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Distributed measurement system based on CAN data bus

机译:基于CAN数据总线的分布式测量系统

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Purpose This paper aims to describe the idea behind and design of a miniaturized distributed measurement system based on a controller area network (CAN) data bus.Design/methodology/approach The intention of the designers was to build a light and modular measurement system which can be used in remotely piloted aircraft systems and ultra-light aircraft during flight tests, as well as normal operation. The structure of this distributed measurement system is based on a CAN data bus. The CAN aerospace standard has been applied to the software as well as the hardware comprising this system. PRP-W2 software designed for PCs is an additional component of the proposed measurement system. This software supports data acquisition from a recorder unit and allows for preliminary data analysis, as well as data conversion and presentation.Findings The system, complete with a high-speed data recorder, was successfully installed on board of an MP-02 Czajka aircraft. A research experiment using the system and oriented on airframe high frequency vibration analysis is presented in the final part of this paper.Research limitations/implications This measurement system allows analysis of high-frequency vibrations occurring at selected points of the aircraft. A data set is recorded by three-axis accelerometers and gyroscopes at frequencies up to 1 kHz.Practical implications The use of a miniature and lightweight modular measurement system will, in many cases, be faster and less expensive than full-scale measurement and data acquisition systems, which often require a lengthy assembly process. The implementation of this class of lightweight flight test systems has many advantages, in particular to the operation of small aircraft. Such solutions are likely to become increasingly common in unmanned aerial vehicles and in other light aircraft in the future.Originality/value The adaptation of a distributed measuring system with a high frequency of measurements for purposes of small and miniature aircraft.
机译:目的本文旨在描述基于控制器局域网(CAN)数据总线的小型分布式测量系统的思想和设计。设计/方法/方法设计者的目的是构建一种轻便的模块化测量系统,该系统可以在飞行测试以及正常运行期间,可用于远程驾驶飞机系统和超轻型飞机。该分布式测量系统的结构基于CAN数据总线。 CAN航空航天标准已应用于构成该系统的软件以及硬件。专为PC设计的PRP-W2软件是建议的测量系统的附加组件。该软件支持从记录仪单元获取数据,并允许进行初步数据分析以及数据转换和演示。发现该系统已配备高速数据记录仪,已成功安装在MP-02 Czajka飞机上。本文的最后部分提出了使用该系统并针对机身进行高频振动分析的研究实验。研究局限/意义该测量系统可以分析飞机选定点处发生的高频振动。三轴加速度计和陀螺仪以高达1 kHz的频率记录数据集。实践意义在许多情况下,比起全面的测量和数据采集,使用微型轻巧的模块化测量系统将更快,更便宜。系统,这通常需要漫长的组装过程。这类轻型飞行测试系统的实施具有许多优势,特别是在小型飞机的操作方面。这样的解决方案将来可能会在无人驾驶飞机和其他轻型飞机中变得越来越普遍。原创性/价值为了小型和微型飞机的目的,对具有高测量频率的分布式测量系统进行了改进。

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