Abstract We present four integration methods which exploit efficient numerical techniques for orbit propagation. The methods have been selected to compare the strategy of using first order differential equations, required by the use of regularization, to integrating the equations of motion directly so that second order integrators can be used. All the methods have demonstrated high levels of orbital accuracy as well as very short integration times in astronomical simulations of long term dynamical evolution. We outline the bases of these techniques and illustrate their accuracy by comparing the orbital predictions with data from a GPS receiver on board a satellite in Sun synchronous LEO orbit.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    High Precision Integration Methods for Orbit Propagation


    Beteiligte:
    Palmer, P. L. (Autor:in) / Aarseth, S. J. (Autor:in) / Mikkola, S. (Autor:in) / Hashida, Yoshi (Autor:in)


    Erscheinungsdatum :

    1998




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    BKL:    55.60 Raumfahrttechnik
    Lokalklassifikation TIB:    770/7040




    High Precision Integration Methods for Orbit Propagation

    Palmer, P. L. / Aarseth, S. J. / Mikkola, S. et al. | Springer Verlag | 1998




    High-Precision, Practical Relative Orbit Propagation Using Least-Squares Method

    Yang, Zhen / Luo, Ya-Zhong / Tang, Guo-jin | AIAA | 2013