| Citation: | KOU Xiping, LI Binbin, YANG Zhichun, et al. Active vibration control technology of wind tunnel model based on PD control algorithm[J]. Journal of Aerospace Power, 2025, 40（5）：20230685 doi: 10.13224/j.cnki.jasp.20230685
|
Considering the phenomenon of low frequency and large amplitude vibration of the test model in the process of transonic wind tunnel test, a multi-mode PD control algorithm was designed and good control effect was achieved in numerical simulation, ground test and wind tunnel test. The algorithm was designed to suppress the pitch direction vibration with the largest amplitude, the first two main vibration modes were obtained by modal decomposition of the pitching direction vibration data using Fourier series, the recursive least square method was used to identify the parameters of the channel transfer function of the single mode, the control algorithm was designed for the single-mode channel transfer function. The adopted theoretical methods and algorithm design ideas were discussed, and the methods adopted by numerical simulation were verified. The results showed that the algorithm can achieve better control of the controlled object. The designed control algorithm was loaded into the active vibration suppression system. Through ground debugging verification and wind tunnel test, it was finally shown that the developed damping system can effectively suppress the vibration of the wind tunnel model, and the vibration attenuation can reach more than 80%. The wind tunnel test duration increased by about 50 s, and the measured value of the test angle of attack balance increased to 5°. Thanks to its engineering practical value, this research can provide strong support for the follow-up research of multi-freedom control, multi-actuator collaborative control, and intelligent control algorithm.
| [1] |
曾开春,寇西平,杨兴华,等. 跨声速风洞试验模型主动减振结构优化设计[J]. 航空学报,2022,43(2): 224944. ZENG Kaichun,KOU Xiping,YANG Xinghua,et al. Optimization of active vibration damping structure for transonic wind tunnel test model[J]. Acta Aeronautica et Astronautica Sinica,2022,43(2): 224944. (in Chinese
ZENG Kaichun, KOU Xiping, YANG Xinghua, et al. Optimization of active vibration damping structure for transonic wind tunnel test model[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(2): 224944. (in Chinese)
|
| [2] |
余立,杨兴华,寇西平,等. 跨声速风洞模型主动减振系统试验研究[J]. 南京航空航天大学学报,2019,51(4): 526-533. YU Li,YANG Xinghua,KOU Xiping,et al. Experiment on active vibration reduction system for transonic wind tunnel model[J]. Journal of Nanjing University of Aeronautics and Astronautics,2019,51(4): 526-533. (in Chinese
YU Li, YANG Xinghua, KOU Xiping, et al. Experiment on active vibration reduction system for transonic wind tunnel model[J]. Journal of Nanjing University of Aeronautics and Astronautics, 2019, 51(4): 526-533. (in Chinese)
|
| [3] |
RIVERS M B,BALAKRISHNA S. NASA common research model test envelope extension with active sting damping at NTF[R]. AIAA 2014-3135,2014.
|
| [4] |
BALAKRISHNA S,BUTLER D,ACHESON M,et al. Design and performance of an active sting damper for the NASA common research model[R]. AIAA 2011-953,2011.
|
| [5] |
曾开春,查俊,马涛,等. 风洞模型抑振装置及系统: CN110907128A[P]. 2020-03-24. ZENG Kaichun,ZHA Jun,MA Tao,et al. Wind tunnel model vibration suppression device and system: CN110907128A[P]. 2020-03-24. (in Chinese).
ZENG Kaichun, ZHA Jun, MA Tao, et al. Wind tunnel model vibration suppression device and system: CN110907128A[P]. 2020-03-24. (in Chinese).
|
| [6] |
FEHREN H,GNAUERT U,WIMMEL R,et al. Validation testing with the active damping system in the European Transonic Windtunnel[R]. AIAA 2001-610,2001.
|
| [7] |
SINGH S,KAUR M. Gain scheduling of PID controller based on fuzzy systems[R]. Incheon,South Korea: 3th International Conference on Advancements in Engineering & Technology (ICAET-2016),2016.
|
| [8] |
佘重禧. 跨音速风洞测力试验模型的振动主动控制研究[D]. 南京: 南京航空航天大学,2013. SHE Chongxi. Study on active vibration control for wind tunnel testing model in transonic test[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2013. (in Chinese
SHE Chongxi. Study on active vibration control for wind tunnel testing model in transonic test[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2013. (in Chinese)
|
| [9] |
GANESH RAM A. Real time implementation of fuzzy based adaptive PI controller for a spherical tank system[J]. International Journal of Simulation Systems Science & Technology,2013,14(6): 1-8.
