A simulator study was undertaken to compare and evaluate the design features of the electronic displays for possible use in V/STOL aircraft: a combined transition display (Display A), a perspective display (Display B), and a hover display (Display C). Display B presents height information via integrated elements; Displays A and C present information similarly except that Display C presents vertical and lateral guidance via conventional cross pointers. High pilot work load was attained by evaluating the displays only as situational guidance displays in a simulated vehicle without stability augmentation. Glide slopes of 6 and 15 deg were used, and steady-state and no-wind conditions were randomly presented. Six pilots participated, and fifty-five objective performance measures were taken along with pilot opinions


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    Title :

    Simulator evaluation of three situation and guidance displays for V/STOL aircraft zero-zero landing approaches


    Contributors:
    Murphy, M. R. (author) / Palmer, E. A. (author) / Wempe, T. E. (author) / Mcgee, L. A. (author) / Paulk, C. H. (author)

    Publication date :

    1978-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Simulator evaluation of three situation and guidance displays for V/STOL zero-zero landings

    Murphy, M. R. / Mcgee, L. A. / Palmer, E. A. et al. | NTRS | 1974




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