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Titlebook: Control of Sandwich Nonlinear Systems; Avinash Taware,Gang Tao Book 2003 Springer-Verlag Berlin Heidelberg 2003 Hybrid Control.Sandwich Co

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发表于 2025-3-21 18:32:52 | 显示全部楼层 |阅读模式
书目名称Control of Sandwich Nonlinear Systems
编辑Avinash Taware,Gang Tao
视频videohttp://file.papertrans.cn/238/237416/237416.mp4
概述Unique monograph introducing an important new area of control system research.Includes supplementary material:
丛书名称Lecture Notes in Control and Information Sciences
图书封面Titlebook: Control of Sandwich Nonlinear Systems; Avinash Taware,Gang Tao Book 2003 Springer-Verlag Berlin Heidelberg 2003 Hybrid Control.Sandwich Co
描述V VII X Table of Contents Table of Contents XI XII Table of Contents A. Taware and G. Tao: Control of Sandwich Nonlinear Systems, LNCIS 288, pp. 1-8, 2003. Springer-Verlag Berlin Heidelberg 2003 A. Taware and G. Tao: Control of Sandwich Nonlinear Systems, LNCIS 288, pp. 9-16, 2003. Springer-Verlag Berlin Heidelberg 2003 x(t), pilot valve piston position Return Pressure Source Return Load M, b y(t) A. Taware and G. Tao: Control of Sandwich Nonlinear Systems, LNCIS 288, pp. 17-28, 2003. Springer-Verlag Berlin Heidelberg 2003 load displacement, y(t) 3 2 1 0 ?1 ?2 ?3 0 10 20 30 40 50 60 70 80 90 100 solid?without DZ, dotted? with DZ Load displacement, y(t) 0.4 0.2 0 ?0.2 ?0.4 ?0.6 ?0.8 10 20 30 40 50 60 70 80 90 100 solid?without DZ, dotted?with DZ, dashdot?compensated Load displacement, y(t) 3 2 1 0 ?1 ?2 ?3 0 10 20 30 40 50 60 70 80 90 100 Control input, x(t) 0.8 0.6 0.4 0.2 0 ?0.2 ?0.4 ?0.6 0 10 20 30 40 50 60 70 80 90 100 solid?without DZ, dotted?with DZ, dashdot?compensated Load displacement, y(t) 0.6 0.4 0.2 0 ?0.2 ?0.4 ?0.6 ?0.8 0 10 20 30 40 50 60 70 80 90 100 solid?without DZ, dotted?with DZ, dashdot?compensated A. Taware and G. Tao: Control of Sandwich Nonlinear Systems, LNCI
出版日期Book 2003
关键词Hybrid Control; Sandwich Control Theory; Sandwich Nonlinear Systems; actuator; control; control system; co
版次1
doihttps://doi.org/10.1007/3-540-46127-2
isbn_softcover978-3-540-44115-1
isbn_ebook978-3-540-46127-2Series ISSN 0170-8643 Series E-ISSN 1610-7411
issn_series 0170-8643
copyrightSpringer-Verlag Berlin Heidelberg 2003
The information of publication is updating

书目名称Control of Sandwich Nonlinear Systems影响因子(影响力)




书目名称Control of Sandwich Nonlinear Systems影响因子(影响力)学科排名




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书目名称Control of Sandwich Nonlinear Systems被引频次学科排名




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书目名称Control of Sandwich Nonlinear Systems年度引用学科排名




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Friction Compensation for A Sandwich Dynamic System,s important to design control strategies that can alleviate the performance deterioration due to friction. In addition to the disruptive nature of friction and the lack of an universal model of friction, friction compensation is further complicated by the fact that friction parameters vary with temperature and age.
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发表于 2025-3-22 15:29:19 | 显示全部楼层
Control of Systems with Sandwiched Backlash,sation and tracking control can be both achieved. Nonlinear zero dynamics systems caused by joint damping are bounded-input, bounded state stable so that feedback linearization control designs ensure that all closed-loop signals are bounded and asymptotic tracking is achievable.
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Book 20032003. Springer-Verlag Berlin Heidelberg 2003 A. Taware and G. Tao: Control of Sandwich Nonlinear Systems, LNCIS 288, pp. 9-16, 2003. Springer-Verlag Berlin Heidelberg 2003 x(t), pilot valve piston position Return Pressure Source Return Load M, b y(t) A. Taware and G. Tao: Control of Sandwich Nonline
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发表于 2025-3-22 21:54:18 | 显示全部楼层
https://doi.org/10.1007/978-3-662-24723-5, aircraft accidents have been caused by actuator failures. The compensation of actuator nonlinearities is equally important as they limit both static and dynamic performance of control systems. These nonlinearities are typically nonsmooth nonlinearities such as dead-zone, hysteresis and backlash.
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发表于 2025-3-23 02:10:21 | 显示全部楼层
Control of Systems with Actuator Nonlinearities and Failures,, aircraft accidents have been caused by actuator failures. The compensation of actuator nonlinearities is equally important as they limit both static and dynamic performance of control systems. These nonlinearities are typically nonsmooth nonlinearities such as dead-zone, hysteresis and backlash.
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