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High-fidelity modeling of semi-autonomous attitude control during aerobrakingWe investigate the automation of a Mars aerobraking vehicle that uses reaction wheels for attitude and angular momentum control during atmospheric flythrough.
Document ID
20060029942
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/9806
Authors
Lyons, D. T.
Johnson, W.
Longuski, J. M.
Date Acquired
August 23, 2013
Publication Date
August 5, 2002
Subject Category
Astrodynamics
Distribution Limits
Public
Copyright
Other
Keywords
aerobraking Mars orbiters

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