首页> 外国专利> SMART AIRCRAFT SKIN IMPACT AREA POSITIONING METHOD BASED ON TRUNCATED REVERSE WEIGHTED SUM

SMART AIRCRAFT SKIN IMPACT AREA POSITIONING METHOD BASED ON TRUNCATED REVERSE WEIGHTED SUM

机译:基于截断逆加权和的智能飞机皮肤碰撞区域定位方法

摘要

A smart aircraft skin impact area positioning method based on a truncated reverse weighted sum, belonging to the technical fields of smart aerospace structures and health monitoring. Piezoelectric sensor arrays are arranged in a smart aircraft skin structure and are connected to multiple impact area monitoring systems. After each impact area monitoring system obtains a digital sequence generated by an impact, the method comprises: first truncating the digital sequence as characteristic digital sequences, calculating reverse weighted values of the characteristic digital sequences, then a monitoring center calculating, according to piezoelectric sensors constituting impact monitoring sub-areas, a reverse weighted sum of each impact monitoring sub-area, and finally determining the impact monitoring sub-area having the maximum reverse weighted sum as an area where the impact occurs. The method is simple, has high accuracy of impact area positioning, facilitates realizing embedded programming, and can solve the problem of a positioning conflict during networked monitoring of multiple impact area monitoring systems and the problem of the difficulty in accurately positioning a middle area.
机译:一种基于截尾反加权和的智能飞机皮肤撞击区域定位方法,属于智能航空航天结构和健康监测技术领域。压电传感器阵列布置在智能飞机的蒙皮结构中,并连接到多个撞击区域监视系统。在每个撞击区域监控系统获得撞击产生的数字序列后,该方法包括:首先将数字序列截断为特征数字序列,计算特征数字序列的反向加权值,然后由监控中心根据构成的压电传感器进行计算。冲击监测子区域,每个冲击监测子区域的反向加权总和,最后确定具有最大反向加权和的冲击监测子区域作为发生冲击的区域。该方法简单,影响区定位精度高,便于实现嵌入式编程,可以解决多个影响区监控系统联网监测过程中的定位冲突问题和中间区定位困难的问题。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

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