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.
Guidance and Control for Mars Atmospheric Entry: Adaptivity and Robustness
1997-01-01
Miscellaneous
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English
Mars atmospheric entry guidance for optimal terminal altitude
Elsevier | 2018
|Mars atmospheric entry guidance for reference trajectory tracking
Online Contents | 2015
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