Any good set of explicit guidance equations for large multistage space launching vehicles is capable of accurately achieving simultaneously several components of desired position and velocity at thrust termination; equations described offer possibility of changing targets on launch pad, or in flight; fundamental principles upon which these guidance equations are based together with their computer simulation as now in operation at Aerospace Corp; illustrative examples of simulated trajectories are also presented.


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    Titel :

    Explicit tangent-steering guidance for multi-stage boosters


    Weitere Titelangaben:

    Astronautica Acta


    Beteiligte:
    Perkins, F.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Pitch-Over Maneuver and Guidance for Rocket-Back Boosters

    Lu, Ping / Horneman, Kenneth / Neal, David et al. | AIAA | 2011


    Bilinear tangent yaw guidance

    BRUSCH, R. | AIAA | 1979


    Pitch-Over Maneuver and Guidance for Rocket-Back Boosters

    Lu, P. / Neal, D. / Su, S. et al. | British Library Conference Proceedings | 2011



    On boosters

    Stephens, G. | Engineering Index Backfile | 1903