Title :
Auto Reconfiguration of Reaction Wheels in IRS
Author :
Goel, P.S. ; Agrawal, V.K. ; Krishnan, A. ; Upadhyaya, J.S.
Author_Institution :
Indian Space and Research Organization Satellite Centre Airport Road Bangalore-560 017 India
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.
Keywords :
Computer errors; Computer simulation; Ground support; Microprocessors; Payloads; Redundancy; Remote sensing; Satellite ground stations; Space vehicles; Wheels;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.1985.310550