This article deals with the problem of multi-objective regulating and protecting control for a ducted rocket, in order to get maximum thrust while avoiding extremely dangerous phenomenon like inlet buzz. First, the mathematical models involving gas flow regulating system and ducted rocket are introduced. The description of inlet buzz margin is also given and analyzed. Second, the multi-objective switching control problem of ducted rocket is proposed and discussed. Third, a robust bumpless transfer scheme for solving the problem is presented. The designed bumpless transfer compensator based on model reference adaptive sliding-mode control ensures that the switched system performs a smooth transition at the transfer moment. The stability analysis is then given utilizing the Lyapunov functional approach. Finally, the bumpless transfer strategy is applied to the ducted rocket control system, and the simulation results show its effectiveness.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Multi-objective regulating and protecting control for ducted rocket using a bumpless transfer scheme


    Beteiligte:
    Bao, Wen (Autor:in) / Qi, Yiwen (Autor:in) / Chang, Juntao (Autor:in)


    Erscheinungsdatum :

    01.02.2013


    Format / Umfang :

    15 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt





    Performance of ducted rocket

    Kassner, R.R. / Gobetz, F.W. | Engineering Index Backfile | 1960


    Bumpless Transfer(BT) Techniques for Predictive Control

    Zheng, J.-g. / Shi, R. / Wang, M.-x. | British Library Online Contents | 2003



    Control system design and experiment of needle-type gas regulating system for ducted rocket

    Niu, W-Y / Bao, W / Chang, J et al. | SAGE Publications | 2010