OPTIM generates profile of altitude, airspeed, and flightpath angle as function of range between given set or origin and destination points for particular models of transport aircraft. Profile is optimized in sense of minimizing fuel or time or in minimizing direct operating cost expressed as combination of fuel and time.


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    Titel :

    Vertical Profiles for Turbojet-Powered Aircraft


    Beteiligte:
    Sorensen, J. A. (Autor:in) / Waters, M. H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.05.1983



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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    Approximate solutions to optimum flight trajectories for turbojet-powered aircraft

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    Deformable turbojet aircraft

    MA YUE / YAN XIAO / TANG MUCHENG et al. | Europäisches Patentamt | 2024

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