Abstract The problem of estimation of the orbital and attitude motion parameters of a spacecraft using readings of a three-axis onboard magnetometer and solar sensor with considerable uncertainty of the initial conditions is solved. Primary attention is paid to improvement of the observability of the desired parameters and acceleration of the estimation process.


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    Title :

    Information Support for a Low-Orbit Spacecraft Using Magnetometer and Solar Sensor Readings


    Contributors:

    Published in:

    Cosmic Research ; 41 , 5 ; 485-493


    Publication date :

    2003-09-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English