The paper describes the integrated aircraft navigation system, which includes the strapdown inertial navigation system (SINS), GPS receiver, optical horizon sensor and magnetometer. The integration algorithm for such system based on the Kalman filtering is represented. Application of this algorithm allows to improve the accuracy of the aircraft motion parameter estimation. For an optical horizon sensor a self-contained horizon recognition algorithm that enables real-time aircraft attitude determination relative to the horizon line is developed. A scaled-down simulation and performance analysis of the operation of the integrated navigation system is carried out.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Integrated aircraft navigation system


    Beteiligte:


    Erscheinungsdatum :

    2013-10-01


    Format / Umfang :

    514875 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Integrated navigation system, method and aircraft

    ZHOU HONGGANG / RAO XINGQIAO / LUO XIAOQIU et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Integrated aircraft ground navigation control system

    JONATHAN EDELSON / NEAL GILLERAN / ISAIAH WATAS COX et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Integrated aircraft ground navigation control system

    EDELSON JONATHAN / GILLERAN NEAL / COX ISAIAH WATAS et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft Navigation System with Integrated Data Communication

    Niemoeller, H.-G. / Gustke, F. / Henzler, J. et al. | British Library Conference Proceedings | 1997


    Aircraft navigation system and method for aircraft navigation

    HEINZINGER OLAF / OBERHAUSER MATTHIAS / MAMESSIER SÈBASTIEN et al. | Europäisches Patentamt | 2019

    Freier Zugriff