2016 4th International Conference on Robotics and Mechatronics (ICROM) 2016
DOI: 10.1109/icrom.2016.7886854
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Position control of a servo-pneumatic actuator using generalized Maxwell-Slip friction model

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Cited by 5 publications
(4 citation statements)
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“…Friction compensation is also significant in step positioning on top of trajectories. As presented by Soleymani et al [19], Tran et al [20], and Rahman et al [21], the RMSE errors for sinewave tracking were reduced from 15% to up to 50%. Figure 28 shows the tracking error of a sinewave trajectory comparison between two different friction models applied where GMS model performs better than Stribeck model.…”
Section: Experimental Analysismentioning
confidence: 71%
See 1 more Smart Citation
“…Friction compensation is also significant in step positioning on top of trajectories. As presented by Soleymani et al [19], Tran et al [20], and Rahman et al [21], the RMSE errors for sinewave tracking were reduced from 15% to up to 50%. Figure 28 shows the tracking error of a sinewave trajectory comparison between two different friction models applied where GMS model performs better than Stribeck model.…”
Section: Experimental Analysismentioning
confidence: 71%
“…https://doi.org/10.31436/iiumej.v24i2. 2766 An example of a controller that adapts both nonlinear controls with a friction compensation is an SMC with generalized Maxwell Slip (GMS) dynamic friction as explored by [19], whereby the author adapts both dynamic and static friction. The GMS model is applied during near zero velocity while static friction is implemented during velocity.…”
Section: Introductionmentioning
confidence: 99%
“…It includes both velocity and displacement in modeling friction behavior [7]. GMS is now one of the most used models in piston seal design [8], [9], [10]. Therefore, in this study, the GMS model is used as a benchmark for validating the proposed method.…”
Section: Introductionmentioning
confidence: 99%
“…). This becomes critical when the perpendicular force is the dominant one, such as in airplane wings and engine blades ( Figure 1A) [22][23][24][25][26][27]. In all aforementioned parameters, the abrupt mechanical and thermodynamic changes at the interface of A and B are the origin of stress in the system.…”
Section: Introductionmentioning
confidence: 99%