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Fault-tolerant parallel six-component force sensor

机译:容错并联六分量力传感器

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摘要

During some key force measuring tasks in the harsh environment such as aerospace, national defense, deep-sea exploration, higher working reliability is required. The design concept of fault-tolerance is proposed in the design of parallel six-component force sensor. Two kinds of fault-tolerant parallel structure force sensor without pre-stressing platform and two kinds of fault-tolerant and fully pre-stressed parallel structure force sensor using modified spherical pairs, together with another three kinds of wheel-spoke fault-tolerant force sensor are proposed. Compared with traditional Stewart platform-based sensor, the structural characteristics of the sensors are analyzed. The complete mathematic models including the models before and after signal fault are established by using theory of screw and the relations between stiffness and force distribution. The unified mathematic model is suitable for all the fault-tolerant six-component force sensor with different structures proposed in this paper. Calibration study of a sensor prototype without fault and with signal fault is carried out and non-linear errors are analyzed. The research of the paper provides not only theoretical basis and practical significance for the study on high reliable six-component force sensor, but also a new applied orientation for the redundant parallel mechanism.
机译:在诸如航空航天,国防,深海勘探等恶劣环境中进行某些关键力测量任务时,要求更高的工作可靠性。在并联六分量力传感器的设计中提出了容错的设计思想。两种不带预应力平台的容错并联结构力传感器,以及两种使用改进的球形对的容错和完全预应力的并联结构力传感器,以及另外三种轮辐式容错力传感器被提议。与传统的基于Stewart平台的传感器相比,分析了传感器的结构特征。利用螺钉理论以及刚度与力分布之间的关系,建立了包括信号故障前后模型在内的完整数学模型。本文提出的统一数学模型适用于所有具有不同结构的容错六分量力传感器。进行了无故障和有信号故障的传感器原型的校准研究,并分析了非线性误差。本文的研究不仅为高可靠的六分量力传感器的研究提供了理论依据和实践意义,而且为冗余并联机构的应用提供了新的方向。

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