Presented is a procedure for improving the communication of requirements and specifications in the early design phases of an integrated helicopter/engine control system. The procedure is based on establishing a bound on a transfer matrix that relates blade cyclic and collective inputs to rotor speed variations. This bound becomes a new specification for the propulsion control system designer that embodies the mission-level performance goals of the helicopter. An example application of the procedure is provided for a Blackhawk/T700 system undergoing vertical accelerations from hover.


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    Title :

    Integrated flight/propulsion control for helicopters


    Contributors:


    Publication date :

    1994-07-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Integrated Flight/Propulsion Control for Helicopters

    Rock, S. M. / Neighbors, W. K. / American Helicopter Society | British Library Conference Proceedings | 1993


    Integrated Flight-Propulsion Control for Helicopters

    Rock, S.M. | Online Contents | 1994


    Integrated flight/propulsion control for helicopters

    Rock, S.M. / Neighbors, K. | Tema Archive | 1994



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    Free access