Based on a series of H-I launches in Japan, a review of control system designs of expendable launch vehicles is presented in terms of their flexibility. The equations of motion are first formulated for lateral and longitudinal dynamics of a flexible vehicle, after which the aerodynamic loads caused by in-flight atmospheric wind are described in relation to trajectory planning. Included are mode analyses for launch vehicles and time responses to the flight environment. Finally, stability analyses for lateral and longitudinal vibrations of launch vehicles are presented with special emphasis on POGOs.


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    Titel :

    Control system design of flexible-body launch vehicles


    Weitere Titelangaben:

    Entwurf eines Regelungssystems für flexible Raumfahrzeuge


    Beteiligte:
    Mori, H. (Autor:in)

    Erschienen in:

    Control Engineering Practice ; 7 , 9 ; 1163-1175


    Erscheinungsdatum :

    1999


    Format / Umfang :

    13 Seiten, 20 Bilder, 2 Tabellen, 12 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Control of Launch Vehicles as Flexible Bodies

    Mori, H. / International Federation of Automatic Control | British Library Conference Proceedings | 1999


    An adaptive control concept for flexible launch vehicles

    ENGLEHART, MATTHEW / KRAUSE, JAMES | AIAA | 1992


    Near Optimal Control for Flexible Expendable Launch Vehicles

    Tan, Z. / Bainum, P. M. / American Astronautical Society et al. | British Library Conference Proceedings | 1997


    Control/Structure Interaction Associated with Flexible Expendable Launch Vehicles

    Pai, R. V. / Bainum, P. M. / Li, F. et al. | British Library Conference Proceedings | 1995


    Launch operations of minimum cost design launch vehicles

    BRAUN, M. / COHN, B. / GROO, R. | AIAA | 1970