Combined Satellite and Inertial Navigation Systems can achieve extremely high positioning accuracies in the sub meter range even in the dynamic environment of aircraft. This paper presents the concept of the 'Integrated Navigation System' developed at the Institute of Flight Guidance using coupled satellite and inertial sensors. Flight test results are shown, which demonstrate that this system has the potential to achieve the accuracy requirements according to ICAO CAT 3 for high precision approaches even under bad weather conditions.


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    Title :

    Integrated Precision Navigation System


    Contributors:
    G. Schaenzer (author) / B. Tiemeyer (author)

    Publication date :

    1992


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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