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- W2348312384 abstract "It is a trend that the aircraft onboard machine electronic equipment is controlled and managed integrated. Based on distributed fault tolerant technique, high reliable bus technique of avionics and application technique of embedded real time operation system, a design and an implementation of a distributed fault tolerant computer system which can control and manage aircraft onboard machine electronic equipment integrated are presented. The work feature and structure of the system, the communication network, the redundancy management and the real time fault tolerant administer software is discussed." @default.
- W2348312384 created "2016-06-24" @default.
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- W2348312384 date "2001-01-01" @default.
- W2348312384 modified "2023-09-25" @default.
- W2348312384 title "Design of Distributed Fault-Tolerant System for UMS" @default.
- W2348312384 hasPublicationYear "2001" @default.
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