A control system (100) for a rotary wing aircraft having a reconfigurable element. The control system includes a model predictive control module (110)receiving operator commands (102), objectives (112) and constraints (106); and a dynamic inversion module (116) receiving an output (114) of the model predictive control module (110), the dynamic inversion module (116) providing control commands to reconfigure the reconfigurable element (118) of the rotary wing aircraft.


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    Title :

    Control system for reconfigurable rotary wing aircraft


    Additional title:

    Steuersystem für rekonfigurierbaren Drehflügler
    Système de commande pour aéronef à voilure tournante reconfigurable


    Contributors:

    Publication date :

    2019-06-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen




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