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火箭结构系统纵向模态自动辨识方法

AN AUTOMATIC IDENTIFICATION METHOD FOR LONGITUDINAL MODES OF STRUCTURAL SYSTEM OF ROCKET

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【作者】 方勃唐冶杨飞虎张业伟臧健

【Author】 Fang Bo;Tang Ye;Yang Feihu;Zhang Yewei;Zang Jian;School of Astronautics,Harbin Institute of Technology;China Department of Astronautics,Shenyang Aerospace University;Beijing Institute of Structure and Environment Engineering;Shanghai Institute of Applied Mathematics and Mechanics;

【机构】 哈尔滨工业大学航天学院沈阳航空航天大学航空航天工程学部北京环境强度研究所上海大学上海市应用数学和力学研究所

【摘要】 针对工程中需要从火箭结构系统的整体模态中识别纵向模态,根据模态有效质量理论,提出了一种识别火箭结构系统纵向模态的自动辨识方法.以具有集中质量系统的振动特性作为算例,通过有限元软件,建立了具有集中质量系统的梁模型,利用自动辨识的方法,自动辨识出系统的纵向模态,并与应用模态分析法所计算的系统模态信息相比较,这种自动辨识方法不仅能准确的辨识出振动系统的纵向模态,而且还具有自动高效的识别特点.为准确快速建立液体火箭POGO振动系统的动力学模型等工程系统的模型提供理论依据.

【Abstract】 Aiming at the problem that the longitudinal modes of structural system of rocket need to be identified from its integral modes in engineering,a method that automatically identifies the longitudinal modes of structural system of rocket was proposed according to the theory of modal effective mass. Taking the vibration characteristics of system with lumped mass as a computing example,applying the finite element software,the beam model of system with lumped mass was established,and the longitudinal modes of the system were automatically identified based on the method. Compared with the system modal information calculated by the method of modal analysis,this automatic identification method not only can accurately identify the longitudinal modes of vibrating system,but also has automatic and high efficiency identification feature. It provides a theoretical basis for the dynamic model of POGO vibrating system in liquid rockets and other model of engineering systems to be accurately and promptly established.

【基金】 国家自然科学基金资助项目(11202140)~~
  • 【文献出处】 动力学与控制学报 ,Journal of Dynamics and Control , 编辑部邮箱 ,2014年03期
  • 【分类号】V414
  • 【被引频次】1
  • 【下载频次】124
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