一种基于模板匹配的蜂窝结构板撞击定位方法及装置

By combining template matching and neural networks, the problem of accurate impact positioning of cellular structure panels under extreme high and low temperatures was solved, realizing accurate impact positioning of spacecraft cellular structure panels and improving signal quality and positioning accuracy.

CN121144864BActive Publication Date: 2026-07-17AEROSPACE DONGFANGHONG SATELLITE

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
AEROSPACE DONGFANGHONG SATELLITE
Filing Date
2025-08-14
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies struggle to accurately monitor multi-point strain and pressure parameters of spacecraft honeycomb structure panels under extreme high and low temperatures, especially given the inhomogeneity within the honeycomb structure, making precise impact positioning difficult.

Method used

A template matching-based approach is adopted. By collecting FBG sensor signals after a simulated impact on a cellular structure panel, a feature library is established, signal feature extraction and template matching are performed, and combined with a neural network method, feature comparison and weighted averaging of real-time impact signals are realized to determine the global impact location.

Benefits of technology

It achieves precise impact positioning of cellular structure panels, improves signal quality and positioning accuracy, and can adapt to sensor failure and structural changes in complex environments, thereby improving positioning coverage and accuracy.

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Abstract

本发明提供了一种基于模板匹配的蜂窝结构板撞击定位方法及装置,包括:采集蜂窝结构板模拟撞击后的多个FBG传感器信号,对信号进行特征提取并建立特征库;获取实时撞击的多个传感器信号,对信号进行特征提取;采用模板匹配方法将实时撞击的各传感器信号的信号特征与特征库中的信号特征进行逐一比较,确定特征库中最相似的信号特征作为该传感器信号的模板匹配结果;将各传感器信号的模板匹配结果加权平均确定全局冲击位置,获得模板匹配预测的撞击位置。本发明提供的适用于蜂窝结构板的撞击定位方法,定位精度高,对航天器结构的安全监测具有重要意义。
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