Synonyme wurden verwendet für: Stabilität
Suche ohne Synonyme: keywords:(Stabilität)

1–14 von 14 Ergebnissen
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    A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design

    Cotting, M. Christopher / Cox, Timothy H. | NTRS | 2005
    Schlagwörter: Aircraft Stability And Control

    String Stability of a Linear Formation Flight Control System

    Allen, Michael J. / Ryan, Jack / Hanson, Curtis E. et al. | NTRS | 2002
    Schlagwörter: Aircraft Stability And Control

    Impact of flying qualities on mission effectiveness for helicopter air combat, volume 1

    Harris, T. M. / Beerman, D. A. | NTRS | 1983
    Schlagwörter: Aircraft Stability And Control

    Description of the Spacecraft Control Laboratory Experiment (SCOLE) facility

    Williams, Jeffrey P. / Rallo, Rosemary A. | NTRS | 1987
    Schlagwörter: Aircraft Stability And Control

    Fully Automatic Guidance and Control for Rotorcraft Nap-of-the-earth Flight Following Planned Profiles. Volume 2: Mathematical Model

    Clement, Warren F. / Gorder, Peter J. / Jewell, Wayne F. | NTRS | 1991
    Schlagwörter: Aircraft Stability And Control

    Development of an advanced pitch active control system for a wide body jet aircraft

    Guinn, Wiley A. / Rising, Jerry J. / Davis, Walt J. | NTRS | 1984
    Schlagwörter: Aircraft Stability And Control

    Aircrew-aircraft integration: A summary of US Army research programs and plans

    Key, D. L. / Aiken, E. W. | NTRS | 1984
    Schlagwörter: Aircraft Stability And Control

    Development of an integrated configuration management/flight director system for piloted STOL approaches

    Hoh, R. H. / Klein, R. H. / Johnson, W. A. | NTRS | 1977
    Schlagwörter: Aircraft Stability And Control

    Fully automatic guidance and control for rotorcraft nap-of-the-Earth flight following planned profiles. Volume 1: Real-time piloted simulation

    Clement, Warren F. / Gorder, Peter J. / Jewell, Wayne F. | NTRS | 1991
    Schlagwörter: Aircraft Stability And Control

    Handling qualities of a wide-body transport airplane utilizing Pitch Active Control Systems (PACS) for relaxed static stability application

    Grantham, William D. / Person, Lee H., Jr. / Brown, Philip W. et al. | NTRS | 1985
    Schlagwörter: Aircraft Stability And Control

    Subsonic pitch-up alleviation on a 74 deg delta wing

    Rao, D. M. / Johnson, T. D., Jr. | NTRS | 1981
    Schlagwörter: Aircraft Stability And Control