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Title: Analytical redundancy scheme for improving reliability of automatic flight control systems for aircraft
Author: Alkhatib, K. Y.
ISNI:       0000 0001 3414 6831
Awarding Body: Loughborough University of Technology
Current Institution: Loughborough University
Date of Award: 1985
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Any redundancy scheme in aircraft control systems is usually considered separately from the control algorithms involved. All feedback control systems are usually designed under the assumption that their sensors will not fail. When the integrity requirements demand it, then a redundancy scheme must be designed to provide any required measurements with only extremely short interruptions to normal service being caused by failures of individual sensors.
Supervisor: Not available Sponsor: Not available
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID:  DOI: Not available
Keywords: Aircraft flight control & aircraft instrumentation