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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    Title :

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


    Contributors:
    Cook, G. (author) / Witt, R. M. (author)

    Publication date :

    1976-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :




    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 Archive | 1982