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dc.contributorPothiawala, A. (Asis)en_US
dc.contributorDahleh, Munther A.en_US
dc.contributorMassachusetts Institute of Technology. Laboratory for Information and Decision Systems.en_US
dc.date.accessioned2003-04-29T15:35:20Z
dc.date.available2003-04-29T15:35:20Z
dc.date.issued1990en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/3208
dc.descriptionCover title. On t.p. "[infinity]" is the mathematical symbol and subscript.en_US
dc.descriptionIncludes bibliographical references (p. 52-53).en_US
dc.description.sponsorshipSupported by the National Science Foundation. NSF 8810178-ECS Supported by the U.S. Army Research Office (Center for Intelligent Control Systems) DAAL03-86-K-0171en_US
dc.format.extent81 p.en_US
dc.format.extent3335305 bytes
dc.format.mimetypeapplication/pdf
dc.language.isoengen_US
dc.publisherLaboratory for Information and Decision Systems, Massachusetts Institute of Technology]en_US
dc.relation.ispartofseriesLIDS-P ; 1985en_US
dc.subject.lccTK7855.M41 E3845 no.1985en_US
dc.titleH [infinity] optimal control for the attitude control and momentum management of the space station A. Pothiawala, M.A. Dahleh.en_US


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