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出 处:《导航》2006年第2期106-108,共3页
摘 要:为了更好的评估陆基无线电导航系统机载设备的性能,提出了应用DSP技术改装部分飞行检测系统的观点.在飞行检验陆基无线电导航设备的过程中,传统的飞行检测系统均是用模拟电路来实现的,但受温度和湿度变化及飞行抖动的影响容易产生测量误差,为了补偿这些误差就需要在飞行过程中进行定标.而基于DSP技术的飞行检测系统将不需要这一繁琐的过程.该系统最为关键的模拟处理设备就是一个模,数(A/D)转换器.该系统两种特别的用途:(1)ILS航道偏移量的测定;(2)VOR系统方位角的测定.此外,应用DSP技术改装的飞行检测系统还比较经济适用.This paper discusses the application of DSP techniques in a portable flight inspection system for the airborne evaluation of ground-based radio navigational aids. Traditional flight inspection systems use analog circuitry and thus require in-flight calibration between measurements to compensate for variations caused by temperature and humidity changes, and vibration. The need for such calibration has been eliminated as a result of the work addressed in this paper, since by relying on DSP techniques it is possible to reduce the key analog processing hardware to a single A/D converter. Two specific applications are presented here: 1) course displacement determination for the immanent landing system (ILS), and 2) azimuth angle determination for the VOR. The DSP techniques presented here were implemented in a flight inspection system which is in commercial use.
分 类 号:TN965[电子电信—信号与信息处理]
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