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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    Title :

    Rotorcraft flight-propulsion control integration


    Contributors:

    Published in:

    Publication date :

    1984-10-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Rotorcraft flight-propulsion control integration

    Mihaloew, James R. / Ballin, Mark G. / Ruttledge, D. G. C. | NTRS | 1988


    Rotorcraft Flight-Propulsion Control Integration

    J. R. Mihaloew / M. G. Ballin / D. G. C. Ruttledge | NTIS | 1988



    Rotorcraft Flight-Propulsion Control Integration: An Eclectic Design Concept

    J. R. Mihaloew / M. G. Ballin / D. C. G. Ruttledge | NTIS | 1988


    Rotorcraft flight-propulsion control integration: An eclectic design concept

    Mihaloew, James R. / Ballin, Mark G. / Ruttledge, D. C. G. | NTRS | 1988