This lecture series is intended to cover experience with flight tested fly-by-wire systems as well as issues in redundancy management of synchronous and asynchronous approaches. It will specifically address the individual aspects of software fault tolerance, actuation fault tolerance, reliable data communication, and multi-computer operation using the ADA language. Partial contents: Digital Fly-by-wire Experience; Redundancy Management of Synchronous and Asynchronous Systems; Software Fault Tolerance Experiments; Can Design Faults Be Tolerated; Dependable Avionic Data Transmission; Multi-Computer Fault Tolerant Systems Using ADA; Design Issues in Data Synchronous Systems; Digital Fault-Tolerant Flight Actuation Systems; Design Validation of Fly-by-wire Flight Control Systems.
Fault Tolerant Hardware/Software Architecture for Flight Critical Function
1985
160 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Computer architecture , Fly by wire control , Fault tolerant computing , Digital computers , Actuation , Avionics , Data transmission systems , Computer programs , Flight , Functions , Reliability , Validation , Asynchronous systems , Information systems , Management , Redundancy , Foreign technology , NATO furnished
Analysis of a Hardware and Software Fault Tolerant Processor for Critical Applications
British Library Conference Proceedings | 1993
|Fault-Tolerant Software For Flight Control
NTRS | 1988
|