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
27.08.2013
6 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Safety enhanced digital flight control system
Emerald Group Publishing | 2009
|Safety enhanced digital flight control system
Online Contents | 2009
|