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Applied adaptive disturbance rejection using output redefinition on magnetic bearings.

机译:在磁性轴承上使用输出重新定义应用自适应干扰抑制。

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摘要

Recent work has shown Adaptive Disturbance Rejection to be an effective technique for rejecting forces due to imbalance, runout and base motion disturbances on flywheels supported by magnetic bearings over a large span of frequencies. Often the applicability of some of the adaptive methods is limited because they require certain properties (such as almost-strict positive realness) that magnetic bearings do not possess. In this thesis, one method for adaptive disturbance rejection, called Adaptive Feedforward Cancellation (AFC), is modified to allow for a much wider range of frequencies to be rejected. This is accomplished by redefining the output of the original system to be the output from a reduced order state estimator instead. This can give a new system with an infinite gain margin. Additionally, the adaptation laws for the two disturbance rejection gains are slightly modified so that each adapts to a different signal in order to provide the best performance. A detailed model of a magnetic bearing is developed and computer simulations based on that model are performed to give an initial test of the new control law. A state-of-the-art magnetic bearing setup is then developed and used to implement the new control laws and determine their effectiveness. The results are successful and validate the new ideas that are presented.
机译:最近的工作表明,自适应扰动抑制是一种有效的技术,可以消除由于大范围频率上的电磁轴承支撑的飞轮上的不平衡,偏心和基本运动扰动而产生的力。通常,某些自适应方法的适用性受到限制,因为它们需要磁性轴承不具备的某些属性(例如,几乎严格的正真实性)。在本文中,一种用于自适应干扰抑制的方法被称为自适应前馈消除(AFC),被修改为允许更大范围的频率被抑制。这是通过将原始系统的输出重新定义为降阶状态估计器的输出来实现的。这可以给新系统带来无限的增益余量。另外,对两个干扰抑制增益的自适应律进行了轻微修改,以便每个自适应不同的信号,以提供最佳性能。开发了电磁轴承的详细模型,并基于该模型进行了计算机仿真,以对新的控制规律进行初步测试。然后,开发了一种最新的电磁轴承装置,并用于实施新的控制规律并确定其有效性。结果是成功的,并验证了提出的新想法。

著录项

  • 作者

    Matras, Alex Logan.;

  • 作者单位

    University of Colorado at Boulder.;

  • 授予单位 University of Colorado at Boulder.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2005
  • 页码 147 p.
  • 总页数 147
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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