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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    Title :

    Guidance and Control for Mars Atmospheric Entry: Adaptivity and Robustness


    Contributors:

    Publication date :

    1997-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English