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.
Assessment and Reliability Assurance of the Navigation Systems of the Civil Aircraft Under the Conditions of Influence by Different Interference
Springer Aerospace Techn.
Modern Requirements for Noise Immunity Aircraft Navigation Equipment ; Chapter : 2 ; 43-66
2021-05-14
24 pages
Article/Chapter (Book)
Electronic Resource
English
The Development of GPS Navigation Systems in Civil Aircraft
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