结合超疏水表面的柔性热差压传感器阵列,用于飞行参数估计。

IF 9.9 1区 工程技术 Q1 INSTRUMENTS & INSTRUMENTATION
Xin Ke, Yu Gao, Zheng Gong, Yunfan Li, Zihao Dong, Bowei Wan, Yurun Guo, Yonggang Jiang
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引用次数: 0

摘要

分布式压力传感器阵列是一种很有前途的小型无人机飞行参数估计方法。目前的柔性压力传感器阵列通常受到传感器分辨率的限制,弯曲灵活性差,包装保护不足,导致飞行参数估计精度不足。在这里,我们提出了一个高分辨率的差压传感器阵列,使用量热测量方法和多层聚酰亚胺键合技术。所提出的差压传感器阵列在500 Pa范围内的检测极限为36.5 mPa,并且在连接到不同曲面时具有很高的重复性。此外,超疏水封装集成到传感器制造过程中,赋予其防水能力。利用多层感知器神经网络,我们展示了传感器阵列在估计空速和攻角方面的功能,平均求解误差分别为0.15 m/s和0.37°。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Flexible calorimetric differential pressure sensor array integrated with a superhydrophobic surface for flight parameter estimation.

Distributed pressure sensor array is a promising approach for the estimation of flight parameters for small unmanned aerial vehicles. Current flexible pressure sensor arrays are conventionally subjected to limited sensor resolution, poor bending flexibility, and inadequate packaging protection, resulting in insufficient precision for flight parameter estimation. Here we present a high-resolution differential pressure sensor array using a calorimetric measurement method and a multilayer polyimide bonding technique. The proposed differential pressure sensor array reaches a detection limit of 36.5 mPa over a range of 500 Pa and shows high repeatability when attached to varying curved surfaces. In addition, a superhydrophobic packaging is integrated into the sensor fabrication process, endowing it with waterproof capability. Utilizing a multilayer perceptron neural network, we demonstrated the function of the sensor array in estimating airspeeds and angle of attacks, achieving average solving errors of 0.15 m/s and 0.37°, respectively.

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来源期刊
Microsystems & Nanoengineering
Microsystems & Nanoengineering Materials Science-Materials Science (miscellaneous)
CiteScore
12.00
自引率
3.80%
发文量
123
审稿时长
20 weeks
期刊介绍: Microsystems & Nanoengineering is a comprehensive online journal that focuses on the field of Micro and Nano Electro Mechanical Systems (MEMS and NEMS). It provides a platform for researchers to share their original research findings and review articles in this area. The journal covers a wide range of topics, from fundamental research to practical applications. Published by Springer Nature, in collaboration with the Aerospace Information Research Institute, Chinese Academy of Sciences, and with the support of the State Key Laboratory of Transducer Technology, it is an esteemed publication in the field. As an open access journal, it offers free access to its content, allowing readers from around the world to benefit from the latest developments in MEMS and NEMS.
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