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
05.08.2002
Aufsatz (Konferenz)
Keine Angabe
Englisch
AIAA-2002-4909 High-Fidelity Modeling of Semi-Autonomous Attitude Control During Aerobraking
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