For survival and achieving reliability in ultra long-life missions, fault tolerant design techniques need to handle the predominant failure mode, which is the wear-out of components. Conventional design methodologies will need excessive redundancy to achieve the required reliability. The objective of this paper is to present a new approach to design a more efficient fault-tolerant avionics system architecture that requires significantly fewer redundant components.
Ultra long-life avionics architecture
2002 Core Technologies for Space Systems Conference
2002-11-19
Conference paper
No indication
English
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