Disturbance/Uncertainty Estimation and Attenuation Techniques in PMSM Drives—A Survey

Yang, Jun; Chen, Wenhua; Li, Shengbo Eben; Guo, Lei; Yan, Yunda

doi:10.1109/tie.2016.2583412

Cited by 522 publications

(264 citation statements)

References 92 publications

(136 reference statements)

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“…A third-order NLESO is designed to estimate the new state _ X 3 for system (13). The form of NLESO is shown as follows …”

Section: Nleso For Hrvmentioning

confidence: 99%

“…Consider the estimation error system (16) for an HRV with nonlinear uncertainty and actuator saturation described in (13). 35 Conditions (19), (20), (21), and (22) are satisfied with ð0Þ ¼ 0.…”

Section: Theoremmentioning

confidence: 99%

“…To overcome the disadvantages caused by uncertain disturbances in nonlinear systems, some investigations have been done in recent years. [12][13][14] To efficiently tackle unknown external disturbances, a nonlinear disturbance observer has been developed for a class of nonlinear systems. 15 In the work by Chen and Ge, 16 both a state observer and a nonlinear disturbance observer have been developed to estimate unmeasured states and unknown compounded disturbances, respectively.…”

Section: Introductionmentioning

confidence: 99%

See 2 more Smart Citations

Active disturbance rejection attitude control for a hypersonic reentry vehicle with actuator saturation

Yang¹,

Yu²,

Wang³

et al. 2017

International Journal of Advanced Robotic Systems

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In this article, nonlinear uncertainty has been investigated for a hypersonic reentry vehicle subject to actuator saturation via active disturbance rejection control technology. A nonlinear extended state observer is designed to estimate "total disturbances," which is compensated with a linear controller. Both convergence of the nonlinear extended state observer and stabilization of the closed-loop system are studied in this article. Some simulation results are given to illustrate the effectiveness of the proposed method.

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“…A third-order NLESO is designed to estimate the new state _ X 3 for system (13). The form of NLESO is shown as follows …”

Section: Nleso For Hrvmentioning

confidence: 99%

Section: Theoremmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

See 1 more Smart Citation

Active disturbance rejection attitude control for a hypersonic reentry vehicle with actuator saturation

Yang¹,

Yu²,

Wang³

et al. 2017

International Journal of Advanced Robotic Systems

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show abstract

“…(1) only the position sensor is equipped and the speed sensor is unavailable; (2) the position sensor measurement signal is polluted by white noise; and (3) multiple internal and external disturbances concurrently exist in the PMSM drive system [19]. It should be specially pointed out that the dynamic of PMSM is an essential nonlinear subject to a wide range of disturbances/uncertainties in many highperformance applications.…”

Section: Introductionmentioning

confidence: 99%

“…It should be specially pointed out that the dynamic of PMSM is an essential nonlinear subject to a wide range of disturbances/uncertainties in many highperformance applications. According to Yang et al [19], the disturbances/uncertainties in PMSM systems can be classified as unmodeled dynamics, parametric uncertainties, and external disturbances. The unmodeled dynamics generally include the motor body structure-induced torque (such as cogging torque, flux harmonics, and other factors), deadtime effects, and measurement error effects.…”

Section: Introductionmentioning

confidence: 99%

Antidisturbance Vibration Suppression of the Aerial Refueling Hose during the Coupling Process

Wang

2017

International Journal of Aerospace Engineering

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In autonomous aerial refueling (AAR), the vibration of the flexible refueling hose caused by the receiver aircraft's excessive closure speed should be suppressed once it appears. This paper proposed an active control strategy based on the permanent magnet synchronous motor (PMSM) angular control for the timely and accurate vibration suppression of the flexible refueling hose. A nonsingular fast terminal sliding-mode (NFTSM) control scheme with adaptive extended state observer (AESO) is proposed for PMSM take-up system under multiple disturbances. The states and the "total disturbance" of the PMSM system are firstly reconstituted using the AESO under the uncertainties and measurement noise. Then, a faster sliding variable with tracking error exponential term is proposed together with a special designed reaching law to enhance the global convergence speed and precision of the controller. The proposed control scheme provides a more comprehensive solution to rapidly suppress the flexible refueling hose vibration in AAR. Compared to other methods, the scheme can suppress the flexible hose vibration more fleetly and accurately even when the system is exposed to multiple disturbances and measurement noise. Simulation results show that the proposed scheme is competitive in accuracy, global rapidity, and robustness.

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Bibliography

2020

PID Control System Design and Automatic Tuning Using MATLAB/Simulink

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Disturbance/Uncertainty Estimation and Attenuation Techniques in PMSM Drives—A Survey

Cited by 522 publications

References 92 publications

Active disturbance rejection attitude control for a hypersonic reentry vehicle with actuator saturation

Active disturbance rejection attitude control for a hypersonic reentry vehicle with actuator saturation

Antidisturbance Vibration Suppression of the Aerial Refueling Hose during the Coupling Process

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