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High-fidelity modeling of semi-autonomous attitude control during aerobraking

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dc.contributor.author Lyons, D. T. en_US
dc.contributor.author Johnson, W. en_US
dc.contributor.author Longuski, J. M. en_US
dc.date.accessioned 2004-09-17T07:27:23Z
dc.date.available 2004-09-17T07:27:23Z
dc.date.issued 2002-08-05 en_US
dc.identifier.citation AIAA/AAS Astrodynamics Specialist Conference en_US
dc.identifier.citation Monterey, CA, USA en_US
dc.identifier.clearanceno 02-1963 en_US
dc.identifier.uri http://hdl.handle.net/2014/9806
dc.description.abstract We investigate the automation of a Mars aerobraking vehicle that uses reaction wheels for attitude and angular momentum control during atmospheric flythrough. en_US
dc.format.extent 3435468 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other aerobraking Mars orbiters en_US
dc.title High-fidelity modeling of semi-autonomous attitude control during aerobraking en_US


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