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基于ARM的无人机真空速测量系统设计
引用本文:李超,严家明,刘松林.基于ARM的无人机真空速测量系统设计[J].电子技术应用,2012,38(10).
作者姓名:李超  严家明  刘松林
作者单位:西北工业大学电子信息学院,陕西西安,710129
摘    要:设计了以ARM微处理器为核心的中央控制处理单元,用于无人机真空速测量系统中。通过公式分解,并采用线性低次插值算法,有效解决了真空速解算公式复杂的缺点;同时利用ARM的UART串口总线,实现了传感器输出特性曲线、真空速的上位机实时显示,使系统相对误差控制在2.5%以内。测试结果证明了该系统具有良好的实效性和稳定性、精度高,优于传统的测量装置。

关 键 词:ARM  指示空速  真空速  压力传感器  线性插值

Design of airspeed measuring system for the unmanned aerial vehicle based on ARM
Li Chao , Yan Jiaming , Liu Songlin.Design of airspeed measuring system for the unmanned aerial vehicle based on ARM[J].Application of Electronic Technique,2012,38(10).
Authors:Li Chao  Yan Jiaming  Liu Songlin
Abstract:A central control process unit with ARM as its core is designed in order to implement the airspeed measuring system for the ummanned aerial vchicle.By the formula decomposition,and linear low-interpolation algorithm,an effective solution is made to the shortcomings of the airspeed solution formula for calculating complex.At the same time,taking advantage of the ARM UART serial bus,the sensor output characteristic curve and real airspeed real time showed in host computer are achieved,so that the relative error of measuring system less is within 2.5%.The test results prove that the system has good effctiveness,stability and high accuracy,better than the traditional system.
Keywords:ARM  indicated airspeed  real airspeed  pressure sensor  linear interpolation
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