Scheme, combining use of displays and optimal control theory, was investigated for application to launch vehicles during boost; scheme enables pilot to continually generate predicted fuel-optimal trajectory; problem of determining optimum steering function is converted into related two-point boundary-value problem; pilot solves problem repetitively by adjusting initial conditions on auxiliary variables so that predicted vehicle state as determined by fast-time model of vehicle satisfies desired end conditions; resulting trajectory generated by model is predicted trajectory for vehicle; particular example was simulated, consisting of boost to circular orbit; simulation equations and results. (11874)


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    Titel :

    Manual optimal guidance scheme using predictive model


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Gilchrist, J.D. (Autor:in) / Soland, D.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A manual optimal guidance scheme using a predictive model.

    Gilchrist, J. D. / Soland, D. E. | NTRS | 1967


    A manual optimal guidance scheme using a predictive model

    GILCHRIST, J. / SOLAND, D. | AIAA | 1967


    A manual optimal guidance scheme using a predictive model.

    Gilchrist, J. D. / Soland, D. E. | NTRS | 1968


    A manual optimal guidance scheme using a predictive model.

    GILCHRIST, J. D. / SOLAND, D. E. | AIAA | 1968


    Manual optimal guidance techniques.

    Anderson, P. A. / Gilchrist, J. D. | NTRS | 1968