Identification and experimental study on multidimensional vibration characteristics of wind tunnel model-support system
SUN Chenjin1, ZHOU Mengde1, REN Yuhang1, ZHANG Xinyu1, ZHAO Qi1, YAN Huanhuan2, LIU Wei1
1.State Key Laboratory of High-Performance Precision Manufacturing, School of Mechanical Engineering, Dalian University of Technology, Dalian 116024, China;
2.China Academy of Aerospace Aerodynamics, Beijing 100074, China
Abstract:To address the problem of poor control effectiveness due to unknown vibration characteristics of wind tunnel model-support system, firstly, the structure and principle of wind tunnel model-support system are analyzed, and the identification scheme of system vibration characteristics is proposed. Secondly, the equivalent dynamics model of the system is established, and the pitch and yaw dimensional vibration characteristics of the system are analyzed theoretically by introducing dynamic stiffness. Then, a vibration characteristics identification method is proposed, including sinusoidal sweeping, spectrum refinement, and frequency response function. And the vibration state estimation model is established based on the identification results, which is introduced into the closed-loop control resulting in the identification-based control method. Finally, the impulse response experiment and hammering experiment are conducted, and the vibration suppression results of the conventional control method and the identification-based control method is compared. The experimental results show that the root mean square error of the frequency response discrimination in pitch and yaw dimensions is 0.0840 g/V and 0.0075 g/V, respectively. Compared with the conventional control method, the identification-based control method improves the equivalent damping ratios of pitch and yaw dimensions by 1.48 and 3.00 times, respectively, which has obvious advantages over the conventional control method.
孙晨晋1,周孟德1,任宇航1,张新雨1,赵麒1,闫欢欢2,刘巍1. 风洞模型-支撑系统多维振动特性辨识与实验研究[J]. 振动与冲击, 2024, 43(3): 218-226.
SUN Chenjin1, ZHOU Mengde1, REN Yuhang1, ZHANG Xinyu1, ZHAO Qi1, YAN Huanhuan2, LIU Wei1. Identification and experimental study on multidimensional vibration characteristics of wind tunnel model-support system. JOURNAL OF VIBRATION AND SHOCK, 2024, 43(3): 218-226.
[1] ZHOU M D, LIU W, TANG L L, et al. Multidimensional Vibration Suppression Method with Piezoelectric Control for Wind Tunnel Models[J]. Sensors, 2019, 19(18): 3998.
[2] GORBACHEV N-A, GORBUSHIN A-R, KRAPIVINA E-A, et al. Use of accelerometers for measurement of pitch and bank angles in an aerodynamic experiment[J]. Measurement Techniques, 2012, 55(8): 883-889.
[3] DAI Y K, ZHANG L, ZHAO Z P, et al. Wind-Tunnel Evaluation for an Active Sting Damper Using Multimodal Neural Networks[J]. AIAA journal, 2020, 58(5): 1939-1948.
[4] LIU W, ZHOU M D, WEN Z Q, et al. An active damping vibration control system for wind tunnel models[J]. Chinese Journal of Aeronautics, 2019, 32(9): 2109-2120.
[5] YU Y, SHEN X, HUANG Y. Multidimensional System Identification and Active Vibration Control of a Piezoelectric-Based Sting System Used in Wind Tunnel[J]. Shock and Vibration, 2020, 2020.
[6] RIVERS M-B, BALAKRISHNA S. NASA common research model test envelope extension with active sting damping at NTF[C]// 32nd AIAA Applied Aerodynamics Conference.Atlanta, GA: AIAA International, 2014.
[7] 陈陆军,黄勇,黄迪,等. 低速风洞试验模型主动抑振系统设计与验证[J]. 噪声与振动控制, 2018, 38(S1): 358-361.
CHEN Lujun,HUANG Fong,HUANG Di, et al. The design and experimental study on active vibration control system for low speed wind tunnel test model[J]. Noise and Vibration Control, 2018, 38(Suppl.1): 358-361.
[8] CHEN Lujun, HUANG Yong, HUANG Di, et al. The Design and Experimental Study on Active Vibration Control System for Low Speed Wind Tunnel Test Model[J]. Noise and Vibration Control, 2018, 38.
[9] 甄子洋,刘攀,陆宇平. 变体飞行器智能变形与飞行控制技术研究进展[J]. 南京航空航天大学学报, 2022, 54(06): 995-1006.
ZHEN Ziyang, LIU Pan, LU Yuping. Research Progress on Intelligent Deformation and Flight Control Technology of Morphing Aircraft[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2022, 54.
[10] 张尧,张婉,别大卫,等. 智能变体飞行器研究综述与发展趋势分析[J]. 飞航导弹, 2021(06): 14-23.
ZHANG Yao, ZHANG Wan, BIE Dawei, et al. Review of intelligent variant flying machine research and development trend analysis[J]. Aerodynamic Missile Journal, 2021.
[11] 沈星,涂凡凡,陈金金,等. 风洞悬臂杆结构主动减振系统的研究[J]. 振动.测试与诊断, 2014, 34(03): 414-419.
SHEN Xing, TU Fanfan, CHEN Jinjin, et al. Dynamic Characteristics Matching of Hydraulic Suspension Based on Elastic Cab[J]. Journal of Vibration, Measurement & Diagnosis, 2014, 34.
[12] ZHANG L, DAI Y K, SHEN X, et al. Research on an active pitching damper for transonic wind tunnel tests[J]. Aerospace Science and Technology, 2019, 94.
[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(02): 72-76.
SHAO Minqiang, CHEN Weidong, SHE Zhongxi. Experiment study on the active vibration control using H_∞ method based on ERA identification model[J]. Journal of Vibration and Shock, 2017, 36.
[14] 娄军强,廖江江,李国平,等. 压电柔性机械臂的实验辨识及最优极点配置抑振控制[J]. 振动与冲击, 2017, 36(16): 18-25.
LOU Junqiang, LIAO Jiangjiang, LI Guoping, et al. Experimental identification and vibration suppression of a piezoelectric flexible manipulator using an optimal poles-assignment method[J]. Journal of Vibration and Shock, 2017, 36.
[15] 康建云,毕果,苏史博. 压电柔性机械臂系统辨识与振动主动控制[J]. 振动.测试与诊断, 2021, 41(01): 90-95.
KANG Jianyun, BI Guo, SU Shibo. Experimental Identification and Active Vibration Controlof Piezoelectric Flexible Manipulator[J]. Journal of Vibration, Measurement & Diagnosis, 2021, 41.
[16] 严侠,李晓琳,胡勇. 运用正弦扫频实现电动振动台模型的频域辨识[J]. 装备环境工程, 2015, 12(02): 44-48.
YAN Xia, LI Xiaolin, HU Yong. Application of the Sine-sweep Test in Model Frequency Identification for a Electrodynamic Shaker[J]. Equipment Environmental Engineering, 2015, 12.