Design approach for Malfunction Detection System (MDS) to be used on board manned spacecraft; design is directed toward orbiting laboratory type vehicles, in which man will be subjected to hostile environments for extended periods of time; prime purpose of MDS will be to monitor and evaluate critical signals and display out-of-tolerance conditions; mathematical model approach to monitoring-system design; feasibility of using some value less than specified tolerance as signal "test" limit; various design decisions and trade-offs involved in choosing monitoring subsystem configuration are discussed, and conclusion is that approach is feasible and could be expanded to include other capabilities.
Malfunction detection system for advanced spacecraft
IEEE -- Trans Aerospace Electronic Systems
IEEE Transactions on Aerospace and Electronic Systems ; AES-2 , n 1
1966
9 pages
Article (Journal)
English
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Malfunction Detection System for Advanced Spacecraft
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