Abstract The problem of reentry vehicle control during its descent from a near-Earth orbit is considered under conditions of “enhanced” disturbances. The earlier developed terminal descent control algorithm is considerably improved to satisfy constraints on landing accuracy, load factor, and propellant consumption. A method for automatically shifting the deorbit point, adaptating to actual motion conditions, and modifying the reference bank function is proposed, which ensured the satisfaction of the specified constraints under action of an aggregate of enhanced disturbing factors.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Modification of the Terminal Control Algorithm for Descent from Near-Earth Orbit Applied to “Enhanced” Disturbances


    Beteiligte:
    Evdokimov, S. N. (Autor:in) / Klimanov, S. I. (Autor:in) / Korchagin, A. N. (Autor:in) / Mikrin, E. A. (Autor:in) / Samotokhin, A. S. (Autor:in) / Sikharulidze, Yu. G. (Autor:in) / Tuchin, A. G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2019




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :

    Klassifikation :

    BKL:    55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung
    Lokalklassifikation TIB:    770/3520/8000



    Modification of the Terminal Control Algorithm for Descent from Near-Earth Orbit Applied to “Enhanced” Disturbances

    Evdokimov, S. N. / Klimanov, S. I. / Korchagin, A. N. et al. | Springer Verlag | 2019


    Modification of the Terminal Control Algorithm for Descent under “Magnified” Disturbances after Returning from the Moon

    Evdokimov, S. N. / Klimanov, S. I. / Korchagin, A. N. et al. | Springer Verlag | 2020


    CONTROL OVER SPACECRAFT DESCENT FROM EARTH ARTIFICIAL SATELLITE ORBIT

    SOKOLOV NIKOLAJ LEONIDOVICH / KARTSEV JURIJ ALEKSANDROVICH / KOLOT IRINA JUR EVNA et al. | Europäisches Patentamt | 2015

    Freier Zugriff


    METHOD FOR CONTROLLED DESCENT OF SPACECRAFT FROM NEAR-EARTH ORBIT AT SECTION OF HYPERSONIC SPEEDS

    RULEV IGOR MIKHAJLOVICH | Europäisches Patentamt | 2020

    Freier Zugriff