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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    Title :

    A robust guidance algorithm for the moon landing


    Contributors:

    Published in:

    Cosmic Research ; 51 , 6 ; 465-477


    Publication date :

    2013-11-01


    Size :

    13 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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