This example evaluates the catastrophic failure case of total loss of the pitch axis of a fly‐by‐wire flight control system. It is a much simplified analysis, but serves to illustrate the principles and differences between the dependency diagram approach and the fault tree approach.
Safety Analysis – Flight Control System
Civil Avionics Systems ; 533-538
2013-08-27
6 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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