For the reliability assurance of the GBAS satellite landing system (SLS) the software and hardware implementation in the form of a dual set with “hot” redundancy is proposed. Moreover, both sets of SLS (GBAS) equipment constantly (at least 1 Hz) “interrogate” each other about the working order of the second set.


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    Title :

    Assessment and Reliability Assurance of the Navigation Systems of the Civil Aircraft Under the Conditions of Influence by Different Interference


    Additional title:

    Springer Aerospace Techn.




    Publication date :

    2021-05-14


    Size :

    24 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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