机载测向——导航误差理论

C. Ancker
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引用次数: 34

摘要

斯坦斯菲尔德先前研究了n个固定的、精确定位的测向站通过角方位相交来固定未知发射器位置的情况,其中角方位具有小的、正态分布的误差。确定了最可能的发射极位置和周围的置信区域。斯坦斯菲尔德的解决方案在这里扩展到包括机载测向的情况,这引入了测向站位置的不确定性。这些不确定性来自导航错误,并增加了定位的不确定性,这反映在解决方案方差的增加中。不确定性的增加是由天文、航位推算和测向(罗兰、肖兰等)导航程序引起的。假设导航误差很小,呈正态分布。此外,还研究了在测向切点之间进行天体定位的模型。对各种程序进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Airborne Direction Finding---The Theory of Navigation Errors
The situation where n stationary, accurately located, direction-finding stations fix the position of an unknown emitter by intersecting angular bearings has been previously investigated by Stansfield for the case where the angular bearings have small, normally distributed errors. The most probable location of the emitter and the surrounding confidence regions were determined. Stansfield's solution is here extended to include the case of airborne direction finding, which introduces uncertainties in the locations of the direction-finding stations. These uncertainties arise from navigation errors and increase the uncertainty of the fix, which is reflected in an increase in the variance of the solution. The increase in uncertainty is derived for celestial, dead reckoning, and direction-finding (Loran, Shoran, etc.) navigational procedures. Small, normally distributed navigation errors are assumed. In addition, a model in which celestial position fixes are taken between direction-finding cuts is investigated. The various procedures are compared.
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