The following areas related to landing trajectory optimization research were discussed: (1) programming and modifying the steepest descent optimization procedure, (2) successfully iterating toward the optimum for a four-mile trajectory, (3) beginning optimization runs for a twenty-mile trajectory, and (4) adapt wind tunnel data for computer usage. Other related areas were discussed in detail in the two previous annual reports.


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    Titel :

    Use of steepest descent and various approximations for efficient computation of minimum noise aircraft landing trajectories


    Beteiligte:
    Cook, G. (Autor:in) / Witt, R. M. (Autor:in)

    Erscheinungsdatum :

    1976-08-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    A General Steepest Descent Algorithm

    McSherry, Thomas M. | IEEE | 1976


    Methodology for multiaircraft minimum noise impact landing trajectories

    Cook, G. / Jacobson, I. D. / Chang, R. et al. | NTRS | 1982


    Methodology for multiaircraft minimum noise impact landing trajectories

    Cook, G. / Jacobson, I.D. / Chang, R. et al. | Tema Archiv | 1982