Two further studies are reported concerning the utility of a predictor display instrument in landing jet aircraft. In the first study, the length of prediction span and control stick dynamics were systematically varied and compared to baseline (no prediction and no stick/control response-delay) condition. Performances on all predictor display conditions were superior to the baseline and the best performance was seen on the experimental condition with the longest prediction span and the longest stick/control response-delay. In the second study, a 6-degree of freedom F-4 night carrier landing simulation was flown by pilots who were (N=6) or were not (N=6) experienced in that type aircraft.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Two Studies of Predictor Displays for Jet Aircraft Landings. (1) Optimization of Control Stick Dynamics and Prediction Span Parameters. (2) A Comparison Between Experienced and Novice Navy F-4 Pilot Simulated Landing Performances


    Contributors:
    R. S. Kennedy (author) / R. L. Smith (author) / J. W. Wulfeck (author) / J. E. Queen (author) / W. J. Burger (author)

    Publication date :

    1975


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English








    Cockpit displays for all-wether landings

    Gainer, Charles A. / Welde, William L. / Monroe, Ronald | TIBKAT | 1962