A new class of guidance laws is developed on the basis of the Lyapunov method. The proposed new guidance laws improve the effectiveness of the proportional navigation (PN) law against manoeuvring targets. They augment the PN law which is a part of these laws. Analytical expressions of the new guidance laws for the generalized three-dimensional engagement model are presented. By considering separately the missile longitudinal and lateral motions, the expressions for its radial and lateral accelerations are obtained. The new guidance laws can be utilized for missiles with thrust control as well as for many types of existing missile without throttlable engines.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Generalized missile guidance laws against manoeuvring targets


    Beteiligte:


    Erscheinungsdatum :

    2007


    Format / Umfang :

    7 Seiten, 12 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Estimation and guidance for manoeuvring targets

    Radhika M.N. / Parthasarathy, S.S / Kumar, G. Saroj | IEEE | 2015



    Fuzzy Missile Guidance Laws

    Creaser, P. / Stacey, B. / White, B. et al. | British Library Conference Proceedings | 1998


    Tactical Missile Guidance Laws

    Siouris, George M. | Springer Verlag | 2004


    Fuzzy missile guidance laws

    Creaser, P. / Stacey, B. / White, B. | AIAA | 1998