Abstract We consider the problems of control of the angular and trajectory motion of the Kliper re-entry vehicle. This spacecraft with a moderate hypersonic lift-to-drag ratio is designed according to the load-carrying frame scheme. Gas-dynamic engines, a split balancing flap, and an air brake are used as mounting devices of control.


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    Titel :

    Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere


    Beteiligte:
    Bobylev, A. V. (Autor:in) / Dyad’kin, A. A. (Autor:in) / Kobzev, V. I. (Autor:in) / Poedinok, V. M. (Autor:in) / Reshetin, A. G. (Autor:in) / Suprunenko, S. N. (Autor:in) / Jaroshevskii, V. A. (Autor:in)

    Erschienen in:

    Cosmic Research ; 46 , 1 ; 74-89


    Erscheinungsdatum :

    2008-02-01


    Format / Umfang :

    16 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere

    Bobylev, A. V. / Dyad’kin, A. A. / Kobzev, V. I. et al. | Springer Verlag | 2008


    Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere

    Bobylev, A. V. / Dyad’kin, A. A. / Kobzev, V. I. et al. | Online Contents | 2008



    Distributed Global Trajectory Optimization of a Moderate Lift-to-Drag Re-Entry Vehicle

    Mooij, E. / Hanninen, G. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009


    Variation and control of range traveled in atmosphere by high-drag variable-lift entry vehicle

    Cheatham, D.C. / Young, J.W. / Eggleston, J.M. | Engineering Index Backfile | 1960