Return to search

Reducing spacecraft state uncertainty through indirect trajectory optimization

Not available / text

Identiferoai:union.ndltd.org:UTEXAS/oai:repositories.lib.utexas.edu:2152/2381
Date28 August 2008
CreatorsZimmer, Scott Jason
Source SetsUniversity of Texas
LanguageEnglish
Detected LanguageEnglish
TypeThesis, text
Formatelectronic
RightsCopyright is held by the author. Presentation of this material on the Libraries' web site by University Libraries, The University of Texas at Austin was made possible under a limited license grant from the author who has retained all copyrights in the works.

Page generated in 0.0021 seconds