Abstract The paper deals with a choice of the rational trajectory of motion of a landing module designed for the Moon landing, from the moment of its de-orbiting from the near-lunar orbit up to landing. An integrated conceptual basis is used to develop multistep terminal algorithms for guidance for the three segments of the descent.


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    Titel :

    A robust guidance algorithm for the moon landing


    Beteiligte:
    Zhukov, B. I. (Autor:in) / Zaiko, Yu. K. (Autor:in) / Likhachev, V. N. (Autor:in) / Sikharulidze, Yu. G. (Autor:in) / Tuchin, A. G. (Autor:in) / Fedotov, V. P. (Autor:in)

    Erschienen in:

    Cosmic Research ; 51 , 6 ; 465-477


    Erscheinungsdatum :

    2013-11-01


    Format / Umfang :

    13 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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