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- W2091280491 abstract "General Dynamics/Convair is under NASA contract to integrate the Centaur upper stage into the space transportation system for future planetary missions. This requires that control of all safety critical functions be two-failure tolerant. The control system developed consists of five asynchronous computers, each contributing at their outputs to a 3-out-of-5 voting plane. Subsystem control is based on an end function redundancy management scheme. Analysis of multiple component failures and worst-case time-phase asynchrony among the computers is performed by a real-time computer simulation. The simulation emulates the hardware and subsystem interfaces, wire by wire, providing assessibility to any component for the insertion of preprogrammed failures. Observability is provided via a graphics system and diagnostic software. The simulation provides an engineering tool where the integrity of control system hardware and imbedded software can be demonstrated." @default.
- W2091280491 created "2016-06-24" @default.
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- W2091280491 date "1981-08-17" @default.
- W2091280491 modified "2023-10-16" @default.
- W2091280491 title "Design and verification of a multiple fault tolerant control system for STS applications using computer simulation" @default.
- W2091280491 doi "https://doi.org/10.2514/6.1981-2173" @default.
- W2091280491 hasPublicationYear "1981" @default.
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