[2] [2] COLE S R, NOLL T E, PERRY B. Transonic dynamics tunnel aeroelastic testing in support of aircraft development［J］. Journal of Aircraft, 2015, 40(5):820-831.

[4] [4] RIVERS M B, BALAKRISHNA S. NASA common research model test envelope extension with active sting damping at NTF［J］. AIAA, 2014:3135.

[5] [5] SHEN Xing, ZHANG Lei, CHEN Yuchen. Development and validation research of an active sting damper in a transonic acoustic wind tunnel［C］//Islamabad: International Bhurban Conference on Applied Sciences and Technology (IBCAST), IEEE, 2018: 172-177.

[7] [7] LIU Yanfang, WANG Yan, CHEN Xin.Online hysteresis identification and compensation for piezoelectric actuators［J］. IEEE Transactions on Industrial Electronics, 2019,67(7):5595-5603.

[8] [8] LIU Jiabin, ZHOU Kemin. Active vibration control of a dynamic hysteresis system using μ-synthesis［J］. IEEE Access, 2018,6:76831-76837.

[13] [13] CAMPANELLI S L, CASALINO G, LUDOVICO A D, et al. An artificial neural network approach for the control of the laser milling process［J］. The International Journal of Advanced Manufacturing Technology, 2013, 66(9/12):1777-1784.