Enhancement of Solar Array Drive Assembly System Stability through Linear Active Disturbance Rejection Control

To improve the Solar Array Drive Assembly (SADA) system, a servo control method known as Linear Active Disturbance Rejection Control (LADRC) is introduced, utilizing a speed loop for a Permanent Magnet Synchronous Motor (PMSM). This method serves as an alternative to the conventional proportional–integral (PI) controller, which exhibits a limited stability margin. The use of the LADRC controller leads to decreased overshoot and enhances the system’s robustness against disturbances. First, the mathematical representation of the PMSM alongside the dynamic model of the solar wing is established. Following that, the application of the Lyapunov stability theory is employed to illustrate the stability of the drive system utilizing LADRC, thereby validating the stability of the SADA. Lastly, simulation experiments are performed using the MATLAB2021a/Simulink digital environment. The simulation results under various operational conditions indicate the significant improvement in stability compared to the PI controller, achieving the stability level of 9.603×10−5, demonstrates enhanced performance in terms of speed and resistance to disturbances.

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Publication Details

Journal
Aerospace
Published
2024-09-13
DOI
https://doi.org/10.3390/aerospace11090751
Citations
1
Primary Topic
Microgrid Control and Optimization
Type
article
Field-Weighted Citation Impact
0.33
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Enhancement of Solar Array Drive Assembly System Stability through Linear Active Disturbance Rejection Control

Jianyuan Wang, Jian Wang, Jinbao Chen, Shiyue Gan et al.
1 citations
Aerospace
Microgrid Control and Optimization
0.33
article

Enhancement of Solar Array Drive Assembly System Stability through Linear Active Disturbance Rejection Control

Jianyuan Wang, Jian Wang, Jinbao Chen, Shiyue Gan, Zhuochen Hu
article en
1 citations

Abstract

To improve the Solar Array Drive Assembly (SADA) system, a servo control method known as Linear Active Disturbance Rejection Control (LADRC) is introduced, utilizing a speed loop for a Permanent Magnet Synchronous Motor (PMSM). This method serves as an alternative to the conventional proportional–integral (PI) controller, which exhibits a limited stability margin. The use of the LADRC controller leads to decreased overshoot and enhances the system’s robustness against disturbances. First, the mathematical representation of the PMSM alongside the dynamic model of the solar wing is established. Following that, the application of the Lyapunov stability theory is employed to illustrate the stability of the drive system utilizing LADRC, thereby validating the stability of the SADA. Lastly, simulation experiments are performed using the MATLAB2021a/Simulink digital environment. The simulation results under various operational conditions indicate the significant improvement in stability compared to the PI controller, achieving the stability level of 9.603×10−5, demonstrates enhanced performance in terms of speed and resistance to disturbances.

AerospaceVol. 11(9)
Nanjing University of Aeronautics and Astronautics (CN)
Affordable and clean energy
Openalex Percentile: Top 42%
Microgrid Control and Optimization
0.33
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Enhancement of Solar Array Drive Assembly System Stability through Linear Active Disturbance Rejection Control — Jianyuan Wang, Jian Wang, et al. · Aerospace (2024) | TGRS Research Map | TGRS