Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    An Improved Method to Calculate the Nonlinear Rolling Moment Due to Differential Fin Deflection of Canard Controlled Missiles (AIAA 2015-1018)


    Contributors:

    Conference:

    AIAA atmospheric flight mechanics (Conference)



    Publication date :

    2015-01-01


    Size :

    21 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English