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兵工学报 ›› 2016, Vol. 37 ›› Issue (2): 348-356.doi: 10.3969/j.issn.1000-1093.2016.02.022

• 论文 • 上一篇    下一篇

基于矢量匹配的扰动力矩消除方法

杨雪松, 李长春, 延皓, 黄静, 李竞   

  1. (北京交通大学 机械与电子控制工程学院, 北京 100044)
  • 收稿日期:2015-09-21 修回日期:2015-09-21 上线日期:2016-04-22
  • 通讯作者: 杨雪松 E-mail:yxskey@sina.com
  • 作者简介:杨雪松(1986—),男,博士研究生
  • 基金资助:
    北京高等学校青年英才计划项目(YETP0567)

Vector Matching-based Disturbance Torque Elimination Method

YANG Xue-song, LI Chang-chun, YAN Hao, HUANG Jing, LI Jing   

  1. (School of Mechanical, Electronic and Control Engineering, Beijing Jiaotong University, Beijing 100044, China)
  • Received:2015-09-21 Revised:2015-09-21 Online:2016-04-22
  • Contact: YANG Xue-song E-mail:yxskey@sina.com

摘要: 随着电机制造和驱动技术的不断发展,在航空航天器舵机地面测试中电机正在逐渐替代液压装置,并成为中小功率负载模拟器的首选驱动部件。由于电动、液压系统数学模型间存在相似性,将液压系统阀控缸模型特征方程的分解方法引申到电机加载系统模型的分解中,得到了电动负载模拟器结构参数与位置扰动力矩频域特性的对应关系,这个方法可称为电-液等效法。针对电动负载模拟试验中常用的扫频试验,提出了基于幅相辨识和遗传算法的矢量匹配法以消除扰动力矩。通过AMESim仿真和电动负载模拟试验台上的验证表明,矢量匹配法可将加载力矩控制误差的标准差控制在该电动负载模拟器额定加载范围(±15 N·m)的1%以内。该方法较之其他方法具有适应能力强、简单灵活等优点,可大大提高负载模拟器在正弦位置扰动下的加载精度。随着电机制造和驱动技术的不断发展,在航空航天器舵机地面测试中电机正在逐渐替代液压装置,并成为中小功率负载模拟器的首选驱动部件。由于电动、液压系统数学模型间存在相似性,将液压系统阀控缸模型特征方程的分解方法引申到电机加载系统模型的分解中,得到了电动负载模拟器结构参数与位置扰动力矩频域特性的对应关系,这个方法可称为电-液等效法。针对电动负载模拟试验中常用的扫频试验,提出了基于幅相辨识和遗传算法的矢量匹配法以消除扰动力矩。通过AMESim仿真和电动负载模拟试验台上的验证表明,矢量匹配法可将加载力矩控制误差的标准差控制在该电动负载模拟器额定加载范围(±15 N·m)的1%以内。该方法较之其他方法具有适应能力强、简单灵活等优点,可大大提高负载模拟器在正弦位置扰动下的加载精度。

关键词: 飞行器试验技术, 〖JP9〗电-〖JP〗液等效法, 矢量匹配, 位置扰动, 幅相辨识

Abstract: With the continuous development of manufacturing and drive technologies for electric motor, the electric motor is gradually taking the place of electro-hydraulic device, and becomes the preferred drive element of low and middle power level load simulators in the field of load simulation. There is similarity between the mathematical models of electric and hydraulic systems. The motor-hydraulic equivalent method is proposed, and the corresponding relation among the structure parameters of electric load simulator and the frequency domain characteristics of perturbance torque is obtained. The sweep test plays an important role in the electric load module test. According to the working conditions, a vector-based disturbance torque elimination method is put forward. The feasibility of the principle of the proposed method is verified by the AMESim simulation and the electric load simulation test stand. The test results show that the residual disturbance torque can be controlled within 1% of the rated load range (±15 N·m) of electric load simulator by the proposed method based on the amplitude-phase identification and genetic algorithm. Compared with other methods, the method is simpler, more flexible and adaptable. And it can be used to greatly improve the test accuracy of the load simulator suffered from the sinusoidal position disturbation.

Key words: experimental technology of aerocraft, motor-hydraulic equivalent method, vector matching, position disturbation, amplitude-phase identification

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