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research
Minimum-fuel Attitude Control of a Rigid Body in Orbit by an Extended Method of Steepest-descent
Authors
I. Fluegge-Lotz
K. A. Hales
Publication date
Publisher
Abstract
Minimum fuel control of spacecraft in orbit using extended method of steepest descen
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oai:casi.ntrs.nasa.gov:1967002...
Last time updated on 02/09/2017
