The automatic landing flight experiment, ALFLEX, was conducted by the National Aerospace Laboratory (NAL) and National Space Development Agency of Japan (NASDA), in order to develop their automatic landing technology for future unmanned reentry space vehicle. All the flight experiments were successfully completed. Because the ALFLEX vehicle is an unmanned and autonomous vehicle which has tip-fin wings, the flight control law has to achieve high-response-performance and robustness simultaneously. In this paper, the design method used to achieve these objeetives is presented, as well as the results of flight experiments related to performance and robustness.


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    Titel :

    Robust flight control law design for an automatic landing flight experiment


    Weitere Titelangaben:

    Entwurf einer robusten Flugregelung für ein automatisches Landungsexperiment


    Beteiligte:
    Ohno, M. (Autor:in) / Yamaguchi, Y. (Autor:in) / Hata, T. (Autor:in) / Takahama, M. (Autor:in) / Miyazawa, Y. (Autor:in) / Izumi, T. (Autor:in)

    Erschienen in:

    Control Engineering Practice ; 7 , 9 ; 1143-1151


    Erscheinungsdatum :

    1999


    Format / Umfang :

    9 Seiten, 12 Bilder, 1 Tabelle, 7 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Robust Flight Control Law Design for Automatic Landing Flight Experiment

    Ohno, M. / Yamaguchi, Y. / Hata, T. et al. | British Library Conference Proceedings | 1999


    Flight Control Design of an Automatic Landing Flight Experiment Vehicle

    Atsushi Fujimori / Munerou Kurozumi / Peter N. Nikiforuk et al. | AIAA | 2000


    Flight control system for the Automatic Landing Flight Experiment

    Miyazawa, Yoshikazu / Ishikawa, Kazutoshi / Motoda, Toshikazu et al. | AIAA | 1996