The simulation requirements for investigation of pilot-induced-oscillation (PIO) characteristics during the landing phase are discussed. Orbiters simulations and F-8 digital fly-by-wire aircraft tests are addressed.


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    Title :

    Space shuttle pilot-induced-oscillation research testing


    Contributors:

    Publication date :

    1984-02-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English