A lightweight, low-cost R and D aircraft inertial navigation system is evaluated for use in Army aircraft. A brief description of the system is followed by a summary of the methods of laboratory, truck, and flight testing employed. Test results are presented and show that the system meets the design goals of 2 to 4 nautical miles/hour. Problem areas uncovered during the tests are discussed in detail and areas of suggested future effort are outlined. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Flight Test Report of AN/ASN-82 Inertial Navigation System


    Beteiligte:
    R. Clark (Autor:in)

    Erscheinungsdatum :

    1970


    Format / Umfang :

    105 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch