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加速度计加速退化机理一致性边界确定方法

王前程 陈云霞 邓沣鹂 康锐

王前程, 陈云霞, 邓沣鹂, 等 . 加速度计加速退化机理一致性边界确定方法[J]. 北京航空航天大学学报, 2012, (11): 1512-1516.
引用本文: 王前程, 陈云霞, 邓沣鹂, 等 . 加速度计加速退化机理一致性边界确定方法[J]. 北京航空航天大学学报, 2012, (11): 1512-1516.
Wang Qiancheng, Chen Yunxia, Deng Fengli, et al. Approach of determining accelerated degradation mechanism consistency’s boundary for accelerometers[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (11): 1512-1516. (in Chinese)
Citation: Wang Qiancheng, Chen Yunxia, Deng Fengli, et al. Approach of determining accelerated degradation mechanism consistency’s boundary for accelerometers[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (11): 1512-1516. (in Chinese)

加速度计加速退化机理一致性边界确定方法

详细信息
  • 中图分类号: V241.4

Approach of determining accelerated degradation mechanism consistency’s boundary for accelerometers

  • 摘要: 以加速退化模型——Arrhenius模型为研究对象,发现加速度计在加速试验过程中,保持加速机理不变的应力与退化轨迹斜率存在密切关系.通过针对退化轨迹模型分别为一次函数、指数函数和幂函数三种常见情况,从激活能不变角度推导出保证加速度计加速机理不变的应力-斜率公式,然后基于退化轨迹斜率区间检验提出了一种加速机理一致性条件确定方法,最后根据加速度计恒定高温标度因数稳定性退化仿真试验数据,准确得到了保持加速度计标度因数稳定性退化机理一致的应力边界,验证了该方法的可行性.

     

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出版历程
  • 收稿日期:  2011-06-21
  • 刊出日期:  2012-11-30

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