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A method for identifying factual corruption of the navigation signal and identifying the interference influence on unmanned aerial vehicle receiver

Objectives of this article are to create a method that should identify distortion of navigation signals using supplementary information obtained whilst processing the navigation parameters in the calculator of the navigation receiver. To develop this method, a comparative evaluation of the actual da...

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محفوظ في:
التفاصيل البيبلوغرافية
المؤلفون الرئيسيون: Linets, G. I., Линец, Г. И., Sagdeev, K. M., Сагдеев, К. М., Melnikov, S. V., Мельников, С. В., Isaev, M. A., Исаев, М. А., Isaev, A. M., Исаев, А. М.
التنسيق: Статья
اللغة:English
منشور في: Journal of Aerospace Technology and Management 2021
الموضوعات:
الوصول للمادة أونلاين:https://dspace.ncfu.ru/handle/20.500.12258/18530
الوسوم: إضافة وسم
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الوصف
الملخص:Objectives of this article are to create a method that should identify distortion of navigation signals using supplementary information obtained whilst processing the navigation parameters in the calculator of the navigation receiver. To develop this method, a comparative evaluation of the actual data of the navigation measurements with the calculated data values and a Bayesian probabilistic approach for detecting the navigation field distortion and identifying the interference. Test of results of the developed method showed that it enables a highly reliable assessment of the state of the navigation field and, if distorted, the identification of the distortion type: normal (undistorted) condition; abnormal state: when abnormally high errors appear spasmodically in the positioning estimation within individual measuring channels of the navigation receiver; slightly distorted state leading to a slow change in positioning accuracy; active spoofing manifested in the substitution of positioning coordinates. The article provides a new method for processing navigation parameters allowing to detect the fact of the navigation fields (NF) distortion and identify the interference effect on the navigation receiver (NR) of UAV.