The communication of this method is being used by NASA in the ongoing collaborations with groups interested in the X-56A flight test program. Model generation for body freedom flutter Addressing issues in: State Consistency, Low frequency dynamics, Unsteady aerodynamics. Applied approach to X-56A MUTT: Comparing to flight test data.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design


    Contributors:

    Conference:

    Aerospace Control and Guidance Systems Committee Meeting No. 119 ; 2017 ; Fairborn, OH, United States


    Publication date :

    2017-03-29


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English