Model-free sliding-mode controller for soft landing of reluctance actuators
Resumen: Some electromagnetic actuators suffer from high velocity impacts during non-controlled switching operations, which cause contact bouncing, mechanical wear, and acoustic noise. Soft-landing control strategies aim at minimizing the impact velocities of these devices to improve their performance. This paper presents a sliding-mode controller for soft landing of single-coil reluctance actuators. It is a switching model-free controller, which results in a very simple implementation. A generalized dynamical hybrid model of an actuator is utilized for deriving the robustness condition, based on the Lyapunov theory. Then, the condition is evaluated for a dynamical model, based on a commercial device, and several reference trajectories. Finally, the controller performance is validated through simulations. The effect of the sampling rate on the resulting impact velocities is also analyzed.
Idioma: Inglés
DOI: 10.1016/j.ifacol.2020.12.1738
Año: 2021
Publicado en: IFAC PAPERSONLINE 53, 2 (2021), 6256-6261
ISSN: 2405-8963

Factor impacto SCIMAGO: 0.324 - Control and Systems Engineering (Q3)

Financiación: info:eu-repo/grantAgreement/ES/DGA-FEDER/2014-2020
Financiación: info:eu-repo/grantAgreement/ES/DGA/T45-17R
Financiación: info:eu-repo/grantAgreement/ES/MCIU-AEI-FEDER/PGC2018-098719-B-I00
Financiación: info:eu-repo/grantAgreement/ES/MEC/FPU14-04171
Financiación: info:eu-repo/grantAgreement/ES/MICINN-AEI-FEDER/RTC-2017-5965-6
Tipo y forma: Congress (Published version)
Área (Departamento): Área Ingen.Sistemas y Automát. (Dpto. Informát.Ingenie.Sistms.)
Exportado de SIDERAL (2024-01-04-11:07:06)


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 Notice créée le 2021-08-20, modifiée le 2024-01-04


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