Study of concept of inertially aided barometric altimetry system to meet vertical separation requirements of 1000 and 2000 feet for Mach 3.5 aircraft in altitude hold at 80,000 feet


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    Title :

    Study of the concept of inertially aided barometric altimetry system for supersonic aircraft


    Contributors:

    Publication date :

    1971-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Study of the Concept of Inertially Aided Barometric Altimetry System for Supersonic Aircraft

    K. R. Britting / J. R. Ruetenik / J. H. Thompson | NTIS | 1971



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