Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stability and performance of closed loop system


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Minimax attitude control of aeroballistic launch vehicles


    Publication date :

    1965-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English