According to a number of system studies, large capacity advanced rotorcraft with a capability of high cruise speeds (approx.350 mph) as well as vertical and/or short take-off and landing (V/STOL) flight could alleviate anticipated air transportation capacity issues by making use of non-primary runways, taxiways, and aprons. These advanced aircraft pose a number of design challenges, as well as unknown issues in the flight control and handling qualities domains. A series of piloted simulation experiments have been conducted on the NASA Ames Research Center Vertical Motion Simulator (VMS) in recent years to systematically investigate the fundamental flight control and handling qualities issues associated with the characteristics of large rotorcraft, including tiltrotors, in hover and low-speed maneuvering.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Handling Qualities of Large Rotorcraft in Hover and Low Speed


    Beteiligte:

    Erscheinungsdatum :

    2015-03-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Handling Qualities of Large Rotorcraft in Hover and Low Speed

    C. Malpica / C. R. Theodore / B. Lawrence et al. | NTIS | 2015


    An Investigation of Large Tilt-Rotor Hover and Low Speed Handling Qualities

    Blanken, C. / Decker, W. / Lawrence, B. et al. | British Library Conference Proceedings | 2011


    Rotorcraft Handling Qualities in Turbulence

    Hess, R.A. | Online Contents | 1995



    Rotorcraft Handling-Qualities Design Criteria Development

    E. W. Aiken / J. V. LeBacqz / R. T. N. Chen et al. | NTIS | 1988