An antisaturating adaptive preaction and a slide surface to achieve soft landing control for electromagnetic actuators
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in: IEEE/ASME Transactions on Mechatronics, Jahrgang 17, Nr. 1, 5664793, 02.2012, S. 76-85.
Publikation: Beiträge in Zeitschriften › Zeitschriftenaufsätze › Forschung › begutachtet
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TY - JOUR
T1 - An antisaturating adaptive preaction and a slide surface to achieve soft landing control for electromagnetic actuators
AU - Mercorelli, P.
N1 - Export Date: 22 May 2012 Source: Scopus Art. No.: 5664793 CODEN: IATEF doi: 10.1109/TMECH.2010.2089467 Language of Original Document: English Correspondence Address: Mercorelli, P.; Faculty of Automotive Engineering, Ostfalia University of Applied Sciences, D-38440 Wolfsburg, Germany; email: p.mercorelli@ostfalia.de References: Aström, K.L., Rundqwist, L., Integrator windup and how to avoid it (1987) Presented at the Amer. Control Conf. (ACC), , Pittsburgh; Kothare, M.V., Campo, P.J., Morari, M., Nett, C.N., A unified framework for the study of anti-windup designs (1994) Automatica, 30 (12), pp. 1869-1883. , DOI 10.1016/0005-1098(94)90048-5; Butzmann, S., Melbert, J., Koch, A., Sensorless control of electromagnetic actuators for variable valve train (2000) Proc. Soc. Automotive Eng. (SAE), , http://www.sae.org/automag, Detroit, Tech. Paper 2000-01-1225. [Online]. 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Decision Control, pp. 3790-3795
PY - 2012/2
Y1 - 2012/2
N2 - Real-control applications of any nature can be affected by saturation limits that generate windup. When saturation occurs in a device its performance deteriorates. Electromagnetic actuators for industrial applications are being utilized ever more frequently for positioning and tracking control problems. One of the most important requirements in tracking trajectories is to achieve a soft landing, which guarantees reliable functionality and a longer component life. This paper presents an application of a typical electromagnetic actuator through a hardware-in-the-loop structure in which a soft landing is required in the tracking trajectory. To avoid saturation, which prevents soft landings, a specific new control law is developed. The proposed technique is based on a cyclic adaptive current preaction combined with a sliding surface. The technique consists of building a control law so that the position of the valve at which its velocity assumes its minimum is as close as possible to the landing point. At this time point, the magnetic force compensates for the elastic force and the preaction component is switched off. An experimental setup using a hardware-in-the-loop to allow a pilot investigation, model validation, and testing before implementation is considered. Real measurements of the proposed method are shown.
AB - Real-control applications of any nature can be affected by saturation limits that generate windup. When saturation occurs in a device its performance deteriorates. Electromagnetic actuators for industrial applications are being utilized ever more frequently for positioning and tracking control problems. One of the most important requirements in tracking trajectories is to achieve a soft landing, which guarantees reliable functionality and a longer component life. This paper presents an application of a typical electromagnetic actuator through a hardware-in-the-loop structure in which a soft landing is required in the tracking trajectory. To avoid saturation, which prevents soft landings, a specific new control law is developed. The proposed technique is based on a cyclic adaptive current preaction combined with a sliding surface. The technique consists of building a control law so that the position of the valve at which its velocity assumes its minimum is as close as possible to the landing point. At this time point, the magnetic force compensates for the elastic force and the preaction component is switched off. An experimental setup using a hardware-in-the-loop to allow a pilot investigation, model validation, and testing before implementation is considered. Real measurements of the proposed method are shown.
KW - Engineering
KW - Actuators
KW - position control
KW - sliding-mode control
KW - velocity control
UR - http://www.scopus.com/inward/record.url?scp=84855920642&partnerID=8YFLogxK
U2 - 10.1109/TMECH.2010.2089467
DO - 10.1109/TMECH.2010.2089467
M3 - Journal articles
VL - 17
SP - 76
EP - 85
JO - IEEE/ASME Transactions on Mechatronics
JF - IEEE/ASME Transactions on Mechatronics
SN - 1083-4435
IS - 1
M1 - 5664793
ER -