Show simple item record

dc.contributor.advisorMicahel Athans.en_US
dc.contributor.authorLublin, Leonarden_US
dc.date.accessioned2005-08-18T14:32:54Z
dc.date.available2005-08-18T14:32:54Z
dc.date.copyright1996en_US
dc.date.issued1996en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/10825
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.en_US
dc.descriptionIncludes bibliographical references (p. 165-168).en_US
dc.description.statementofresponsibilityby Leonard Lublin.en_US
dc.format.extent168 p.en_US
dc.format.extent11382347 bytes
dc.format.extent11382097 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582
dc.subjectAeronautics and Astronauticsen_US
dc.titleThe use of additional actuators to enhance performance robustnessen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Dept. of Aeronautics and Astronauticsen_US
dc.identifier.oclc35264026en_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record