Sun Shan-Bin, He Yuan-Yuan, Zhou Si-Da, Yue Zhen-Jiang
School of Aerospace Engineering, Beijing Institute of Technology, Zhongguancun South Street 5, Beijing 100081, China.
Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China.
Sensors (Basel). 2017 Dec 12;17(12):2888. doi: 10.3390/s17122888.
Measurement of dynamic responses plays an important role in structural health monitoring, damage detection and other fields of research. However, in aerospace engineering, the physical sensors are limited in the operational conditions of spacecraft, due to the severe environment in outer space. This paper proposes a virtual sensor model with partial vibration measurements using a convolutional neural network. The transmissibility function is employed as prior knowledge. A four-layer neural network with two convolutional layers, one fully connected layer, and an output layer is proposed as the predicting model. Numerical examples of two different structural dynamic systems demonstrate the performance of the proposed approach. The excellence of the novel technique is further indicated using a simply supported beam experiment comparing to a modal-model-based virtual sensor, which uses modal parameters, such as mode shapes, for estimating the responses of the faulty sensors. The results show that the presented data-driven response virtual sensor technique can predict structural response with high accuracy.
动态响应的测量在结构健康监测、损伤检测及其他研究领域中发挥着重要作用。然而,在航空航天工程中,由于外层空间的恶劣环境,物理传感器在航天器的运行条件下受到限制。本文提出了一种使用卷积神经网络进行部分振动测量的虚拟传感器模型。传递函数被用作先验知识。提出了一种具有两个卷积层、一个全连接层和一个输出层的四层神经网络作为预测模型。两个不同结构动力系统的数值例子证明了所提方法的性能。通过与基于模态模型的虚拟传感器(该传感器使用模态参数,如振型,来估计故障传感器的响应)进行比较的简支梁实验,进一步表明了该新技术的优越性。结果表明,所提出的数据驱动响应虚拟传感器技术能够高精度地预测结构响应。