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基于光纤张差场重建和规范计算的航天器细分损坏识别方法.
Jihong Xu1, Jie Zeng1, Binbin Chen1
1College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Sensors (Basel, Switzerland)
|November 14, 2023
概括
这项研究引入了一种新的算法,用于实时检测使用应变反应的航天器损伤. 该方法只使用工作负载准确地定位结构损伤,这对于健康监测至关重要.
科学领域:
- 航空航天工程 航空航天工程
- 结构健康监测 结构健康监测
- 材料科学 材料科学 材料科学
背景情况:
- 实时识别航天器损坏对于结构健康监测和预测运行寿命至关重要.
- 现有的方法难以仅通过应变反应分析来检测轻微的结构损伤.
研究的目的:
- 为实时开发算法,在线识别和精确定位航天器结构损坏.
- 为了克服仅使用应变反应数据检测小损伤的局限性.
主要方法:
- 提出了基于应变应答差异重建的损伤应答特征场逆转算法.
- 开发了使用矢量规范计算的四种裂损伤位置识别方法.
- 实施了一个航天器部分结构损坏监测系统,配有光纤格子传感器.
主要成果:
- 实现在线识别和精确定位结构损伤事件,仅使用航天器的工作负载,没有外部激发.
- 曲率向量2-规范计算方法的平均损伤定位误差为2.58毫米,平方根平均误差为1.98毫米.
结论:
- 开发的算法和方法证明了对轨道航天器服务环境的卓越工程适用性.
- 该方法通过准确的损伤检测,可以有效地监测结构健康状况和预测寿命.
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