Design and tests for a space camera support structure under random vibration responses
LI Lin1,2,WANG Dong1,3,KONG Lin1,3,TAN Luyang1,2,YANG Hongbo1
1.Changchun Institute of Optics,Fine Machinery and Physics,University of Chinese Academy of Sciences,Changchun 130033,China;
2.University of Chinese Academy of Sciences,Beijing 100039,China;
3.Chang Guang Satellite Technology Ltd.,Changchun 130033,China
In order to solve the problem of too large random vibration acceleration response of a high resolution space camera,the main support structure of the space camera was designed optimally.Firstly,the mechanical model was established based on the random vibration response analysis,and the random vibration root-mean-square response expression was deduced.Then,the camera supporting structure was designed based on the principles of the three-point locationing and the bipod flexible structure.With an objective function of minimizing the acceleration response RMS of the installing point of the camera and the fundamental natural frequency of the structure as a constraint,the optimal model for the random vibration response fo the camera support structure was built.The position of its flexible link was optimized.Using the FE software MSC.Patran & Nastran,the engineering analysis was done for the optimized camera support structure.The results showed that the maximum camera installation point random acceleration response RMS value is 19.6 grms.Finally,the camera support structure was tested with random vibration tests.The results showed that the maximum relative error between analysis results and test results is 8.2%; the designed camera support structure can meet the service requirements of the space camera,the feasibility of the proposed optimization method is verified.
李林1,2, 王栋1,3,孔林1,3,谭陆洋1,2,杨洪波1. 随机振动响应下空间相机支撑结构设计与试验[J]. 振动与冲击, 2017, 36(7): 208-212.
LI Lin1,2,WANG Dong1,3,KONG Lin1,3,TAN Luyang1,2,YANG Hongbo1. Design and tests for a space camera support structure under random vibration responses. JOURNAL OF VIBRATION AND SHOCK, 2017, 36(7): 208-212.
[1] 毛国斌.某航天器姿态控制机组随机振动响应分析[J].上海航天,2007,3:54-57.
MAO Guo-bin. Random Vibration Response Prediction of Some Spacecraft Attitude-Control Thruster Set[J]. AEROS PACE SHANGHAI,2007,3:54-57.(in Chinese)
[2] 张军,谌勇,张志谊,等.卫星随机试验的振动响应分析[J].机械强度,2006,28(1):016-019.
ZHANG Jun, CHEN Yong, ZHANG Zhi-yi, et al. Research on the random vibration test of the satellite[J]. Journal of Mechanical Strength, 2006,28(1):016-019. (in Chinese)
[3] 杨新峰,赵志明,邓卫华,等.小卫星随机振动特性分析与试验验证方法探讨[J].航天器环境工程,2014,31(4):357-362.
Yang Xin-feng, Zhao Zhi-ming, Deng Wei-hua, et al. Random vibrations of small satellites and the testing method[J]. SPACECRAFT ENVIRONMENT ENGINEERING, 2014,31(4):357-362. (in Chinese)
[4] 张玉梅,韩增尧,邹元杰.航天器随机振动设计载荷有限频段法研究[J].航天器工程,2013,22(1):49-52.
ZHANG Yu-mei, HAN Zeng-yao, ZUO Yuan-jie. Research on limited frequency bandwidth method of spacecraft design load for random vibration[J].SPACECRAFT ENGINEERING, 2013,22(1):49-52. (in Chinese)
[5] 陈志敏,朱海潮,匡贡献.基于二阶循环统计量的近场声全息试验研究[J].振动与冲击,2011,30(9):202-206.
CHEN Zhi-min, ZHU Hai-chao, KUANG Gong-xian. Experimental study on near-field acoustic holography based on the second-order cyclic statistics[J]. JOURNAL OF VIBARATION AND SHOCK, 2011,30(9):202-206. (in Chinese)
[6] 盛骤,谢式千,潘承毅.概率论与数理统计(第3 版)[M] .北京:高等教育出版社,2001.
SHENG Zhou,XIE Shi-qian, PAN Cheng-yi .Probability and Mathematical Statistics(3rd Edition)[M]. Beijing :Higher Education Press , 2001 .(in Chinese)
[7] 田利思,李相辉,马越峰,等. MSC Nastran 动力学分析指南[M]. 北京:中国水利水电出版社,2012.
TIAN Li-si, LI Xiang-hui, MA Yue-feng, et al. MSC Nastran enchiridion of dynamic analysis[M]. Beijing: China water conservancy and hydropower Press, 2012. (in Chinese)
[8] 王忠素,翟岩,梅贵,等.空间光学遥感器反射镜柔性支撑的设计[J].光学精密工程,2010,18(8):1833-1840.
WANG Zhong-su, ZHAI Yan, MEI Gui, et al. Design of flexible support structure of reflector in space remote sensor[ J]. Op t. Precision Eng , 2010, 18( 8) : 1833-1840. ( in Chinese)
[9] 闫勇, 贾继强, 金光. 新型轻质大口径空间反射镜支撑设计[J].光学精密工程, 2008, 16(8): 1533-1539.
YAN Yong, JIA Ji-guang, JIN Guang. Design of new type space borne light weighted primary mirror support[ J]. Op t. Precision Eng, 2008, 16( 8): 1533-1539. ( in Chinese)
[10] 王辉.极紫外光刻系统物镜光学元件的支撑与分析[J].中国光学与应用光学,2010,3(6):598-604.
WANG Hui. Objective optical mounts and analysis for EUVL[J]. Chinese Journal of Optics and Applied Optics, 2010,3(6):598-604.
[11] 崔永鹏,何欣.遥感仪器光学系统用非球面反射镜的支撑结构设计[J].红外, 2013, 34(10): 16-19.
CUI Yong-peng, HE xin. Design of support for aspheric mirror used in remote sensor[J]. INFRARED, 2013, 34(10): 16-19.
[12] 鲁亚飞,范大鹏,范世珣,等.快速反射镜两轴柔性支承设计[J].光学精密工程,2010,18 ( 12 ) :2574-2582.
LU Ya-fei,FAN Da-peng,FAN Shi-xun,et al.Design of two axis elastic support for fast steering mirror[J]. Opt.Precision Eng.2010,18(12): 2574-2582.( in Chinese)