A diagnosis scheme for senors of a flight control system is presented. A duplex sensor of configurations. Based on analytic redundancy, provides the fail-operational capability of a conventional triplex sensor system. This is achieved by using deterministic observers. The feasibilty of the presented concept is demonstrated by flight test results.
Diagnosis Scheme for Sensors of a Flight Control System Using Analytic Redundancy
1983
12 pages
Report
Keine Angabe
Englisch
Avionics , Aircraft , Flight control systems , Detectors , Jet transport aircraft , Failure , Diagnosis(General) , Closed loop systems , Control systems , Integrated systems , Symposia , Reliability , Fail safe , Redundancy , Feedback , Malfunctions , West Germany , Duplex sensors , Detectability , Redundancy management , Deterministic observers , NATO furnished , Component reports
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