2018 Annual American Control Conference (ACC) 2018
DOI: 10.23919/acc.2018.8431637
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Control Design For Disturbance Rejection in Wind Turbines

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Cited by 2 publications
(3 citation statements)
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“…In [32], equivalence between the ADRC and flatnessbased controllers was presented. Combining Equations ( 9), ( 10), (11), and (19) results in a feedback controller with the following transfer function:…”
Section: B Optimization Problem For Controller Parametersmentioning
confidence: 99%
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“…In [32], equivalence between the ADRC and flatnessbased controllers was presented. Combining Equations ( 9), ( 10), (11), and (19) results in a feedback controller with the following transfer function:…”
Section: B Optimization Problem For Controller Parametersmentioning
confidence: 99%
“…Thus far, Active Disturbance Rejection Control (ADRC) has found widespread applications in various fields, including the control of robotic systems [8]- [10], energy systems [11], [12], autonomous vehicles [13], the chemical industry [14]- [16], civil engineering [17], and biomedical systems [18], [19]. ADRC has demonstrated its broad value in commercial applications, such as the InstaSPIN-MOTION motor control solution developed by Texas Instruments, which incorporates ADRC for high-performance control [20].…”
Section: Introductionmentioning
confidence: 99%
“…Recently, developments of wind disturbance rejection method have made significant progress. Dealing with wind disturbances, commonly used methods include robust control (Cabecinhas et al, 2014, 2015; Liu et al, 2014, 2015; Raffo et al, 2010; Soltanpour et al, 2014), designing disturbance observers (Ahmed and Kendoul, 2010; Dong et al, 2014; Leonard et al, 2012; Khaniki et al, 2018) or using adaptive control (Dong et al, 2016; Escareno et al, 2013). In addition, in Xu et al (2019), a technique based on prelinearizing transformation and singular perturbation techniques is proposed to decompose the quadrotor flight system into two subsystems, finite frequency H control and H loop shaping control for the two subsystems are designed respectively to enable the aircraft system to achieve ideal performance under wind disturbances.…”
Section: Introductionmentioning
confidence: 99%