Three atmospheric guidance concepts proposed for an aeroassist flight experiment are presented. The flight experiment will simulate a return from geosynchronous orbit by an aeroassisted orbital transfer vehicle and is proposed to be flown on board the Space Shuttle in 1992. The three guidance concepts include an analytic predictor/corrector, a numeric predictor/corrector, and an energy controller. The algorithms for the three guidance methods are developed and performance results are presented for the nominal case and for several cases dispersed from the nominal conditions.


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    Titel :

    Atmospheric guidance concepts for an aeroassist flight experiment


    Beteiligte:
    Gamble, J. D. (Autor:in) / Cerimele, C. J. (Autor:in) / Moore, T. E. (Autor:in) / Higgins, J. (Autor:in)


    Erscheinungsdatum :

    1988-06-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aeroassist flight experiment guidance Quiet Time

    Striepe, Scott A. / Suit, William T. | NTRS | 1988


    Aeroassist Flight Experiment (AFE)

    Siemers, Paul M., III | NTRS | 1988


    The Aeroassist Flight Experiment

    Walberg, G. D. / Siemers, P. M., III / Calloway, R. L. et al. | NTRS | 1987


    Aeroassist Flight Experiment (AFE)

    P. M. Siemers | NTIS | 1988