1–10 von 14 Ergebnissen
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    Rotorcraft control system design for uncertain vehicle dynamics using quantitative feedback theory

    Hess, R. A. | NTRS | 1994
    Schlagwörter: Aircraft Stability And Control

    Identification of pilot-vehicle dynamics from in-flight tracking data

    Hess, R. A. / Mnich, M. A. | NTRS | 1986
    Schlagwörter: Aircraft Stability And Control

    Investigation of control, display, and crew-loading requirements for helicopter instrument approach

    Lebacqz, J. V. / Gerdes, R. M. / Forrest, R. D. et al. | NTRS | 1981
    Schlagwörter: Aircraft Stability And Control

    Piloted simulator investigation of helicopter control systems effects on handling qualities during instrument flight

    Forrest, R. D. / Chen, R. T. N. / Gerdes, R. M. et al. | NTRS | 1979
    Schlagwörter: Aircraft Stability And Control

    A piloted simulator investigation of augmentation systems to improve helicopter nap-of-the-earth handling qualities

    Chen, R. T. N. / Talbot, P. D. / Gerdes, R. M. et al. | NTRS | 1978
    Schlagwörter: Aircraft Stability And Control

    Design and evaluation of an integrated flight-control system concept for manual IFR VTOL operations

    Merrick, V. K. / Gerdes, R. M. | NTRS | 1977
    Schlagwörter: Aircraft Stability And Control

    An in-flight simulation of VTOL hover control concepts

    Corliss, L. D. / Greif, R. K. / Gerdes, R. M. | NTRS | 1977
    Schlagwörter: Aircraft Stability And Control

    Quantitative feedback theory applied to the design of a rotorcraft flight control system

    Hess, R. A. / Gorder, P. J. | NTRS | 1993
    Schlagwörter: Aircraft Stability And Control

    Design and evaluation of flight directors for V/STOL aircraft

    Hess, R. A. | NTRS | 1977
    Schlagwörter: Aircraft Stability And Control