The parallel development of digital engine and flight controls for U.S. Army helicopters has made possible the future derivation of a fully integrated digital flight/propulsion control system. A NASA/Army research program has been undertaken to exploit these possibilities, ultimately yielding a generation of helicopters with exceptional agility and maneuverability in military roles and low pilot workloads in all-weather civil aviation missions. The program's three phases respectively address system modeling and analysis, flight hardware and software development, and flight evaluations aboard a research vehicle.


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    Titel :

    Rotorcraft flight-propulsion control integration


    Beteiligte:
    Mihaloew, J. R. (Autor:in) / Chen, R. T. N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.10.1984



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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