Digital system gives pilot partial command when primary system fails. Emergency system provides digital control of rigid circulation-control rotor for experimental X-wing aircraft. In addition to centering collective-pitch control, new command provides limited roll control via collective pitch and gyroscopic decoupling in pitch and aerodynamic decoupling.


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    Titel :

    Emergency Control for a Circulation-Control Helicopter Rotor


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.06.1987



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Investigation of a Stoppable Helicopter Rotor with Circulation Control

    J. D. Ballard / J. L. Mccloud / T. J. Forsyth | NTIS | 1980


    Circulation Control Applied to a High Speed Helicopter Rotor

    K. R. Reader / J. B. Wilkerson | NTIS | 1977


    An investigation of a stoppable helicopter rotor with circulation control

    Ballard, J. D. / Mccloud, J. L., III / Forsyth, T. J. | NTRS | 1980



    Tandem Rotor Helicopter Control

    Ng, Tian Seng | Springer Verlag | 2018