Construction of virtual vibration testing platform for spacecraft

LIU Yuan; DONG Li-Min; KONG Xian-ren; WANG Ri-kun; LI Sen-sheng

doi:10.3788/OPE.20132105.1258

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Construction of virtual vibration testing platform for spacecraft

更新时间：2020-08-12

- Construction of virtual vibration testing platform for spacecraft
- Optics and Precision Engineering Vol. 21, Issue 5, Pages: 1258-1264(2013)
- 作者机构：
  
  哈尔滨工业大学航天学院2. 上海航天卫星总装试验部
- 作者简介：
- 基金信息：
- DOI：10.3788/OPE.20132105.1258
  CLC： V416.2
- Received：18 November 2012，
  
  Revised：04 January 2013，
  
  Published Online：24 May 2013，
  
  Published：15 May 2013
- 稿件说明：
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刘源董立珉孔宪仁王日昆李霖圣. 飞行器虚拟振动试验平台构建[J]. 光学精密工程, 2013,21(5): 1258-1264

LIU Yuan DONG Li-Min KONG Xian-ren WANG Ri-kun LI Sen-sheng. Construction of virtual vibration testing platform for spacecraft[J]. Editorial Office of Optics and Precision Engineering, 2013,21(5): 1258-1264
刘源董立珉孔宪仁王日昆李霖圣. 飞行器虚拟振动试验平台构建[J]. 光学精密工程, 2013,21(5): 1258-1264 DOI： 10.3788/OPE.20132105.1258.

LIU Yuan DONG Li-Min KONG Xian-ren WANG Ri-kun LI Sen-sheng. Construction of virtual vibration testing platform for spacecraft[J]. Editorial Office of Optics and Precision Engineering, 2013,21(5): 1258-1264 DOI： 10.3788/OPE.20132105.1258.

摘要

针对用振动台进行飞行器振动环境试验时存在试验周期长、耗费高及易发生过试验或欠试验等问题，采用虚拟现实技术建立了飞行器虚拟振动试验平台。采用系统仿真软件LMS AMESim建立了电振动台正弦振动控制仪模型；通过多学科系统仿真软件LMS Virtual.Lab建立了振动台的多体系统动力学模型，进行了振动台多体动力学模型与电磁作动系统模型的机电联合仿真；实现了振动控制系统、电磁作动系统、振动台与试件机械系统的闭环仿真，构建了飞行器虚拟振动试验平台。利用该虚拟振动试验平台系统进行了盒式试件的正弦振动试验。结果表明，采用机电耦合建模方法构建的虚拟振动试验平台综合考虑了试件、振动台机械系统、控制系统及电气系统的耦合效应，可为飞行器的试前分析和虚拟振动试验提供试验环境。

Abstract

As the spacecraft vibration testing based on a shaking table has some defects

such as long time cycle

high cost

easy to produce overtesting and undertesting

a virtual vibration testing platform was built based on virtual reality technology. A sine vibration controller model of the electrical vibration table was built by system simulation software LMS AMESim and a multibody model for the vibration table was established based on the multibody simulation software LMS Virtual.Lab Motion. Furthermore

the model of electromagnetic actuator in the vibration testing system was realized using the simulation software LMS AMESim

and the cosimulation of vibration testing system was carried out by uniting the multibody model and LMS AMESim model. In combination of the vibration control system

electromagnetic actuation system and shaking table test mechanical system

the whole virtual vibration test system was implemented. Finally

a virtual sine vibration test for a box &thin specimen was performed by using the proposed system. Test results show that the virtual vibration testing platform based on the electrical and mechanical coupling modeling method can provide test environments for test analysis and virtual vibration test because it considers the coupling effect of the testpiece and the electrical vibration table.

