Robust control of microvibrations with experimental verification

Author:

Tan A C H1,Meurers T1,Veres S M1,Aglietti G1,Rogers E2

Affiliation:

1. School of Engineering Sciences, University of Southampton, Southampton, UK

2. School of Electronics and Computer Science, University of Southampton, Southampton, UK

Abstract

The paper addresses the problem of actively attenuating a particular class of vibrations, known as microvibrations, which arise, for example, in panels used on satellites. A control scheme that incorporates feedback action is developed which operates at a set of dominant frequencies in a disturbance spectrum, where the control path model is estimated online. Relative to earlier published techniques, a new feature of the presented controller is the use of the inverse Hessian to improve adaptation speed. The control scheme also incorporates a frequency estimation technique to determine the relevant disturbance frequencies with higher precision than the standard fast Fourier transform (FFT). The control scheme is implemented on an experimental test-bed and the total achieved attenuation, as measured from the experiments, is 26 dB. The low computational demand of the control scheme allows for single chip controller implementation, a feature which is particularly attractive for potential applications areas, such as small satellites, where there are critical overall weight restrictions to be satisfied while delivering high quality overall performance.

Publisher

SAGE Publications

Subject

Mechanical Engineering

Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Modeling and identification of vibration transmission in a dual-servo stage;Journal of Sound and Vibration;2018-10

2. A H∞/μ solution for microvibration mitigation in satellites: A case study;Journal of Sound and Vibration;2017-07

3. Modeling and analysis of a flywheel microvibration isolation system for spacecrafts;Advances in Space Research;2015-01

4. Microvibration analysis of a cantilever configured reaction wheel assembly;Advances in aircraft and spacecraft science;2014-10-25

5. Design and test of a soft suspension system for cantilevered momentum wheel assembly;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2012-06-27

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