@article {Bouras2020237,
	title = {A review of the most adopted fault tolerance approaches for sram based fpga real time critical embedded system},
	journal = {Journal of Advanced Research in Dynamical and Control Systems},
	volume = {12},
	number = {3 Special Issue},
	year = {2020},
	note = {cited By 0},
	pages = {237-241},
	abstract = {Since the downscaling in technology FPGAs became widely used in space embedded systems, due to their high computing capability, flexibility and easiness of implementation. Especially, SRAM-based FPGAs are now more adopted and implemented; as processing unit; in digital systems like the ADCS, in nanosatellite. However, this continuous downscaling made radiation-induced errors become a major concern. Particularly for SRAMs-based FPGAs, because they are more sensitive to radiations and more prone to soft errors. Regarding this matter, many approaches were developed and adopted in literature. Our objective is to optimize the reliability of the ADCS system, by improving the reliability of its SRAM based-FPGA. Therefore, in this paper we briefly describe the SRAM based FPGA configuration memory. Also, we present the different faults tolerance approaches proposed in the literature, and we evaluate these approaches by illuminating their advantages and disadvantages. {\textcopyright} 2020, Institute of Advanced Scientific Research, Inc.. All rights reserved.},
	doi = {10.5373/JARDCS/V12SP3/20201258},
	url = {https://www.scopus.com/inward/record.uri?eid=2-s2.0-85082941306\&doi=10.5373\%2fJARDCS\%2fV12SP3\%2f20201258\&partnerID=40\&md5=996763606f1d62a920796c21a385771b},
	author = {Bouras, M. and Berbia, H.}
}
@article {Bouras2016409,
	title = {On modeling and fault tolerance of nanosatellite attitude control system},
	journal = {Lecture Notes in Electrical Engineering},
	volume = {380},
	year = {2016},
	note = {cited By 0},
	pages = {409-417},
	abstract = {The modeling of a satellite system and its orientation in space is a difficult and important step to define before controlling its attitude. Many methods have been developed since the first satellite was built. In this paper we propose a comparative study of the most important attitude representation methods adopted in the literature. We point out the advantages and disadvantages of each of these methods before choosing the one that suits our objective. Then we present, the Simulink blocks for Rotation angles method, which will be used in our attitude model. After that, we will present the implementation of this model in a system on chip, following the proposed architecture. {\textcopyright} Springer International Publishing Switzerland 2016.},
	doi = {10.1007/978-3-319-30301-7_43},
	url = {https://www.scopus.com/inward/record.uri?eid=2-s2.0-84964467535\&doi=10.1007\%2f978-3-319-30301-7_43\&partnerID=40\&md5=dd44b013d3b2209a95e92773688e7175},
	author = {Bouras, M. and Berbia, H. and Nasser, T.}
}
