The objective of the advanced launch system (ALS) program is to develop a family of launch vehicles which provides a substantial improvement in reliability, operability, and economy over existing systems. This requires that autopilot design and verification procedures be of minimum sensitivity to recurring costs while providing adequate, but not necessarily optimal, vehicle performance. One approach to accomplishing this task, namely, the utilization of advanced control design and analysis techniques, is considered. It is shown that the techniques, which represent a cross-section of developments in control theory, attempt to solve the ALS control problem in one of two ways: 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. It is concluded that the methods are promising and cost effective.<>


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    Titel :

    Advanced concepts for launch vehicle control


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


    Erscheinungsdatum :

    01.02.1991


    Format / Umfang :

    679792 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    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. | Tema Archiv | 1990


    Advanced launch vehicle concepts

    Bono, P. | Engineering Index Backfile | 1963



    Advanced Launch Vehicle System Concepts: An Historical Overview

    Ehrlich, C. F. / University of New Mexico; School of Engineering; Institute for Space and Nuclear Power Studies | British Library Conference Proceedings | 1997