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个人信息Personal Information
研究员 博士生导师
招生学科专业:
航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 航空学院
机械 -- 【招收博士、硕士研究生】 -- 航空学院
性别:男
毕业院校:南京航空航天大学
学历:博士毕业
学位:工学博士学位
所在单位:航空学院
办公地点:明故宫校区行政楼515
联系方式:13951782331
电子邮箱:
Structure modal optimization of a strapdown inertial navigation system for an electric helicopter using an adaptive surrogate model
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所属单位:航空学院
发表刊物:JOURNAL OF VIBROENGINEERING
关键字:modal analysis extended radial basis function adaptive surrogate model optimization
摘要:The purpose of this research is to prove the eventuality of using a novel adaptive surrogate model for optimization problems. The adaptive surrogate model is based on iteration sampling and extended radial basis function (ERBF). This method improves the precision by a means that new sample points is placed in the blank area and all the sample points is uniformly distributed in the design region. The precision of the surrogate model is checked using standard error measure to determine whether updating the surrogate model or not. Since the prediction of modal frequencies require structure modal simulations. In order to decrease the number of computer simulations, a Multi-Island GA approach is combined with the adaptive surrogate model to find the optimum modal frequencies of a strapdown inertial navigation system for electric helicopters. The strapdown inertial navigation system is comprised of damping material, counterweight material and inertial navigation sensor. This is a multi-objective functions optimization problem since the modal frequencies are considered from mode 1 to mode 6 in this paper. Several weights of multi-objective functions are utilized to research the modal frequencies. The whole number of 15 sampling points is picked to build the primary surrogate model using Latin hypercube sampling (LHS). The results of adaptive surrogate model show that two new sampling points are needed to reform the precision of the surrogate model under the condition of 2 % confidence bounds. The structure modal optimization results show that the choice of the weights for the multi-objective functions has a major effect on the final optimum modal frequencies. Time-and frequency-domain analysis indicated that the optimum modal frequencies are far away from the excitation frequencies to avoid strapdown inertial navigation system resonance as far as possible.
ISSN号:1392-8716
是否译文:否
发表时间:2017-11-01
合写作者:郭述臻,昂海松
通讯作者:郑祥明