A feedback linearization approach to spacecraft control using momentum exchange devices
By: John Edward Dzielski.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA-CR -- 172057.; NASA contractor report -- NASA CR-172057.
Publisher: The Charles Stark Draper Laboratory
Published: 1988
Place of publication: Cambridge, Mass
Language: eng
Format: Microform
Subjects: Space vehicles -- Attitude control systems.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 3 microfiches.