We suggest a determined iterative algorithm of defining the planar parameters of a spacecraft Keplerian orbit in the velocity reference frame. Analytical relations for creating the iterative algorithm and the numeric example of defining parameters of a spacecraft Keplerian orbit are given.


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    Title :

    Onboard Iterative Algorithm of Defining the Parameters of Keplerian Orbits Based on Solving the Orbital Motion Equations in Velocity Reference Frame


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 64 , 3 ; 432-440


    Publication date :

    2021-07-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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