|
| [10] |
聂旭涛,陈万华,陈振华,等. 压电组件嵌入式风洞模型支撑系统振动主动控制仿真[J]. 振动与冲击,2014,33(9): 137-141,152. NIE Xutao,CHEN Wanhua,CHEN Zhenhua,et al. Active vibration control simulation for a piezoelectric package-embedded wind tunnel model support system[J]. Journal of Vibration and Shock,2014,33(9): 137-141,152. (in Chinese
NIE Xutao, CHEN Wanhua, CHEN Zhenhua, et al. Active vibration control simulation for a piezoelectric package-embedded wind tunnel model support system[J]. Journal of Vibration and Shock, 2014, 33(9): 137-141, 152. (in Chinese)
|
| [11] |
王学,陈陆军,黄勇,等. 低速风洞模型振动主动控制仿真研究[J]. 振动与冲击,2014,33(5): 14-19. WANG Xue,CHEN Lujun,HUANG Yong,et al. Active control method for model vibration in a low speed wind tunnel[J]. Journal of Vibration and Shock,2014,33(5): 14-19. (in Chinese
WANG Xue, CHEN Lujun, HUANG Yong, et al. Active control method for model vibration in a low speed wind tunnel[J]. Journal of Vibration and Shock, 2014, 33(5): 14-19. (in Chinese)
|
| [12] |
PATIL N J,BORASE R P. Tuning of fuzzy controller using set point weighing PID parameters[C]//2015 International Conference on Pervasive Computing. New York: IEEE,2015: 1-6.
|
| [13] |
邵敏强,陈卫东,佘重禧. 基于ERA模型辨识的H∞振动主动控制试验研究[J]. 振动与冲击,2017,36(2): 72-76. SHAO Minqiang,CHEN Weidong,SHE Chongxi. Experiment study on the active vibration control using H∞ method based on ERA identification model[J]. Journal of Wibration and Shock,2017,36(2): 72-76. (in Chinese
SHAO Minqiang, CHEN Weidong, SHE Chongxi. Experiment study on the active vibration control using H∞ method based on ERA identification model[J]. Journal of Wibration and Shock, 2017, 36(2): 72-76. (in Chinese)
|
| [14] |
FAHMIZAL,SURRIANI A,BUDIYANTO M,et al. Altitude control of quadrotor using fuzzy self tuning PID controller[C]//2017 5th International Conference on Instrumentation,Control,and Automation. New York: IEEE,2017: 67-72.
|
| [15] |
温正权. 风洞模型多模态振动主动控制方法研究[D]. 辽宁 大连: 大连理工大学,2020. WEN Zhengquan. Research on active multi-modal vibration control of windtunnel model[D]. Dalian Liaoning: Dalian University of Technology,2020. (in Chinese
WEN Zhengquan. Research on active multi-modal vibration control of windtunnel model[D]. Dalian Liaoning: Dalian University of Technology, 2020. (in Chinese)
|
| [16] |
刘巍,孙晨晋,周孟德,等. 一种模型适应型振动主动抑制方法: CN202111344651.9[P] . 2022-08-09.
|
| [17] |
LIU W,ZHOU M D,WEN Z Q. An active damping vibration control system for wind tunnel models[J]. Chinese Journal of Aeronautics,2019(32): 2109-2120.
|
| [18] |
刘伟国. 支杆式风洞模型主动振动抑制控制方法研究[D]. 辽宁 大连: 大连理工大学,2015.
|
| [19] |
杨智春,王巍,谷迎松,等. 一种弯曲型压电堆作动器的设计及在振动控制中的应用[J]. 振动与冲击,2009,28(9): 130-134,219. YANG Zhichun,WANG Wei,GU Yingsong,et al. Smart structure vibration control using a new bending type of piezoelectric stack actuator[J]. Journal of Vibration and Shock,2009,28(9): 130-134,219. (in Chinese doi: 10.3969/j.issn.1000-3835.2009.09.028
YANG Zhichun, WANG Wei, GU Yingsong, et al. Smart structure vibration control using a new bending type of piezoelectric stack actuator[J]. Journal of Vibration and Shock, 2009, 28(9): 130-134, 219. (in Chinese) doi: 10.3969/j.issn.1000-3835.2009.09.028
|
| [20] |
PRAKASH S,RENJITH KUMAR T G,RAJA S,et al. Active vibration control of a full scale aircraft wing using a reconfigurable controller[J]. Journal of Sound and Vibration,2016,361: 32-49. doi: 10.1016/j.jsv.2015.09.010
|
DownLoad:
