This paper presents an integrated guidance and control design for the homing missiles with the radome error compensation to address the guidance problems caused by radome. Firstly, a mathematics model of the integrated guidance and control system with the compensation for the radome error is built by integrating the missile dynamics and the engagement kinematics between the missile and ground target on the longitudinal motion. Secondly, the model is transformed into a normal form by nonlinear coordinate transformation because the system is a time-varying system with mismatched uncertainties. Thirdly, an adaptive control law of the system is designed by adopting the sliding mode control theory, and the stability of the closed-loop system is also conducted. Finally, the simulation proves that the proposed integrated guidance and control scheme can effectively compensate for the radome error and ensure the hit-to-kill attack to the target.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Adaptive control law based integrated guidance and control design for missile with the radome error compensation


    Beteiligte:
    Guo, Jianguo (Autor:in) / Zhou, Yinghe (Autor:in) / Zhou, Min (Autor:in)


    Erscheinungsdatum :

    01.03.2024




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    L1 Adaptive Control Integrated Missile Autopilot and Guidance

    Erdos, David / Shima, Tal / Kharisov, Evgeny et al. | AIAA | 2012


    Adaptive, Integrated Guidance and Control for Missile Interceptors

    Sharma, Manu / Richards, Nathan | AIAA | 2004


    L1 Adaptive Control Integrated Missile Autopilot and Guidance

    Erdos, D. / Shima, T. / Kharisov, E. et al. | British Library Conference Proceedings | 2012


    Optimal design of integrated missile guidance and control

    Lin, Ching-Fang / Bibel, John / Ohlmeyer, Ernest et al. | AIAA | 1998