Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    AUTOPILOT DESIGN FOR AN AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL



    Kongress:

    Congress; 28th, International Council of the Aeronautical Sciences; ICAS 2010 proceedings ; 2012 ; Brisbane, Australia



    Erscheinungsdatum :

    01.01.2012


    Format / Umfang :

    ICAS2012-P5.4


    Anmerkungen:

    Includes bibliographical references and author index; Held in e-store (RMS)



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Adaptive filtered backstepping control for integrated missile guidance and autopilot

    Liang, Xiao-Ling / Hou, Ming-Zhe / Duan, Guang-Ren | IEEE | 2014


    Missile autopilot design and analysis based on backstepping

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



    Missile Autopilot Design During Boost Phase Using Robust Backstepping Approach

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


    Autopilot Design for Agile Missile Using Time-Varying Control Technique

    Lee, H. C. / Choi, Y. S. / Choi, J. W. et al. | British Library Conference Proceedings | 2004