According to the aircraft is under complex work hard to electromagnetic environment performance analysis of the issue, a vehicle body and control lead in ultra-wideband high power microwave (UWS-HPM) under the irradiation of coupling effect and experimental study. Use back to lose signal simulator with the repetitive; the change control the length of the wire, radiation orientation, irradiation parts and other measures to make the experiment generality. The results of the study show that: aircraft in more than 25 kV/m of field UWS-HPM irradiation, interference and make its crash. Interference coupling mechanism is energy electromagnetic pulse through the control lead into the control box, and influence the formation of the control order. On the basis of experiment, this paper analyzes the interference with various factors coupling relation, which for electromagnetic protection equipment provides a theoretical basis.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Control of the Flight Vehicle Cable over Wide Spectrum Radiation Effects Simulation Experiment Research


    Beteiligte:
    Lv, Yi (Autor:in)


    Erscheinungsdatum :

    2012


    Format / Umfang :

    6 Seiten




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Flight control system of Hypersonic Flight Experiment vehicle

    Ishimoto, Shinji / Takizawa, Minoru / Suzuki, Hirokazu et al. | AIAA | 1996


    Flight Control Design of Hypersonic Flight Experiment (HYFLEX) Vehicle

    Ishimoto, S. / Takizawa, M. / Suzuki, H. et al. | British Library Conference Proceedings | 1996


    Flight Simulation and Experiment

    Cai, Guowei / Chen, Ben M. / Lee, Tong Heng | Springer Verlag | 2011


    Flight Control Design of an Automatic Landing Flight Experiment Vehicle

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