Guidance and Control for Mars Atmospheric Entry: Adaptivity and Robustness

Details Guidance and Control for Mars Atmospheric Entry: Adaptivity and Robustness Guidance and Control for Mars Atmospheric Entry: Adaptivity and Robustness

Jan 1997

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1997stin...0060813l&link_type=abstract

Technical Report, Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States

Mathematics

Adaptive Control, Approach Control, Control Theory, Atmospheric Entry, Mars Atmosphere, Mars (Planet), Mars Landing, Spacecraft Guidance, Space Navigation, Robustness (Mathematics), Velocity Distribution

Scientific paper

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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