3 edition of H [sub infinity] optimal controller design and reduction for the intertial hold mode of the attitude control system of the XTE spacecraft found in the catalog.
H [sub infinity] optimal controller design and reduction for the intertial hold mode of the attitude control system of the XTE spacecraft
by Mathematics Dept., the University of Texas at Brownsville, National Aeronautics and Space Administration, National Technical Information Service, distributor in Brownsville, Tex, [Washington, DC, Springfield, Va
Written in English
|Statement||p.i. Zhong Ling Xu.|
|Series||[NASA contractor report] -- NASA CR-195137., NASA contractor report -- NASA CR-195137.|
|Contributions||United States. National Aeronautics and Space Administration.|
|The Physical Object|
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