Abstract An algorithm of aerodynamic control is suggested for the descent of a spacecraft with a small lift-to-drag ratio into a predetermined region of space. The algorithm provides for an oriented descent with accepted accuracy for a subsequent operation of the landing control system. It needs less computing in comparison with traditional algorithms due to reduction of the initial nonlinear boundary value problem to the Cauchy problem.


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    Title :

    An Effective Algorithm of Aerodynamic Control over Spacecraft Descent


    Contributors:

    Published in:

    Cosmic Research ; 43 , 6 ; 450-455


    Publication date :

    2005-11-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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