A vehicle has first and second portions, with a front aerodynamic element located in the first portion and a rear aerodynamic element located in the second portion. The front and rear aerodynamic elements are each independently movable to respective deployment positions between respective stowed positions and respective fully-extended positions. A controller is operatively connected to each of the front and rear aerodynamic elements and has a processor and tangible, non-transitory memory. The controller is programmed to obtain a front target position (Tf,n) for the front aerodynamic element at a current time step (n) based at least partially on at least one vehicle state parameter at a previous time-step (n−1) and a detected position (Dr,n−1) of the rear aerodynamic element at the previous time-step (n−1).


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    Title :

    DETERMINATION OF AERODYNAMIC ACTUATION COMMANDS


    Contributors:

    Publication date :

    2017-03-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B62D MOTOR VEHICLES , Motorfahrzeuge



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