A hybrid navigation system, composed of an Inertial Navigation System (INS) and the Global Positioning System (GPS), has been developed. The paper outlines the hybrid navigation system. The system's architecture is characterized by a correction of INS, based on GPS data and Kalman filtering techniques, so as to prevent an increase in the INS position error. To demonstrate the feasibility and the performance of the system, an engineering evaluation model was made and flight-tested in a company-owned MU-300 business jet aircraft. Test results indicate that the INS position data that are corrected by GPS data and Kalman filter closely coincide with GPS position data.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Hybrid Navigation System


    Contributors:
    T. Konishi (author) / I. Yoshie (author) / H. Takahira (author) / Y. Kinoshita (author)

    Publication date :

    1987


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Hybrid Navigation System

    M. Ikeuchi / M. Harigae | NTIS | 1989



    Hybrid Navigation Systems

    G. R. Marner / B. P. Leonard / M. W. Mitchell et al. | NTIS | 1970



    Real-Time Navigation Algorithm for the SHEFEX2 Hybrid Navigation System Experiment

    Steffes, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012