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    Guidance and Control for Mars Atmospheric Entry: Adaptivity and Robustness (1997)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: 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.
    Keywords: Lunar and Planetary Science and Exploration
    Format: application/pdf
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