Abstract To design and analyze planar orbit control systems, including orbit shape control with radial and tangential thrust, and nonlinear thrust vectoring for de-orbiting a satellite from circular orbit. To design and analyze nonlinear orbital plane control systems, including those based upon switching thrust direction and smooth thrust modulation. To design and analyze spacecraft attitude control systems with impulsive thrust, reaction wheels, momentum wheels, and control moment gyros, and taking into account gravity-gradient and solar radiation disturbances.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    ORBIT-SERVICED AUTOMATIC SPACECRAFT

    LEONOV ALEKSANDR GEORGIEVICH / EFREMOV GERBERT ALEKSANDROVICH / PALKIN MAKSIM VYACHESLAVOVICH et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Spacecraft automatic umbilical system

    Rudy, G. C. | NTRS | 1982


    SPACECRAFT FOR SERVICING ON-ORBIT AUTOMATIC SPACECRAFT AND METHOD FOR DOCKING SERVICING SPACECRAFT WITH FAULTY ROTATING SPACECRAFT

    LEONOV ALEKSANDR GEORGIEVICH / EFREMOV GERBERT ALEKSANDROVICH / PALKIN MAKSIM VJACHESLAVOVICH et al. | Europäisches Patentamt | 2016

    Freier Zugriff