关键词

Keywords

references

柯受全. 卫星环境工程和模拟试验 \[M\]. 北京：中国宇航出版社，1996：23-27.KE SH Q. Satellite Environment Engineering and Simulation Test \[M\]. BeiJing: China's Space Press, 1996: 23-27. (in Chinese)[2]蒋明, 何小元. 振动轮式微机械陀螺动态特性的光学测试 \[J\]. 光学精密工程, 2008, 16(2): 295-299.JIANG M, HE X Y. Optical testing of dynamic characteristic of vibrating wheel micromechanical gyroscope \[J\]. Opt. Precision Eng., 2008, 16(2): 295-299. (in Chinese)[3]贾学志, 王栋, 张雷, 等. 轻型空间相机调焦机构的优化设计与精度试验\[J\]. 光学精密工程, 2011, 19(8): 1824-1831.JIA X ZH, WANG D, ZHANG L, et al.. Optimizing design and precision experiment of focusing mechanism in lightweight space camera \[J\]. Opt. Precision Eng., 2011, 19(8): 1824-1831. (in Chinese)[4]向树红, 于丹, 晏廷飞, 等. 卫星动力学虚拟试验的几个关键技术 \[J\]. 航天器环境工程, 2002(4): 13-22. XIANG SH H, YU D, YAN T F, et al.. Some key techniques of dynamic virtual test for safellites \[J\]. Spacecraft Environment Engineering, 2002(4): 13-22. (in Chinese) [5]RICCI S, PEETERS B, DEBILLE J, et al.. Virtual shaker testing: A novel approach for improving vibration test performance \[C\]. International Conference on Noise and Vibration Engineering, Leuven: Katholieke University Leuven, 2008: 1767-1782.[6]RICCI S, PEETERS B. Virtual shaker testing for predicting and improving vibration test performance \[C\]. Proceedings of the IMAC-XXVII, Orlando, 2009: 1-16.[7]BETTS E J, VANSANT K, PAULSON C, et al.. Smart testing using virtual vibration testing \[C\]. Proceedings of the 24th Aerospace Testing Seminar (ATS), Manhattan Beach, 2008: 103-111.[8]APPOLLONI M, COZZANI A. Use of advanced integrated CAE tools to provide an end-to-end simulation of payload testing on Hydra \[C\]. Proceedings of Seminar on Integrated open CAD/CAE Platforms for Mechanical Engineering, Noordwijk, 2005: 579-591.[9]KLENKE S E, BACA T. Structural dynamics test simulation and optimization for aerospace components \[C\]. Proceedings of the Second Test and Evaluation International Aerospace Forum, Washington, 1996:82-89.[10]KLENKE S E, LAUFFER J P, GREGORY D L, et al.. The Vibration Virtual Environment for Test Optimization \[M\]. New Mexico: S. V. Symp, 1996: 67-76.[11]KLENKE S E, REESE G M, SCHOOF L A, et al.. Modal test optimization using VETO (Virtual Environment for Test Optimization) \[R\]. Sandia: Sandia Report SAND95-2591, 1996: 1-7.[12]向树红, 晏廷飞, 邱吉宝. 40吨振动台虚拟试验仿真技术研究 \[J\]. 宇航学报, 2004, 25(4): 375-381.XIANG SH H,YAN T F, QIU J B. Research on the computer simulate technology of vibration virtual environment for test about 40 t shaker \[J\]. Journal of Astronautics, 2004, 25(4) : 375-381. (in Chinese)[13]邱吉宝, 王建民. 航天器虚拟动态试验技术研究及展望 \[J\]. 航天器环境工程，2007，24(1): 1-14.QIU J B, WANG J M. A review on virtual dynamic test techniques for space vehicles \[J\]. Spacecraft Environment Engineering, 2007, 24(1):1-14. (in Chinese)[14]陈家焱, 王海东, 周建川, 等. 多点激励振动试验控制技术进展 \[J\]. 振动与冲击，2011, 30(3): 69-73.CHEN J Y, WANG H D, ZHOU J CH, et al.. Progress in multi-exciter vibration testing control technology \[J\]. Journal of Vibration and Shock, 2011，30(3): 69-73.

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