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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Integrated Precision Navigation System


    Beteiligte:
    G. Schaenzer (Autor:in) / B. Tiemeyer (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Integrated Navigation-Communication Information System with High Precision Autonomous Star Navigation

    Kuskov, V.D. / Novikova, E.L. | British Library Conference Proceedings | 2006


    High Precision Integrated Navigation System for Vehicle Guidance

    Schaenzer, G. / Scientific Council of the Academy of Sciences on the Problems of Motion Control and Navigation / State Research Center of the Russian Federation; Central Scientific and Research Institute "Elektropribor" et al. | British Library Conference Proceedings | 1999




    Integrated navigation and guidance for precision landing at Mars

    Burkhart, P. D. / Bishop, R. H. / Crain, T. P. | NTRS | 2001