作者: Martin W. Feintuch
DOI:
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摘要: A flight control computer system includes a plurality of computing channels (11 , 21 and 31 ) where each channel further main processor (113) monitor (114) under distinct operating systems. When the miscompare, cross-channel failure discretes (131 are transmitted to other local generic fault discrete is armed. armed (141 142) received from channels, program interrupt (133) issued causing execute minimal fully tested 'get home' software package (150).