轨道飞行器捕获辅助装置的可能精度

R. T. Dames
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引用次数: 0

摘要

跟踪系统的有效运行要求在车辆接近前每个站点都有一定的获取辅助设备。获得这种辅助的一种方法是根据一组轨道参数外推飞行器的位置。由于外推误差一般会随时间增加,轨道参数必须定期更新,以便自动获取。提出一种评估车辆位置外推误差的统计分析方法。从一组轨道元出发,根据轨道元误差的规定分布,得到与飞行器位置误差矢量大小相关的统计参数的上界。该上限与时间有关,并用于估计获取辅助工具中的相关误差。因此,所有的估计都依赖于自轨道参数更新以来已经过期的时间间隔。分析方法是通用的,可以应用于广泛的跟踪系统。包括一个例子,以表明误差的大小为一个特定的假设车辆。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Probable Accuracy in Acquisition Aids for an Orbiting Vehicle
Efficient operation of a tracking system requires that certain acquisition aids be available to each station prior to vehicle approach. One method of deriving such aids is based on extrapolation of vehicle position from a set of orbital parameters. Since in general, extrapolation errors tend to increase with time, orbital parameters must be updated periodically to provide for automatic acquisition. A statistical analysis is presented for assessing extrapolation errors in vehicle position. Starting with a set of orbital elements and a prescribed distribution of errors in the latter, an upper bound is obtained for a statistical parameter associated with the magnitude of the vehicle position error vector. This upper bound is time-dependent and is applied to estimate the related errors in acquisition aids. Thus, all estimates depend upon the time lapse which has expired since the orbital parameters were updated. The method of analysis is general and may be applied to a wide class of tracking systems. An example is included to indicate the magnitude of errors for a particular hypothetical vehicle.
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