In this paper, we address the atmospheric entry guidance and control problem for Mars precision landing. The guidance and control design is based on the principle of tracking a reference drag versus velocity profile in the entry flight corridor, which is determined by physical constraints of the flight. An integrated adaptive/robust control approach to atmospheric entry guidance and control is introduced to deal with different uncertainties.


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    Titel :

    Guidance and Control for Mars Atmospheric Entry: Adaptivity and Robustness


    Beteiligte:
    W. M. Lu (Autor:in) / D. S. Bayard (Autor:in)

    Erscheinungsdatum :

    1997


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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