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    GPS INS Integration Application in Flight Management System

    GPS INS Integration Application in Flight Management System

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    Flight management system (FMS) is a specialized computer system that automates a wide variety of in-flight tasks, reducing the workload on the flight crew to the point that modern aircraft no longer carry flight engineers or navigators. The primary function of FMS is to perform the in-flight management of the flight plan using various sensors (such as GPS and INS often backed up by radio navigation) to determine the aircraft's position. From the cockpit FMS is normally controlled through a Control Display Unit (CDU) which incorporates a small screen and keyboard or touch screen. This paper investigates the performance of GPS/ INS integration techniques in which the data fusion process is done using Kalman filtering. This will include the importance of sensors calibration as well as the alignment of the strap down inertial navigation system. The limitations of the inertial navigation systems are investigated in order to understand why INS sometimes is integrated with other navigation aids and not just operating in standalone mode. Finally, both the loosely coupled and tightly coupled configurations are analyzed for several types of situations and operational conditions.

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    Titel :

    GPS INS Integration Application in Flight Management System

    Beteiligte:
    Othman Maklouf (Autor:in) / Abdurazag Ghila (Autor:in) / Saleh Gashoot (Autor:in) / Ahmed Abdulla (Autor:in)
    Erscheinungsdatum :

    2012-11-23

    Anmerkungen:

    oai:zenodo.org:1331067
    International Journal of Mechanical, Industrial and Aerospace Sciences 5.0(11)

    DOI :

    https://doi.org/10.5281/zenodo.1331067

    Medientyp :

    Aufsatz (Zeitschrift)

    Format :

    Elektronische Ressource

    Sprache :

    Englisch

    Klassifikation :

    DDC:    629

    Lizenzbestimmungen :

    https://creativecommons.org/licenses/by/4.0/legalcode

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