A real-time piloted flight simulator is under development in the Laboratory for Control and Automation at Princeton University. This facility will be used to study piloted flight through a simulated wind shear. It will also provide a testbed for real-time flight guidance laws. The hardware configuration and aerodynamic model used are discussed. The microburst model to be incorporated into the simulation is introduced, and some proposed cockpit display concepts are described.


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    Title :

    Flight simulation for wind shear encounter


    Contributors:


    Publication date :

    1990-12-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






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