首页> 外文会议>AIAA infotech@aerospace conference;AIAA Sci'Tech forum >Acceleration and Velocity Sensing from Measured Strain
【24h】

Acceleration and Velocity Sensing from Measured Strain

机译:根据测得的应变进行加速度和速度传感

获取原文

摘要

A simple approach for computing acceleration and velocity of a structure from the strain is proposed in this study. First, deflection and slope of the structure are computed from the strain using a two-step theory. Frequencies of the structure are computed from the time histories of strain using a parameter estimation technique together with an autoregressive moving average model. From deflection, slope, and frequencies of the structure, acceleration and velocity of the structure can be obtained using the proposed approach. Simple harmonic motion is assumed for the acceleration computations, and the central difference equation with a linear autoregressive model is used for the computations of velocity. A cantilevered rectangular wing model is used to validate the simple approach. Quality of the computed deflection, acceleration, and velocity values are independent of the number of fibers. The central difference equation with a linear autoregressive model proposed in this study follows the target response with reasonable accuracy. Therefore, the handicap of the backward difference equation, phase shift, is successfully overcome.
机译:这项研究提出了一种简单的方法来从应变计算结构的加速度和速度。首先,使用两步理论从应变计算结构的挠度和斜率。使用参数估计技术和自回归移动平均模型,根据应变的时间历史记录来计算结构的频率。根据结构的挠度,斜率和频率,可以使用所提出的方法获得结构的加速度和速度。假定简单的谐波运动进行加速度计算,并且使用具有线性自回归模型的中心差分方程式进行速度计算。悬臂矩形翼模型用于验证这种简单方法。计算的挠度,加速度和速度值的质量与纤维的数量无关。在这项研究中提出的带有线性自回归模型的中心差分方程遵循目标响应,具有合理的精度。因此,成功克服了后向差分方程相移的障碍。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号