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    Evaluation of Pilot's Ability to Stabilize a Flexible Launch Vehicle During First-Stage Boost

    R. W. Gunderson / G. H. Hardy / C. O. Jones et al. | NTIS | 1964
    Schlagwörter: Control

      Evaluation of Pilot's Ability to Stabilize a Flexible Launch Vehicle During First-Stage Boost

      R. W. Gunderson / G. H. Hardy / J. V. West | NTIS | 1965
      Schlagwörter: Flight control , Manual control , Control

    A Piloted Simulation Study of Manual Guidance of the Upper Stages of a Large Launch Vehicle

    G. H. Hardy / R. L. Kurkowski / G. D. Ritter | NTIS | 1967
    Schlagwörter: Guidance and control , Manual control , Control

    Simulation Studies for Planning an in-Flight Experiment to Define Manual Guidance and Control Techniques for Large Launch Vehicles

    G. H. Hardy / G. W. Stinnett / D. M. Watson | NTIS | 1969
    Schlagwörter: Navigation, Guidance, & Control , Manual control

    A Study of Display Systems for Manual Guidance of Large Launch Vehicles Utilizing the X-15 Airplane and Flight Simulators Technical Note

    R. M. Gerdes / G. H. Hardy / A. E. Lopez | NTIS | 1970
    Schlagwörter: Navigation, Guidance, & Control , Manual control

    The 4D Area Navigation System Description and Flight Test Results

    H. Q. Lee / F. Neuman / G. H. Hardy | NTIS | 1975
    Schlagwörter: Air traffic control

    Flight Evaluation of Stabilization and Command Augmentation System Concepts and Cockpit Displays During Approach and Landing of Powered-Lift STOL Aircraft

    J. A. Franklin / R. C. Innis / G. H. Hardy | NTIS | 1980
    Schlagwörter: Attitude control , Manual control

    Flight-Test Evaluation of STOL Control and Flight Director Concepts in a Powered-Lift Aircraft Flying Curved Decelerating Approaches

    W. S. Hindson / G. H. Hardy / R. C. Innis | NTIS | 1981
    Schlagwörter: Approach control , Manual control , Flight control

    Flight-Test Evaluation of a Go-around Control System for a Twin Engine Powered-Lift STOL Airplane

    D. M. Watson / G. H. Hardy | NTIS | 1983
    Schlagwörter: Flight control

    Design, Development, and Flight Test of a Demonstration Advanced Avionics System

    D. G. Denergy / G. P. Callas / G. H. Hardy et al. | NTIS | 1983
    Schlagwörter: Flight control

    Longitudinal Stability and Control Characteristics of the Quiet Short-Haul Research Aircraft (QSRA)

    J. D. Stephenson / G. H. Hardy | NTIS | 1989
    Schlagwörter: Longitudinal control

    Lateral-Directional Stability and Control Characteristics of the Quiet Short-Haul Research Aircraft (QSRA)

    J. D. Stephenson / J. A. Jeske / G. H. Hardy | NTIS | 1990
    Schlagwörter: Lateral control

    Simulation Evaluation of a Low-Altitude Helicopter Flight Guidance System Adapted for a Helmet-Mounted Display

    H. N. Swenson / R. E. Zelenka / G. H. Hardy et al. | NTIS | 1992
    Schlagwörter: Optimal control

    Piloting Considerations for Terminal Area Operations of Civil Tiltwing and Tiltrotor Aircraft

    W. S. Hindson / G. H. Hardy / G. E. Tucker et al. | NTIS | 1993
    Schlagwörter: Aircraft control , Flight control , Thrust vector control

    Design and Flight Evaluation of an Integrated Navigation and Near-Terrain Helicopter Guidance System for Night-Time and Adverse Weather Operations

    H. N. Swenson / R. E. Zelenka / M. G. Dearing et al. | NTIS | 1994
    Schlagwörter: Control systems design , Helicopter control , Numerical control

    Synthesis from Design Requirements of a Hybrid System for Transport Aircraft Longitudinal Control, Volume 1

    C. S. Hynes / G. H. Hardy / L. Sherry | NTIS | 2007
    Schlagwörter: Longitudinal control

    Synthesis from Design Requirements of a Hybrid System for Transport Aircraft Longitudinal Control, Volume 2

    C. S. Hynes / G. H. Hardy / L. Sherry | NTIS | 2007
    Schlagwörter: Longitudinal control

    Use of a Portable Programmable Guidance Display in Support of Helicopter Noise Testing

    W. A. Decker / G. E. Tucker / I. E. Moralez et al. | NTIS | 2007
    Schlagwörter: Air traffic control terminal areas

    Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations

    R. W. Craun / D. M. Acosta / S. D. Beard et al. | NTIS | 2013
    Schlagwörter: Boundary layer control