The application of a modified Rutowski logic to mission throttle/energy management was extended, investigating additional types of mission segments and providing a means of logically integrating optimum segments into mission profiles. Measurable fuel savings through throttle modulation were predicted for a demonstration flight mission for the F-4E airplane. A flight path and throttle control system was designed for following the optimum paths. A hybrid simulation plan was prepared.


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    Title :

    Analysis and Simulation of Variable Throttle/Energy Management Concepts for Fighter Aircraft


    Contributors:
    G. G. Grose (author) / R. J. Landy (author) / R. G. Marsh (author) / R. D. Turner (author)

    Publication date :

    1974


    Size :

    152 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English