TY - CHAP

T1 - Soft Landing for electromagnetic actuators through adaptive pre-action combined with a slide surface to avoid electrical saturation

AU - Mercorelli, Paolo

N1 - Conference code: 74842 Export Date: 22 May 2012 Source: Scopus Art. No.: 4677251 CODEN: 85PTA doi: 10.1109/ISIE.2008.4677251 Language of Original Document: English Correspondence Address: Mercorelli, P.; University of Applied Sciences Wolfsburg, Department of Vehicles, Production and Process Engineering, Robert Koch Platz 12, D-38440 Wolfsburg, Germany; email: p.rnercorelli@fh-wolfsburg.de References: Aström, K.L., Rundqwist, L., Integrator windup and how to avoid it (1987) Proc. of the ACC'87 American Control Conference, , Pittsburgh; Bemporad, A., Morari, M., Dua, V., Pistikopoulos, E.N., The explicit linear quadratic regulator for constrained systems (2002) Automation, 38, pp. 3-20; Birch, S., Renault research Automotive Engineering International, , http://www.sae.org/automag, Online, 2000; Butzmann, S., Melbert, J., Koch, A., Sensorless control of electromagnetic actuators for variable valve train (2000) Proc. SAE Technical Paper 2000-01-1225, , Detroit; Flierl, R., Klüting, M., The third generation of valvetrains - new fully variable valvetrains for throttle-free load control (2000) SAE, 2000-01-1227 (http://www.sae.org/automag/); Gramann, M., Nagel, M., Rockl, T., Wilczek, R., Electromagnetic actuator. In (2000), US Pat. 6, 037, 851Kothare, M.V., Campo, P.J., Morari, M., Nett, C.N., An unified framework for the study of anti-windup designs (1994) Automatica, pp. 1869-1883; Mercorelli, P., Paden, B., Prattichizzo, D., Perfect anti-windup in output tracking scheme with preaction (1998) Proc. of CCA'98 IEEE International Conference on Control Applications, , Trieste Italy; Mercorelli, P., Terwiesch, P., An anti-windup algorithm by using orthonormal haar functions in wavelet packets (2000) Proc. of International Conference in Systems with time-domain constraints, , Eindhoven (NL) Technical University; Pischinger, F., Kreuter, P., Electromagnetically operating actuator. In (1984), US Pat. 4, 455, 543Schechter, M.M., Levin, M.B., Camless engine (1996) SAE, 960581 (http://www.sae.org/automag/); M. A. Theobold, B. Lequesne, and R. Henry. Control of engine load via electromagnetic valve actuators. In SAE, 940816 (http://www.sae.org/automag/) , 1994UR - http://www.scopus.com/inward/record.url?eid=2-s2.0-57849135741&partnerID=40&md5=1f0f3e52e84adb6aed8e852a96c46e1a

PY - 2008/6/1

Y1 - 2008/6/1

N2 - Electromagnetic actuators for industrial applications are being utilized more and more frequently. One of the most important requirements in the tracking trajectories problem is to achieve a Soft Landing. This guarantees reliable functionality and a longer component life. Real control applications are affected by saturation limits which generate slew rate and windup. This paper presents an industrial application of a typical electromagnetic actuator in which Soft Landing is required in a tracking trajectories problem during a closing phase. In order to avoid saturations, which do not allow enough Soft Landing, a specific control law is developed. The proposed technique is based on a cyclic adaptive current pre-action combined with a sliding surface. The technique consists of building a control law so that the point at which the velocity assumes its minimum is as close as possible to the landing point. At that point the magnetic force compensates for the elastic one. After that the pre-action component is switched off. An experimental setup is considered and real measurements of the proposed method are shown.

AB - Electromagnetic actuators for industrial applications are being utilized more and more frequently. One of the most important requirements in the tracking trajectories problem is to achieve a Soft Landing. This guarantees reliable functionality and a longer component life. Real control applications are affected by saturation limits which generate slew rate and windup. This paper presents an industrial application of a typical electromagnetic actuator in which Soft Landing is required in a tracking trajectories problem during a closing phase. In order to avoid saturations, which do not allow enough Soft Landing, a specific control law is developed. The proposed technique is based on a cyclic adaptive current pre-action combined with a sliding surface. The technique consists of building a control law so that the point at which the velocity assumes its minimum is as close as possible to the landing point. At that point the magnetic force compensates for the elastic one. After that the pre-action component is switched off. An experimental setup is considered and real measurements of the proposed method are shown.

KW - Engineering

UR - http://www.scopus.com/inward/record.url?scp=57849135741&partnerID=8YFLogxK

U2 - 10.1109/ISIE.2008.4677251

DO - 10.1109/ISIE.2008.4677251

M3 - Article in conference proceedings

SN - 1424416655

SN - 9781424416653

T3 - IEEE International Symposium on Industrial Electronics

SP - 919

EP - 924

BT - 2008 IEEE International Symposium on Industrial Electronics, ISIE 2008

PB - IEEE - Institute of Electrical and Electronics Engineers Inc.

T2 - Institute of Electrical and Electronics Engineers International Symposium on Industrial Electronics - 2008

Y2 - 30 June 2008 through 2 July 2008

ER -