Results are presented to illustrate the application of established procedures of linear, quadratic, Gaussian optimal estimation and control to a spacecraft with dynamically significant elastic appendages. Interpretations are provided in both time domain and frequency domain, and conclusions are drawn for a wide class of problems of flexible spacecraft attitude control.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    An application of modern control theory to an elastic spacecraft


    Beteiligte:
    Larson, V. (Autor:in) / Likins, P. W. (Autor:in)


    Erscheinungsdatum :

    1976-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Modern spacecraft dynamics & control

    Kaplan, Marshall H. | TIBKAT | 1976


    Modern spacecraft dynamics & control

    Kaplan, Marshall H. | SLUB | 1976


    CAN Bus for Modern Spacecraft Control Systems

    Sanchez, A.V. / Carretero, A.V. / Furano, G. et al. | British Library Conference Proceedings | 2011


    Adaptive control and stabilization of elastic spacecraft

    Singh, S.N. / de Araujo, A.D. | IEEE | 1999


    Review of modern spacecraft thermal control technologies

    Hengeveld, Derek W. / Braun, James E. / Mathison, Margaret et al. | Tema Archiv | 2010