Inertial navigation system algorithmic correction methods were studied. Navigation system errors model calculation was carried out on board the aircraft. When calculating the models, it was proposed to ensure prefiltering of the measurement signals using a modified trend.


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    Title :

    Signals prefiltering in the aircraft navigation system



    Conference:

    XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration ; 2019 ; Moscow, Russia


    Published in:

    Publication date :

    2019-11-15


    Size :

    4 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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