A mathematical model describing the dynamics of a self-contained flight control actuator is established. Typical failures of the actuator are defined in the space of the model parameters in the form of a failure pattern library. A diagnostic model of the actuator, intentionally sensitive to particular failures, is defined. A diagnostic procedure, featuring on-line parameter estimation of the diagnostic model, failure detection, and isolation, is proposed. A failure prediction procedure, utilizing trends exhibited by parameter estimates, is formulated. The results are verified by computer simulation.<>
On-line diagnostics of a self-contained flight actuator
IEEE Transactions on Aerospace and Electronic Systems ; 30 , 1 ; 186-196
01.01.1994
730701 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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