一种用于航空航天应用的灵活数据采集系统

A. V. Radogna, S. Capone, L. Francioso, P. Siciliano, S. D’Amico
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引用次数: 0

摘要

提出了一种面向航天应用的柔性数据采集系统。该系统能够从电阻式、电容式和数字/脉冲输出传感器获取原始信号。在读出能力的灵活性是可能的,这要归功于:(1)采用集成模拟前端(AFE)电路的通用接口的电阻和电容传感器;(2)对所有连接的传感器采用相同的时间-数字转换方法。AFE通过产生方波来实现电阻/电容与时间的转换,其周期与电阻或电容值成正比。时间到数字的转换是由一个通用的微控制器板的定时器外设,从而避免了模数转换器(ADC)。提出了所提出的数据采集系统的体系结构,并详细介绍了AFE电路的设计,重点介绍了每次测量能量(EpM)性能。作为工作实例,制作了一个带有两个NTC热敏电阻和一个霍尔效应传感器的演示器,并给出了测量结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Flexible Data Acquisition System for Aerospace Applications
This paper presents a flexible data acquisition (DAQ) system targeted to aerospace applications. The system is able to acquire raw signals from resistive, capacitive and digital/pulsed output sensors. The flexibility in the read-out capability is made possible thanks to: (1) the adoption of an integrated analog front-end (AFE) circuit for the generic interfacing of resistive and capacitive sensors; (2) the adoption of the same time-to-digital conversion approach for all the connected sensors. The AFE implements the resistance/capacitance-to-time conversion by generating a square wave, whose period is proportional to resistance or capacitance values. The time-to-digital conversion is made by the timer peripheral of a generic microcontroller board, thus avoiding the analog-to-digital converter (ADC). The architecture of the proposed DAQ system is presented and the design of the AFE circuit is detailed with emphasis on the energy-per-measurement (EpM) performance. As an example of operation, a demonstrator with two NTC thermistors and an Hall effect sensor, is made and measurement results are shown.
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