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子空间跟踪算法在热模态问题中的应用研究
引用本文:周昊天,赵婕,曹为政,史晓鸣,于开平.子空间跟踪算法在热模态问题中的应用研究[J].上海航天,2018(4):85-90.
作者姓名:周昊天  赵婕  曹为政  史晓鸣  于开平
作者单位:哈尔滨工业大学航天学院;黑龙江科技大学计算机与信息工程学院;上海机电工程研究所
基金项目:国家自然科学基金(11372084);上海航天科技创新基金(SAST2015012)
摘    要:总结子空间跟踪算法识别模态参数的一般步骤。对一个有理论参考解的时变两自由度系统进行仿真,利用添加不同量级噪声的响应数据对系统进行辨识。辨识结果表明:基于新信息准则的子空间跟踪算法拥有较好的抗噪能力。对飞行器舵面结构进行受控快速加热,辨识快速升温过程中的模态参数。辨识结果表明:子空间跟踪算法可用于热模态辨识,有一定的工程应用价值。

关 键 词:子空间跟踪    热模态    模态试验    时变结构    模态参数辨识    新信息准则    飞行器    舵面结构
收稿时间:2017/10/13 0:00:00
修稿时间:2018/1/10 0:00:00

Application of Subspace Tracking Algorithm in Thermo-Mode Identification
ZHOU Haotian,ZHAO Jie,CAO Weizheng,SHI Xiaoming and YU Kaiping.Application of Subspace Tracking Algorithm in Thermo-Mode Identification[J].Aerospace Shanghai,2018(4):85-90.
Authors:ZHOU Haotian  ZHAO Jie  CAO Weizheng  SHI Xiaoming and YU Kaiping
Institution:School of Astronautics, Harbin Institute of Technology, Harbin 150001, Heilongjiang, China,School of Astronautics, Harbin Institute of Technology, Harbin 150001, Heilongjiang, China,College of Computer and Information Engineering, Heilongjiang University of Science and Technology, Harbin 150022, Heilongjiang, China,Shanghai Electromechanical Engineering Institute, Shanghai 201109, China and School of Astronautics, Harbin Institute of Technology, Harbin 150001, Heilongjiang, China
Abstract:The general procedure of modal parameter identification by use of subspace tracking algorithm is reviewed in this paper. A two degree-of-freedom spring-mass model with theoretical reference solution is simulated. In order to evaluate anti-noise abilities of different algorithms, the simulation acceleration responses with factitiously added random noise are used for identification. The identified results show that the anti-noise ability of subspace tracking algorithm based on novel information criterion (NIC) is better compared to other three methods. The thermo-modal test with controlled heating procedure for a rudder is carried out. The identification results show that the subspace tracking algorithm is suitable for thermo-modal analysis.
Keywords:subspace tracking  thermo-mode  modal test  time-varying structure  modal parameter identification  novel information criterion  flight vehicle  rudder structure
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