Dynamometer Test Rig Drive Train Control with a High Dynamic Performance: Measurements and Experiences

被引:5
|
作者
Neshati, Mohsen [1 ]
Wenske, Jan [1 ]
机构
[1] Fraunhofer Inst Wind Energy Syst IWES, Dynam Nacelle Lab, D-27572 Bremerhaven, Germany
来源
IFAC PAPERSONLINE | 2020年 / 53卷 / 02期
关键词
Dynamometers; Automatic control; H-infinity control; Feedforward control; Kalman filters; Torque control; Dynamic tests; Dynamic properties; Hardware-in-the-loop simulation;
D O I
10.1016/j.ifacol.2020.12.1846
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents the control design and dynamic performance evaluation for a 10 MW dynamometer test rig for wind turbine nacelles. The purpose is to control the applied torque by the drive train, required for an accurate emulation of rotor characteristics in the laboratory. This is implemented in a hardware-in-the-loop simulation framework for electrical certification test procedures, introducing high dynamic requirements. Therefore, a feedback-feedforward as well as a H-infinity controller is implemented to benefit from high dynamic and robustness capabilities, respectively. Furthermore, due to the lack of a suitable torque measurement in the meganewton-meter range, model-based algorithms are incorporated and the implemented time-varying Kalman filter provides the unmeasured variables. In addition, for performance analysis independent of any specimen, experiments using small signal perturbation as test functions are executed under load conditions. The results are analysed here elaborately and the obtained control bandwidth is distinguished under realistic conditions. Overall, the measurements demonstrate an effe.tive control with a bandwidth of up to 30Hz. Copyright (C) 2020 The Authors.
引用
收藏
页码:12663 / 12668
页数:6
相关论文
共 50 条
  • [21] Repeatability in measurements and control settings of a small francis turbine test rig
    Kumar, Sandeep
    Gandhi, Bhupendra K.
    Cervantes, Michel J.
    FLOW MEASUREMENT AND INSTRUMENTATION, 2022, 88
  • [22] Effect of climatic conditions on the performance of a multistage dynamic dehumidifier test rig
    Salins, Sampath Suranjan
    Reddy, S. V. Kota
    Kumar, Shiva
    BUILDING AND ENVIRONMENT, 2021, 205
  • [23] Recuperator dynamic performance: Experimental investigation with a microgas turbine test rig
    Ferrari, Mario L.
    Sorce, Alessandro
    Pascenti, Matteo
    Massardo, Aristide F.
    APPLIED ENERGY, 2011, 88 (12) : 5090 - 5096
  • [24] Test Rig for High-Temperature Thermopower and Electrical Conductivity Measurements
    S. Boldrini
    A. Famengo
    F. Montagner
    S. Battiston
    S. Fiameni
    M. Fabrizio
    S. Barison
    Journal of Electronic Materials, 2013, 42 : 1319 - 1323
  • [25] Test Rig for High-Temperature Thermopower and Electrical Conductivity Measurements
    Boldrini, S.
    Famengo, A.
    Montagner, F.
    Battiston, S.
    Fiameni, S.
    Fabrizio, M.
    Barison, S.
    JOURNAL OF ELECTRONIC MATERIALS, 2013, 42 (07) : 1319 - 1323
  • [26] Dynamic analysis of high-speed train with considering drive system
    Qi Y.-Y.
    Dai H.-Y.
    Gao H.
    Gan F.
    Zhendong Gongcheng Xuebao/Journal of Vibration Engineering, 2019, 32 (01): : 176 - 183
  • [27] A Deadbeat Current and Flux Vector Control for IPMSM Drive with High Dynamic Performance
    Ton, That-Dong
    Hsieh, Min-Fu
    APPLIED SCIENCES-BASEL, 2022, 12 (08):
  • [28] A force control test rig for the dynamic characterization of helicopter primary flight control systems
    Bertucci, Alessandro
    Mornacchi, Andrea
    Jacazio, Giovanni
    Sorli, Massimo
    PROCEEDINGS OF THE 2ND INTERNATIONAL CONFERENCE ON DYNAMICS AND VIBROACOUSTICS OF MACHINES (DVM2014), 2015, 106 : 71 - 82
  • [29] Measurements of the performance of BSCCOHTS tape under magnetic fields with a cryocooled test rig
    Young, MA
    Demko, JA
    Gouge, MJ
    Pace, MO
    Lue, JW
    Grabovickic, R
    IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY, 2003, 13 (02) : 2964 - 2967
  • [30] Dynamic Rig for Validation of Control Algorithms at High Angles of Attack
    Ignatyev, Dmitry I.
    Sidoryuk, Maria E.
    Kolinko, Konstantin A.
    Khrabrov, Alexander N.
    JOURNAL OF AIRCRAFT, 2017, 54 (05): : 1760 - 1771