Several advanced control concepts for application to the advanced launch system (ALS) design problem are presented. It is shown that these methods attempt to solve the ALS control problem by one of two ways: autopilot design given increased knowledge of the launch vehicle and its environment through greater model fidelity and additional sensor data; and autopilot design in the presence of quantified model/disturbance uncertainties and less stringent sensing requirements. In general, both these solution approaches would require increased computation and memory allocation for control law implementation, while reducing the preflight validation and verification process. Techniques belonging to the first solution approach would also increase sensor and actuator requirements, thereby having a further impact on the avionics system. It is concluded that concepts belonging to the second category would have less overall impact on avionics and, therefore, would be the more viable approach to solving the ALS design problem.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Advanced concepts for launch vehicle control


    Weitere Titelangaben:

    Verbesserte Konzepte für die Raumfahrzeugsteuerung


    Beteiligte:
    Sifer, J.F. (Autor:in) / Prouty, S.J. (Autor:in) / Mak, P.H. (Autor:in)


    Erscheinungsdatum :

    1990


    Format / Umfang :

    6 Seiten, 12 Quellen



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Advanced concepts for launch vehicle control

    Sifer, J.F. / Prouty, S.J. / Mak, P.H. | Tema Archiv | 1991


    Advanced concepts for launch vehicle control

    Sifer, J.F. / Prouty, S.J. / Mak, P.H. | IEEE | 1991


    Advanced launch vehicle concepts

    Bono, P. | Engineering Index Backfile | 1963


    Advanced launch vehicle concepts

    Bono, P. | Engineering Index Backfile | 1963