H [sub infinity] optimal controller design and reduction for the intertial hold mode of the attitude control system of the XTE spacecraft
By: p.i. Zhong Ling Xu.
Contributors: United States. National Aeronautics and Space Administration.
Edition: .
Series: [NASA contractor report] -- NASA CR-195137.; NASA contractor report -- NASA CR-195137.
Publisher: Mathematics Dept., the University of Texas at Brownsville; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: Brownsville, Tex; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Space vehicles -- Attitude control systems.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0445-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.