□ TPA frame work for obtaining trajectory performance bound of individual aircraft is proposed □ Fixed RTA suboptimal trajectory generation method is proposed □ Trajectory structure is designed by analysis of real optimal trajectory □ The suboptimal trajectory shows the similar performance comparing to real optimal trajectory


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    Titel :

    Fixed RTA fuel optimal profile descent based on analysis of trajectory performance bound


    Beteiligte:


    Erscheinungsdatum :

    01.10.2012


    Format / Umfang :

    1987638 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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