Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Autopilot design for a tail-controlled missile using two-degree-of-freedom controllers


    Contributors:

    Conference:

    Guidance, Navigation, and Control Conference ; 1995 ; Baltimore , MD , U.S.A.



    Publication date :

    1995-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





    Linearization of a Six-Degree-of-Freedom Missile for Autopilot Analysis

    Jonathan R. Bar-On / Robert J. Adams | AIAA | 1998



    Anti-Windup Command Filtered Adaptive Backstepping Autopilot Design for a Tail-Controlled Air-Defense Missile

    Peter, Florian / Hellmundt, Fabian / Holzapfel, Florian et al. | AIAA | 2013


    Autopilot for a Nonlinear Non-Minimum Phase Tail-Controlled Missile (AIAA 2014-1293)

    Narang-Siddarth, A. / Peter, F. / Holzapfel, F. et al. | British Library Conference Proceedings | 2014