Experimental and theoretical study of the electrical failures in a fault-tolerant direct-drive servovalve for primary flight actuators

• Published in: Proceedings of the Institution of Mechanical Engineers. Part I, Journal of systems and control engineering Vol. 222; no. 8; pp. 757 - 769
• Main Authors: Di Rito, G, Galatolo, R
• Format: Journal Article
• Language: English
• Published: London, England SAGE Publications 01.12.2008; SAGE PUBLICATIONS, INC
• Subjects: Actuators; Aerospace engineering; Automobile industry; Circuits; Coiling; Coils; Computer based modeling; Computer simulation; Construction; Control systems; Degradation; Dynamical systems; Electric wire; Electricity; Failure; Failure analysis; Fault tolerance; Fly by wire control; Hydraulics; Mechanical engineering; Servomotors; Short circuits; System dynamics; modelling and simulation; direct-drive servovalve; fault-tolerant actuators; failure analysis; flight control; testing
• ISSN: 0959-6518; 2041-3041
• DOI: 10.1243/09596518JSCE588

The current paper deals with the study of the electrical failures in fault-tolerant flight actuators, with particular reference to the short circuits of the servovalve coils. A high-fidelity model of the servovalve of a modern fly-by-wire actuator is developed and validated through experiments, focusing attention on the characterization of the component dynamics in case of partial and total short circuits of the direct-drive motor coils. The servovalve model is then used to simulate a typical on-ground built-in-test procedure to determine the limit condition for the detection of a partial short circuit. Finally, once different possible combinations of short circuits are injected, the degradation of performances of the whole actuator is characterized through experiments, and the servovalve model is used to justify the test results, highlighting and discussing the effects of the failures on the system dynamics.