MELECON '98. 9th Mediterranean Electrotechnical Conference. Proceedings (Cat. No.98CH36056)
DOI: 10.1109/melcon.1998.699389
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Dynamic behaviour of a linear induction motor

Abstract: Although conventional rotating machines have been largely used to drive underground transportation systems, linear induction motors are also being considered for future applications owing to their indisputable advantages. A mathematical model for the transient behavior analysis of linear induction motors, when operating with constant r.m.s. currents, is presented in this paper.. Operating conditions, like phase short-circuit and input frequency variations and also some design characteristics, such as air-gap a… Show more

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Cited by 11 publications
(7 citation statements)
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“…Dynamic and steady-state modeling of the LIM has been widely addressed in the literature. In this regard, the literature can be divided into four categories, including modified mechanical equation-based models (MMEMs) [4][5][6], winding function-based models (WFMs) [7][8][9], field theory-based models (FTMs) [10][11][12][13][14], and Duncan's approach based models (DAMs) [15][16][17][18][19][20].…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Dynamic and steady-state modeling of the LIM has been widely addressed in the literature. In this regard, the literature can be divided into four categories, including modified mechanical equation-based models (MMEMs) [4][5][6], winding function-based models (WFMs) [7][8][9], field theory-based models (FTMs) [10][11][12][13][14], and Duncan's approach based models (DAMs) [15][16][17][18][19][20].…”
Section: Introductionmentioning
confidence: 99%
“…The braking force due to the end effect has been modeled by using the Taylor series, which is a function of linear velocity [4,5]. In [6], the resultant propulsive force was calculated using the air-gap flux density with consideration of the longitudinal end effect. The MMEMs are simple and can also predict the dynamic performance of LIMs.…”
Section: Introductionmentioning
confidence: 99%
“…In contrast, a thrust correction coefficient introduced by [12] can be used to calculate an actual thrust to compensate for the end effect. A related method to deal with the problem is the introduction of an external force corresponding to the end effect into the RIM model to provide a more accurate modeling of an LIM considering the end effect, as shown in [13]. In another work [14], the authors proposed a new type of end-effect compensator.…”
Section: Introductionmentioning
confidence: 99%
“…On the other hand, there is a thrust correction coefficient introduced by [7] and [8] to calculate the actual thrust to compensate for the end effect. A related method to deal with the problem is that an external force corresponding to the end effect is introduced into the RIM model to provide a more accurate modeling of an LIM under consideration of the end effect as shown in [9]. In another work [10], [21], [22], extra compensating-winding was proposed to alleviate such problem.…”
Section: Introductionmentioning
confidence: 99%