The article discusses the control law of space single axis spin stabilized interceptors, relying on multiple solid fuel thruster engines for orbital control. By analyzing the motion law of the terminal guidance segment with mathematical simulation, an effective divergence control method with proportional guidance is derived. Moreover, the authors go on to discuss the principle of selecting various control parameters, and measures for reducing the off target amount, which have reference value in studying and developing similar types of space interceptors in China.


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    Titel :

    Control Law of Terminal-Guidance Segment of Space Interceptors


    Beteiligte:
    Y. Yingbo (Autor:in) / Z. Huizhong (Autor:in)

    Erscheinungsdatum :

    1996


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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