期刊文献+
共找到3篇文章
< 1 >
每页显示 20 50 100
Unidirectionally Sensitive Flexible Resistance Strain Sensor Based on AgNWs/PDMS
1
作者 LIU Xinyue SUN Weiming +6 位作者 HE Mengfan FANG Yuan DJOULDE Aristide DLING Wei LIU Mei MENG Lingjun WANG Zhiming 《Journal of Shanghai Jiaotong university(Science)》 2025年第2期209-219,共11页
The fexible strain sensor has found widespread application due to its excellent fexibility,extensibility,and adaptability to various scenarios.This type of sensors face challenges in direction identification owing to ... The fexible strain sensor has found widespread application due to its excellent fexibility,extensibility,and adaptability to various scenarios.This type of sensors face challenges in direction identification owing to strong coupling between the principal strain and transverse resistance.In this study,a silver nanowires(Ag-NWs)/polydimethylsiloxane(PDMS)strain sensor was developed,using a filtration method for preparing the AgNWs film which was then combined with PDMS to create a unidirectional,highly sensitive,fast-responsive,and linear fexible strain sensor.When the grid width is 0.25 mm,the AgNWs/PDMS strain sensor demonstrates an outstanding unidirectional sensitivity,with a strain response solely along the parallel direction of the grid lines(noise ratioα≈8%),and a fast reaction time of roughly 106.99 ms.In the end,this sensor's ability to detect curvature was also demonstrated through LEDs,demonstrating its potential applications in various fields,including automotive,medical,and wearable devices. 展开更多
关键词 fexible strain sensor silver nanowires(AgNWs) polydimethylsiloxane(PDMS) unidirectional sensitivity
原文传递
Symplectic Analysis on Coupling Behaviors of Spatial Fiexible Damping Beam
2
作者 Weipeng Hu Xiaojian Xi +3 位作者 Zhe Zhai Pengfei Cui Fan Zhang Zichen Deng 《Acta Mechanica Solida Sinica》 SCIE EI CSCD 2022年第4期541-551,共11页
Although the complex structure-preserving method presented in our previous studies can be used to investigate the orbit–attitude–vibration coupled dynamic behaviors of the spatial flexible damping beam,the simulatio... Although the complex structure-preserving method presented in our previous studies can be used to investigate the orbit–attitude–vibration coupled dynamic behaviors of the spatial flexible damping beam,the simulation speed still needs to be improved.In this paper,the infinite-dimensional dynamic model describing the orbit–attitude–vibration coupled dynamic problem of the spatial flexible damping beam is pretreated by the method of separation of variables,and the second-level fourth-order symplectic Runge–Kutta scheme is constructed to investigate the coupling dynamic behaviors of the spatial flexible damping beam quickly.Compared with the simulation speed of the complex structure-preserving method,the simulation speed of the symplectic Runge–Kutta method is faster,which benefits from the pretreatment step.The effect of the initial radial velocity on the transverse vibration as well as on the attitude evolution of the spatial flexible damping beam is presented in the numerical examples.From the numerical results about the effect of the initial radial velocity,it can be found that the appearance of the initial radial velocity can decrease the vibration frequency of the spatial beam and shorten the evolution interval for the attitude angle to tend towards a stable value significantly.In addition,the validity of the numerical results reported in this paper is verified by comparing with some numerical results presented in our previous studies. 展开更多
关键词 Symplectic Runge-Kutta method Spatial fexible damping beam Orbit-attitudevibration coupled dynamic behavior Structure-preserving
原文传递
Autonomous Recon-guration Strategy Based on Recon-gurability Evaluation
3
作者 Heyu Xu Wenbo Li +1 位作者 Kebei Zhang Fangzhou Fu 《Guidance, Navigation and Control》 2021年第3期98-114,共17页
This paper aims to improve the autonomous operational capabilities of spacecraft.For a complex system with physical coupling and flexible attachments,an autonomous reconfigura-tion strategy based on reconfigurability ... This paper aims to improve the autonomous operational capabilities of spacecraft.For a complex system with physical coupling and flexible attachments,an autonomous reconfigura-tion strategy based on reconfigurability evaluation is proposed.First,a quantitative evaluation index for reconfigurability is given based on operator theory to fully exploit the potential of system reconfigurability under resource constraints.Then,specific requirements and evaluation methods for autonomous reconfiguration are proposed in accordance with the results,thereby providing a theoretical reference for the design of reconfiguration strategy methods.Thus,reconfigurability is maximized from the design point of view.Finally,the validity and cor-rectness of the method are verified by simulation. 展开更多
关键词 Reconfgurability reoonfguration stral egy physical coupling fexible altachments
在线阅读 下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部