2020
DOI: 10.1109/tvt.2019.2955902
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On the Design of Yaw Rate Control via Variable Front-to-Total Anti-Roll Moment Distribution

Abstract: In vehicle dynamics, yaw rate control is used to improve the cornering response in steady-state and transient conditions. This can be achieved through an appropriate anti-roll moment distribution between the front and rear axles of a vehicle with controllable suspension actuators. Such control action alters the load transfer distribution, which in turn provokes a lateral tire force variation. With respect to the extensive set of papers from the literature discussing yaw rate tracking through active suspension … Show more

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Cited by 20 publications
(15 citation statements)
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“…Hence, a system of two equations outputs c 1,i and c 2,i : Figure 5 compares the lateral axle force characteristics from the magic formula, Model A and Model B. The reference operating points, highlighted by the square markers, are defined for nominal values of F y,i,0 , α i,0 and F z,i,0 , corresponding to a y = 3, 6 and 9 m/s 2 , obtained for steady-state cornering through the quasi-static model in [30,[32][33][34]. For all models, the results are reported for:…”
Section: Parabolic Lateral Axle Force Model (Model B)mentioning
confidence: 99%
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“…Hence, a system of two equations outputs c 1,i and c 2,i : Figure 5 compares the lateral axle force characteristics from the magic formula, Model A and Model B. The reference operating points, highlighted by the square markers, are defined for nominal values of F y,i,0 , α i,0 and F z,i,0 , corresponding to a y = 3, 6 and 9 m/s 2 , obtained for steady-state cornering through the quasi-static model in [30,[32][33][34]. For all models, the results are reported for:…”
Section: Parabolic Lateral Axle Force Model (Model B)mentioning
confidence: 99%
“…where A, B and E are the state, input and disturbance matrices, and C, D and F are the respective output equation matrices. In the equations, α i,0 , F z,i,0 , r 0 and f 0 are obtained from the nonlinear quasi-static model from [30], suitable for the analysis of the steadystate cornering behaviour; F y,i,0 , F y,i,0 and C i,0 are calculated through the manipulation of the magic formula, whereas β 0 , ϕ 0 and S 0 result from (21), by imposing q(x 0 , u 0 , w 0 ) = 0.…”
Section: Modelmentioning
confidence: 99%
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