The integrated application of reliability, failure effects and system simulator methods in establishing the airworthiness of a flight critical digital flight control system (DFCS) is demonstrated. The emphasis was on the mutual reinforcement of the methods in demonstrating the system safety.
Integrated Assurance Assessment of a Reconfigurable Digital Flight Control System
1983
125 pages
Report
No indication
English
Online Contents | 2005
|SAGE Publications | 2005
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