The Optimum Stabilization of a tumbling satellite via Hamilton-Jacobi theory has been reported by one of the authors before in ¿On the optimum stabilization of a satellite¿ [2]. This companion paper discusses the synthesis of a specific optimum control law for the same problem and compares the results with the optimum solution. It is shown that a specific optimum control law yields, acceptable performance while being much easier to instrument than the optimum control law.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Stabilization of a Satellite via Specific Optimum Control


    Beteiligte:
    Kumar, K. S. P. (Autor:in) / Teng, Lincoln (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.07.1966


    Format / Umfang :

    1716427 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Stabilization of satellite via specific optimum control

    Kumar, K.S.P. / Teng, L. | Engineering Index Backfile | 1966


    On optimum stabilization of satellite

    Kumar, K.S.P. | Engineering Index Backfile | 1965


    On the Optimum Stabilization of a Satellite

    Kumar, K. S. P. | IEEE | 1965


    Optimum Ship Steering-Stabilization Control

    Whalley, R. | Online Contents | 2003


    Optimum launching of satellite by two impulses of unequal specific impulse

    Ting, L. / Pierucci, M. | Engineering Index Backfile | 1963