The effects of random vertical and longitudinal accelerations and pitching velocity passenger ride comfort responses were examined on the NASA Langley Visual Motion Simulator. Effects of power spectral density shape were studied for motions where the peak was between 0 and 2 Hz. The subjective rating data and the physical motion data obtained are presented without interpretation or detailed analysis. There existed motions in all other degrees of freedom as well as the particular pair of longitudinal airplane motions studied. These unwanted motions, caused by the characteristics of the simulator may have introduced some interactive effects on passenger responses.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Human Comfort Response to Dominant Random Motions in Longitudinal Modes of Aircraft Motion


    Contributors:
    R. W. Stone (author)

    Publication date :

    1980


    Size :

    130 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English