This paper presents a method of controlling an anti-ship missile with the use of the linear-quadratic regulator (LQR). The equations of dynamics of the flight were linearized and written in the form of equations of state. To control the anti-ship missile, a double executive gas-dynamic (moveable nozzle of exhaust gases) and aerodynamic (moveable control surfaces) system is applied. The missile flight is considered in a three dimensional space, whereas the controlling vector is comprised of four components: two components to control the height of the flight and two components to control the direction of the flight. The results are presented in a graphic form.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Optimal Compensator for Anti-Ship Missile with Vectorization of Engine Thrust



    Erschienen in:

    Erscheinungsdatum :

    05.01.2016


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Thrust vectorization for fluid-borne vehicles

    WARREN KEN / HAHNEN OLIVER HENRY / SNOOK MICHAEL ALEXANDER | Europäisches Patentamt | 2022

    Freier Zugriff

    Anti-ship cruise missile barrier

    ADAMS KENNETH M | Europäisches Patentamt | 2016

    Freier Zugriff



    Optimal thrust control of a missile with a pulse motor

    IMADO, FUMIAKI / KURODA, TAKESHI / MIWA, SUSUMU | AIAA | 1991