基于GPS的车辆跟踪系统动态评估有限元分析

S. Jog, P. Gupta, M. Sutaone, V. Badawe, A. Kumar, S. Gade, K. Deshpande
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引用次数: 1

摘要

介绍了在军用地面轮式车辆等苛刻环境下使用的基于GPS的车辆跟踪系统(VTS)的振动影响。本文还简要介绍了振动引起的失效以及振动试验方法的优点。利用CATIA软件建立了HE-30机壳GPS VTS板的几何模型,并利用ANSYS软件进行了应力水平仿真分析。ANSYS使用有限元分析工具模拟固有频率和应力水平。通过对HE-30机壳有无冲击支承的仿真得到了结果。将这些应力水平与极限抗拉强度进行比较,以确定该外壳是否能承受施加的振动。仿真结果表明,无冲击支承时的最大应力水平为30.8 MPa,有冲击支承时的最大应力水平为50 KPa。此外,HE-30外壳观察到的最大应力水平,有和没有冲击支架是远远低于310兆帕的极限抗拉强度。HE-30外壳符合JSS-55555 / MIL 810 E标准的兼容性要求。在HE-30外壳的GPS VTS板上进行了实际振动试验。功能测试结果令人满意,系统未出现机械损伤。
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Finite element analysis of GPS based vehicle tracking system with enclosure for dynamic assessment
This paper introduces vibration effects on the GPS based Vehicle Tracking System (VTS) to be used in stringent environment like ground based wheeled vehicles in Military applications. This paper also gives a brief idea of failures due to vibration and benefits of the vibration test method. The geometrical model for HE-30 Enclosure with GPS VTS board has been prepared using CATIA software and simulated for stress level analysis using ANSYS Software. ANSYS uses the Finite Element Analysis tool to simulate the natural frequencies and the stress level. The results were obtained through simulation of HE-30 Enclosure with and without shock mounts. These stress levels were compared with the Ultimate Tensile Strength to find out, whether this Enclosure would sustain the applied vibrations. The simulation results have indicated that the maximum stress level of 30.8 MPa for Enclosure without shock mounts has been reduced to 50 KPa for Enclosure with shock mounts. Also, the maximum stress level observed for HE-30 Enclosure, with and without shock mounts is much below the Ultimate Tensile Strength of 310 MPa. HE-30 Enclosure meets the compatibility requirements with JSS-55555 / MIL 810 E standards. The actual vibration test was conducted on GPS VTS board with HE-30 Enclosure. Functional test results were found to be satisfactory and no mechanical damage was observed in the system.
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