A time-range-fuel optimization problem is formulated for an airbreathing, hypersonic vehicle. Singular perturbation theory is used to decompose the problem into simpler subproblems. Analysis of the cruise-dash problem shows the importance of a Mach-limit. Energy-heading transients are studied and a family of trajectories, fairing asymptotically to a cruise condition, are generated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Energy-heading transients in atmospheric flight guidance for airbreathing hypersonic vehicles


    Beteiligte:
    Cliff, Eugene M. (Autor:in) / Well, KLAUS-H. (Autor:in)

    Erscheinungsdatum :

    01.12.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Flight-test guidance for airbreathing hypersonic vehicles

    Cliff, Eugene M. / Well, KLAUS-H. / Schnepper, Klaus | NTRS | 1992


    Flight-test guidance for airbreathing hypersonic vehicles

    CLIFF, EUGENE / WELL, KLAUS-H. / SCHNEPPER, KLAUS | AIAA | 1992