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Fault-Tolerant Avionics
| Content Provider | Scilit |
|---|---|
| Author | Spitzer, Cary R. |
| Copyright Year | 2000 |
| Description | Fault-tolerant designs are required to ensure safe operation of digital avionics systems performing flight-critical functions. This chapter discusses the motivation for fault-tolerant designs, and the many different design practices that are evolving to implement a fault-tolerant system. The designer needs to make sure the fault tolerance requirements are fully defined to select the design concept to be implemented from the alternatives available. The requirements for a fault-tolerant system include performance, dependability, and the methods of assuring that the design, when implemented, meets all requirements. The requirements must be documented in a specification of the intended behavior of a system, specifying the tolerances imposed on the various outputs from the system [Anderson and Lee, 1981]. Book Name: Digital Avionics Handbook |
| Related Links | https://content.taylorfrancis.com/books/download?dac=C2009-0-16104-7&isbn=9780429124853&doi=10.1201/9781420036879-37&format=pdf |
| Ending Page | 504 |
| Page Count | 24 |
| Starting Page | 481 |
| DOI | 10.1201/9781420036879-37 |
| Language | English |
| Publisher | Informa UK Limited |
| Publisher Date | 2000-12-20 |
| Access Restriction | Open |
| Subject Keyword | Book Name: Digital Avionics Handbook Hardware and Architecturee Requirements Fault Tolerant |
| Content Type | Text |
| Resource Type | Chapter |
