We investigate the automation of a Mars aerobraking vehicle that uses reaction wheels for attitude and angular momentum control during atmospheric flythrough.
High-fidelity modeling of semi-autonomous attitude control during aerobraking
AIAA/AAS Astrodynamics Specialist Conference
2002-08-05
Conference paper
No indication
English
AIAA-2002-4909 High-Fidelity Modeling of Semi-Autonomous Attitude Control During Aerobraking
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