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基于位移峰值信息的实时自适应分段速度估算方法
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作者 陆熊 宋爱国 《宇航学报》 EI CAS CSCD 北大核心 2007年第6期1740-1746,共7页
力/触觉再现技术是遥操作、飞行器仿真培训以及增强型虚拟现实等系统的有益补充。准确度高、噪声低且计算快速的速度估算是确保高效力/触觉再现系统实现的重要环节之一。从位移数据峰值信息出发,提出了一种自适应分段速度估算方法。相... 力/触觉再现技术是遥操作、飞行器仿真培训以及增强型虚拟现实等系统的有益补充。准确度高、噪声低且计算快速的速度估算是确保高效力/触觉再现系统实现的重要环节之一。从位移数据峰值信息出发,提出了一种自适应分段速度估算方法。相对现有的有限步长差分法在采样率较高时容易引入噪声分量和自适应回溯窗法在低速运动时需要较长计算时间等缺点,自适应分段法在确保估算准确度和光滑度的基础上同时具备计算快速的特性,从而能够满足力/触觉再现技术所需的准确性和实时性要求。文章最后建立了力/触觉再现实验系统,通过实验验证了该速度估算方法的有效性和快速性。 展开更多
关键词 速度估算 计算时间 估算准确度 自适应分段法 力/触觉再现
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The Accuracy of Characteristic Length Method on Failure Prediction of Composite Pinned Joints
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作者 Olanrewaju Aluko Quamrul Mazumder 《Journal of Mechanics Engineering and Automation》 2011年第3期200-210,共11页
A two-dimensioual stress analysis was developed to evaluate the failure of composite joints using characteristic length method. In this study, the accuracy of characteristic length method on the prediction of failure ... A two-dimensioual stress analysis was developed to evaluate the failure of composite joints using characteristic length method. In this study, the accuracy of characteristic length method on the prediction of failure strength and failure mode using different failure criteria was investigated. The stresses required for evaluating the joints were computed from stress functions obtained from displacement expressions that satisfy boundary conditions of the hole. The available experimental data for joint strength in literature were compared with the predicted failure loads and modes of failure for different composite pinned joints. No single failure criterion utilized to evaluate the failure gave a universally best fit across the three joints evaluated. However, the accuracy of characterizing the joints failure varies with joint laminate and choice of failure criterions. 展开更多
关键词 Failure criterions characteristic length evaluate and joint strength.
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