Conference article

Modelling and simulation of a fault-tolerant electrical motor for aerospace servovalves with Modelica

Gianpietro Di Rito
Dipartimento di Ingegneria Aerospaziale - Università di Pisa, Italy

Roberto Galatolo
Dipartimento di Ingegneria Aerospaziale - Università di Pisa, Italy

Download articlehttp://dx.doi.org/10.3384/ecp09430091

Published in: Proceedings of the 7th International Modelica Conference; Como; Italy; 20-22 September 2009

Linköping Electronic Conference Proceedings 43:17, p. 160-167

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Published: 2009-12-29

ISBN: 978-91-7393-513-5

ISSN: 1650-3686 (print), 1650-3740 (online)

Abstract

The paper deals with the design and the simulation of electro-magnetic actuators via object-oriented modelling. The study is carried out in the Modelica-Dymola environment; and focuses on the quadruple-coil direct-drive motor of a modern fly-by-wire servovalve. Starting from basic information about material properties and from a schematic representation of the system geometry; the motor model is created mainly using the components of the Modelica_Magnetic library. The motor performances are then characterised with reference to both the normal operating condition (four active coils) and the worst-case fault-tolerant condition (only two active coils); in terms of current-to-force and current-to-displacement curves. The Modelica model is finally validated by comparing the simulation results with experimental data obtained during previous research activities. The Modelica results are also compared with those provided by a Matlab-Simulink model of the motor; pointing out the advantages of the object-oriented approach for the study of complex electro-magnetic systems. The easy modelling of magnetic circuit networks and the inherent simulation of magnetic material properties allow to achieve accurate results very efficiently; taking into account physical phenomena that are often disregarded during preliminary design phases; such as magnetic saturation or magnetic flux dispersions.

Keywords

Fault-tolerant aircraft systems; electromagnetic actuators; object-oriented modelling

References

[1] Pratt R. W.; “Flight control systems: practical issues in design and implementation”; Institution of Engineering and Technology; Stevenage; 2000. doi: 10.1049/PBCE057E.

[2] Miller F. G.; “Direct drive control valves and their applications”; Proceedings of the IMechE International Conference on Aerospace Hydraulics and Systems; London (UK); 1993; pp. 1–16.

[3] Elmqvist H.; Mattsson S. E.; and Otter M.; “Modelica - the new object-oriented modeling language”; 12th European Simulation Multiconference (ESM’98); Manchester (UK); pp. 1-5; 1998.

[4] Otter M.; and Elmqvist H.; “Modelica: language; libraries; tools; workshop and EU-project RealSim”; Simulation News Europe; pp. 3-8; 2000.

[5] Bodrich T.; Roschke T.; “A magnetic library for Modelica”; Proceedings of the 4th International Modelica Conference; Hamburg (Germany); Vol. 2; pp. 559-565; 2005.

[6] Di Rito G.; and Galatolo R.; “Experimental and theoretical study of the electrical failures in a fault-tolerant direct-drive servovalve for primary flight actuators”; Proceedings of the Institution of Mechanical Engineers; Part I; Journal of Systems and Control Engineering; v. 222; no. I8; 2008; pp. 757-769. doi: 10.1243/09596518JSCE588.

[7] Di Rito G.; “Experimental validation of theoretical and numerical models of a DDV linear force motor”; Proceedings of the 3rd FPNI-PhD Symposium; 2004; pp. 105–114.

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