The performance of the controller is the key to ensure that the missile has a good stability and controllability in the guidance of flight. Without considering the coupling among channels, the three-channel missile body mathematical model of BTT-90 missile is established, and the model is based on BTT control technology. The Backstepping controller is designed and BTT-90 missile closed loop control system is constructed respectively. The result of simulation analysis shows that the control system can track the command signal rapidly, and has good dynamic and steady-state characteristics.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The design of backstepping controller based on BTT missile


    Beteiligte:
    Liu, Shanzhong (Autor:in) / Wei, Ling (Autor:in) / Liu, Yongbin (Autor:in)


    Erscheinungsdatum :

    01.08.2016


    Format / Umfang :

    782100 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Missile autopilot design and analysis based on backstepping

    Fan Jun-fang, / Su Zhong, / Cheng Zhen-xuan, | IEEE | 2010


    An Adaptive Backstepping Controller for a Hypersonic Air-Breathing Missile

    Bialy, B. / Klotz, J. / Curtis, J. Willard et al. | AIAA | 2012


    An Adaptive Backstepping Controller for a Hypersonic Air-Breathing Missile

    Bialy, B. / Klotz, J. / Curtis, J. et al. | British Library Conference Proceedings | 2012


    Missile Autopilot Design During Boost Phase Using Robust Backstepping Approach

    Lee, Seokwon / Kim, Youdan / Moon, Gwanyoumg et al. | AIAA | 2015