A Parameter Self-Tuning Rule Based on Spatial–Temporal Scale for Active Disturbance Rejection Control and Its Application in Flight Test Chamber Systems
Active disturbance rejection control (ADRC) emerges as a promising control approach due to its partial model-based characteristics and strong disturbance rejection capabilities. Nevertheless, it is a difficult problem to tune various parameters of ADRC in practical applications. To address the chall...
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MDPI AG
2025-05-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/12/6/465 |
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| author | Zhuang Xu Hehong Zhang Yunde Xie Chao Zhai Xin Wang Feng Huang |
| author_facet | Zhuang Xu Hehong Zhang Yunde Xie Chao Zhai Xin Wang Feng Huang |
| author_sort | Zhuang Xu |
| collection | DOAJ |
| description | Active disturbance rejection control (ADRC) emerges as a promising control approach due to its partial model-based characteristics and strong disturbance rejection capabilities. Nevertheless, it is a difficult problem to tune various parameters of ADRC in practical applications. To address the challenge of parameter tuning, this work develops a parameter self-tuning rule based on spatial–temporal scale transformations to simplify the tuning process and enhance its control performance. In particular, based on the transformations of spatial–temporal scale, the parameter tuning relationships for ADRC’s components, including tracking differentiator (TD), extended state observer (ESO) and feedback controller, are provided for a second-order nonlinear system. Numerical simulations show that the proposed method can conveniently and effectively provide a set of well-tuned parameters for ADRC to boost the efficiency of control. Finally, the proposed parameter tuning rule is applied to the intake pressure control of the flight test chamber system, further validating its effectiveness. The results demonstrate that the ADRC with the proposed parameter self-tuning method significantly improves the precision of the intake pressure under different operating conditions, thereby ensuring the reliability of aeroengine flight tests. |
| format | Article |
| id | doaj-art-226808d2987a4346b86fc201c0e35e67 |
| institution | Kabale University |
| issn | 2226-4310 |
| language | English |
| publishDate | 2025-05-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Aerospace |
| spelling | doaj-art-226808d2987a4346b86fc201c0e35e672025-08-20T03:26:11ZengMDPI AGAerospace2226-43102025-05-0112646510.3390/aerospace12060465A Parameter Self-Tuning Rule Based on Spatial–Temporal Scale for Active Disturbance Rejection Control and Its Application in Flight Test Chamber SystemsZhuang Xu0Hehong Zhang1Yunde Xie2Chao Zhai3Xin Wang4Feng Huang5College of Computer and Data Science, Fuzhou University, Fuzhou 350108, ChinaCollege of Computer and Data Science, Fuzhou University, Fuzhou 350108, ChinaSchool of New Engineering Industry, Putian University, Putian 351100, ChinaSchool of Automation, China University of Geosciences (Wuhan), Wuhan 430074, ChinaScience and Technology on Altitude Simulation Laboratory, AECC Sichuan Gas Turbine Establishment, Mianyang 621703, ChinaSchool of Mechanical Engineering and Automation, Fuzhou University, Fuzhou 350108, ChinaActive disturbance rejection control (ADRC) emerges as a promising control approach due to its partial model-based characteristics and strong disturbance rejection capabilities. Nevertheless, it is a difficult problem to tune various parameters of ADRC in practical applications. To address the challenge of parameter tuning, this work develops a parameter self-tuning rule based on spatial–temporal scale transformations to simplify the tuning process and enhance its control performance. In particular, based on the transformations of spatial–temporal scale, the parameter tuning relationships for ADRC’s components, including tracking differentiator (TD), extended state observer (ESO) and feedback controller, are provided for a second-order nonlinear system. Numerical simulations show that the proposed method can conveniently and effectively provide a set of well-tuned parameters for ADRC to boost the efficiency of control. Finally, the proposed parameter tuning rule is applied to the intake pressure control of the flight test chamber system, further validating its effectiveness. The results demonstrate that the ADRC with the proposed parameter self-tuning method significantly improves the precision of the intake pressure under different operating conditions, thereby ensuring the reliability of aeroengine flight tests.https://www.mdpi.com/2226-4310/12/6/465flight test chamber systemintake pressure controlactive disturbance rejection controlparameter tuning |
| spellingShingle | Zhuang Xu Hehong Zhang Yunde Xie Chao Zhai Xin Wang Feng Huang A Parameter Self-Tuning Rule Based on Spatial–Temporal Scale for Active Disturbance Rejection Control and Its Application in Flight Test Chamber Systems Aerospace flight test chamber system intake pressure control active disturbance rejection control parameter tuning |
| title | A Parameter Self-Tuning Rule Based on Spatial–Temporal Scale for Active Disturbance Rejection Control and Its Application in Flight Test Chamber Systems |
| title_full | A Parameter Self-Tuning Rule Based on Spatial–Temporal Scale for Active Disturbance Rejection Control and Its Application in Flight Test Chamber Systems |
| title_fullStr | A Parameter Self-Tuning Rule Based on Spatial–Temporal Scale for Active Disturbance Rejection Control and Its Application in Flight Test Chamber Systems |
| title_full_unstemmed | A Parameter Self-Tuning Rule Based on Spatial–Temporal Scale for Active Disturbance Rejection Control and Its Application in Flight Test Chamber Systems |
| title_short | A Parameter Self-Tuning Rule Based on Spatial–Temporal Scale for Active Disturbance Rejection Control and Its Application in Flight Test Chamber Systems |
| title_sort | parameter self tuning rule based on spatial temporal scale for active disturbance rejection control and its application in flight test chamber systems |
| topic | flight test chamber system intake pressure control active disturbance rejection control parameter tuning |
| url | https://www.mdpi.com/2226-4310/12/6/465 |
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