The problem of pilot performance estimates during the aircraft design phase is discussed. The following are found to influence such estimates: low altitude turbulence model, aircraft model, mission model and pilot response model. Pilot responses to stochastic gust disturbances are evaluated and the aircraft transfer functions are calculated. Flight controllers are needed for low altitude flight. Elastic degrees of aircraft motion should be included in the calculation. (Author)


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    Title :

    On the Question of Pilot Deterioration During Low Altitude Flight


    Contributors:
    P. Schulz (author)

    Publication date :

    1974


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English