General condition is derived which must be satisfied by aircraft or space vehicle to reach predetermined point in minimum time; thrust, lift and drag can depend, in arbitrary manner, on instantaneous position and velocity coordinates (or Mach number) and angle of attack between directions of thrust and velocity; to make solution applicable to space vehicles and aircraft, cases of spherical and flat Earth are treated separately.


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    Titel :

    Minimum time flight paths


    Weitere Titelangaben:

    ARS -- J


    Beteiligte:

    Erschienen in:

    ARS Journal ; 30 , n 4


    Erscheinungsdatum :

    1960


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Minimum fuel flight paths for given range

    BREAKWELL, J. / SHOAEE, H. | AIAA | 1980


    Minimum fuel horizontal flight paths in the terminal area

    KREINDLER, E. / NEUMAN, F. | AIAA | 1982



    Time-optimal flight paths

    Berry, R.L. | Engineering Index Backfile | 1968