Citation:
Aranda, L.A., Reviriego, P. y Maestro J. A. (2020). Toward a Fault-Tolerant Star Tracker for Small Satellite Applications. IEEE Transactions on Aerospace and Electronic Systems, 56 (5), pp. 3421 - 3431.
Sponsor:
The authors would like to thank E. Palombo from ESA/ESTEC in Noordwijk, the Netherlands, for providing the star tracker images used in this paper.
Keywords:
Error detection and correction
,
Fault tolerance
,
Soft error
,
SRAM-based FPGA
,
Star tracker
Star trackers are autonomous, high-accuracy electronic systems used to determine the attitude of a spacecraft. In recent years, commercial-off-the-shelf (COTS)-based star trackers are growing in importance for low-cost and short-duration missions, but their faStar trackers are autonomous, high-accuracy electronic systems used to determine the attitude of a spacecraft. In recent years, commercial-off-the-shelf (COTS)-based star trackers are growing in importance for low-cost and short-duration missions, but their fault tolerance against soft errors has not been studied in detail. In this paper, we propose a self-healing system protected with ad hoc techniques that can be used as the first step to implement a fault-tolerant COTS-based star tracker for smallsat applications.[+][-]