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MEMS惯组抗高g值冲击设计方法 被引量:10

Design method of MEMS IMU in high-g shock
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摘要 MEMS惯组以其体积小、成本低、可靠性高在强冲击环境中得到越来越广泛的应用。为解决基于石英微陀螺和硅微加速度计的MEMS惯组抗高g值冲击问题,提出了一种内减振抗冲击设计方法。在该设计方法中,将陀螺与加速度计嵌入式安装在对称六面体框架结构上,并通过粘接在六面体框架八个顶点的24块粘弹性阻尼减震器与惯组基体隔离,实现内减振。同时基于弹簧阻尼系统理论建立了MEMS惯组抗冲击等效数学模型,对模型进行了仿真分析。利用有限元分析软件ANSYS对三维结构模型进行了模态分析和冲击仿真分析,并通过结构扫频实验与9次5000g冲击谱试验进行了验证。仿真分析与试验结果证明了该方法的有效性及可行性。 MEMS IMU is used widely in high-g shock environment for its small volume, low cost and high reliability. MEMS IMU based on quartz gyro and silicon accelerometer need to be protected in high-g shock environment. To solve the anti-shock problem, an inner damping method is introduced. Gyros and accelerometers are embedded in the symmetrical hexahedron frame. The frame is isolated from IMU base by 24 viscoelastic damping materials felted on the frame culmination. Anti-shock math model is built and simulated based on spring-damper system theory. Mode analysis and shock spectrum response analysis of 3-D structure are simulated based on ANSYS finite element. Structure frequency experiment and nine 5000g SRS experiments are implemented. The result of simulation and experiment validate the effectiveness and feasibility of this method.
出处 《中国惯性技术学报》 EI CSCD 北大核心 2014年第3期404-408,共5页 Journal of Chinese Inertial Technology
基金 总装十二五预研项目(51309010401)
关键词 石英陀螺 MEMS惯组 弹簧阻尼系统 高G值 冲击 Accelerometers Damping Experiments Gyroscopes Interactive computer systems Mathematical models Quartz
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  • 1赵万祥,赵乃勤,郭新权.新型功能材料泡沫铝的研究进展[J].金属热处理,2004,29(6):7-11. 被引量:30
  • 2王佩瑶,唐洁影,余存江,恩云飞,师谦.MEMS微悬臂梁在冲击下的粘附失效预测[J].传感技术学报,2006,19(05A):1602-1605. 被引量:9
  • 3马爱娥,黄风雷,李金柱,武海军.钢筋混凝土抗贯穿数值模拟[J].北京理工大学学报,2007,27(2):103-107. 被引量:21
  • 4李莉,任茶仙,张铎.折叠翼机构展开动力学仿真及优化[J].强度与环境,2007,34(1):17-21. 被引量:41
  • 5钱立志.弹载任务设备抗高过载方法研究[J].兵工学报,2007,28(8):1017-1020. 被引量:27
  • 6Y Lee H K, C G Park. Adaptive redundant inertial measurement unit/global positioning system integration filter structure for fault tolerant navigation [ J ]. Journal of Dynamic Systems, Measure- ment, and Control, 2014,136(2) :021009.
  • 7J Cheng, et al. A Novel Optimal Configuration form Redundant MEMS Inertial Sensors Based on the Orthogonal Rotation Method. Sensors[J]. 2014,14(8) : 13661-13678.
  • 8S Habibi, et al. Gun hard inertial measurement unit based on MEMS capacitive accelerometer and rate sensor[ C]. Position, Lo- cation and Navigation Symposium, 2008 IEEE/ION. IEEE, 2008:232-237.
  • 9M Tanenhaus, et al. Miniature IMU/INS with optimally fused low drift MEMS gyro and accelerometers for applications in GPS-denied environments[ C ]. Position Location and Navigation Symposium (PLANS), 2012 IEEE/ION. IEEE, 2012: 259-264.
  • 10J P Gilmore, R AMeKern. A redundant strapdown inertial refer- ence unit (SIRU) [ J]. Journal of Spacecraft and Rockets, 1972,9 ( 1 ) : 39-47.

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