The article addresses the fully distributed time-varying formation control problem for multiple missiles involving uncertainties. An adaptive control protocol is developed for the missiles, which includes uncertainties in the flight dynamics, while the adaptive control protocol does not require global information of the network missile system. Global formation flight stability is proven via the Lyapunov theory. Simulation tests are performed to validate the effectiveness of the developed protocol as applied to the network system.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Fully Distributed Time-Varying Formation Control for Multiple Uncertain Missiles


    Beteiligte:
    Liu, Deyuan (Autor:in) / Liu, Hao (Autor:in) / Valavanis, Kimon P. (Autor:in)


    Erscheinungsdatum :

    2021-06-01


    Format / Umfang :

    1233027 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Shunting Method for Control of Homing Missiles with Uncertain Parameters

    Fradkov, A. / Andrievsky, B. / International Federation of Automatic Control | British Library Conference Proceedings | 2004



    Closed-form optimal guidance law for missiles of time-varying velocity

    Cho, Hangju / Ryoo, Chang K. / Tahk, Min-Jea | AIAA | 1996


    Optimal Trajectory Shaping Guidance of Missiles with Time Varying Acceleration Constraints

    Taub, I. / Shima, T. / Tekhniyon, Makhon tekhnologi le-Yisra'el | British Library Conference Proceedings | 2012