellite (IRS) employs four reaction wheels for attitude control. The fourth, a skew wheel, provides redundancy to the failure of any of the orthogonal wheels. To avoid attitude loss before the redundant skew wheel takes over due to failure of any of the orthogonal wheels, an automatic reconfiguration scheme has been developed and implemented through a microprocessor. The details of reconfiguration logic and the computer simulation results are presented.
| Item Type: | Article |
|---|---|
| Source: | Copyright of this article belongs to Institute of Electrical and Electronic Engineers. |
| ID Code: | 13109 |
| Deposited On: | 11 Nov 2010 06:52 |
| Last Modified: | 02 Jun 2011 08:27 |
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