Less processing and storage of data needed. Mathematical basis developed for Kalman filtering of sequential measurements of range from single-channel receiver in Global Positioning System (GPS) to each of several navigation satellites. Range filtering involves separate applications of kinematic Kalman tracking filter to measurements of signal from each satellite in use. State vector consists of pseudorange and time derivatives. Main advantages: simplification of tuning and decreases in required amounts of storage and processing of data for navigation in ships, airplanes, and ground vehicles.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Range Filtering For Navigation By Satellite


    Contributors:

    Published in:

    Publication date :

    1989-08-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Autonomous Satellite Navigation Via Kalman Filtering of Magnetometer Data

    Wiegand, M. / International Astronautical Federation | British Library Conference Proceedings | 1995



    Autonomous satellite navigation via Kalman filtering of magnetometer data

    Wiegard, M. / International Astronautical Federation | British Library Conference Proceedings | 1996



    A comparison of filtering algorithms for GPS satellite navigation application

    Tapley, B. D. / Peters, J. G. / Schutz, B. E. | NTRS | 1979