Abstract
The electromechanical actuator (EMA) model is presented with the methods for identifying its design parameters. The actuator is part of the system for flap deployment on the commercial transport airplane. The differential equations with the feedback control describe behaviour of the actuator deflection. For parameter identification the Maximum Likelihood (ML) method with two minimization algorithms: linearized Gauss-Newton and Levenberg-Marquardt is applied. Both approaches were effective, while tested on hypothetical data.
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© 2011 Springer-Verlag Berlin Heidelberg
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Ulinowicz, M., Narkiewicz, J. (2011). Identification of EMA Dynamic Model. In: Jabloński, R., Březina, T. (eds) Mechatronics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-23244-2_46
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DOI: https://doi.org/10.1007/978-3-642-23244-2_46
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-23243-5
Online ISBN: 978-3-642-23244-2
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