Helicopter Track and Balance With Artificial Neural Nets

Author:

Taitel Howard J.1,Danai Kourosh1,Gauthier David2

Affiliation:

1. Department of Mechanical Engineering, University of Massachusetts, Amherst, MA 01003

2. Sikorsky Aircraft, Stratford, CT 06601

Abstract

Before a helicopter leaves the plant, it needs to be tuned so that its vibrations meet the required specifications. Helicopter track and balance is currently performed based on “sensitivity coefficients” which have been developed statistically after years of production experience. The fundamental problem with using these sensitivity coefficients, however, is that they do not account for the nonlinear coupling between modifications or their effect on high amplitude vibrations. In order to ensure the reliability of these sensitivity coefficients, only a limited number of modifications are simultaneously applied. As such, a number of flights are performed before the aircraft is tuned, resulting in increased production and maintenance cost. In this paper, the application of feedforward neural nets coupled with back-propagation training is demonstrated to learn the nonlinear effect of modifications, so that the appropriate set of modifications can be selected in fewer iterations (flights). The effectiveness of this system of neural nets for track and balance is currently being investigated at the Sikorsky production line.

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Reference10 articles.

1. Fahlman, S. E., and Lebiere, C., 1990, “The Cascaded-Correlation Learning Architecture,” Technical Report No. CMU-CS-90-100, School of Computer Science, Carnegie Mellon University.

2. Hertz, J. A., Krogh, A. S., and Palmer, R. G., 1991, Introduction to the Theory of Neural Computation, Addison-Wesley, Redwood City, CA.

3. Jordan, M. I., and Rumelhart, D. E., 1992, “Forward Models: Supervised Learning with a Distal Teacher,” Cognitive Science, in print.

4. Kung, S. Y., and Hu, Y. H., 1991, “A Frobenius Approximation Reduction Method (Farm) for Determining Optimal Number of Hidden Units,” Proc. IJCNN, IEEE, Seattle, WA, July, pp. 163–168.

5. Matsuoka K. , 1991, “An Approach to the Generalization Problem in the Backpropagation Method,” Systems and Computers in Japan, Vol. 22, No. 2, pp. 897–905.

Cited by 9 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. A novel constrained optimal tuning method with application to helicopter rotor track and balance;Mechanical Systems and Signal Processing;2023-02

2. Cramer–Rao Bound Development for Linear Time Periodic Systems;Journal of Dynamic Systems, Measurement, and Control;2010-11-23

3. A generalized dynamic balancing procedure for the AH-64 tail rotor;Journal of Sound and Vibration;2009-09

4. A comparison of main rotor smoothing adjustments using linear and neural network algorithms;Journal of Sound and Vibration;2008-04

5. Cramer-Rao Bound Development for Linear Time Periodic Systems;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3