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dc.contributor.advisorAlvar Saenz-Otero and David W. Miller.en_US
dc.contributor.authorSchmidt, Frank Hall, Jren_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2013-11-18T20:41:47Z
dc.date.available2013-11-18T20:41:47Z
dc.date.issued2013en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/82490
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2013.en_US
dc.descriptionThis electronic version was submitted and approved by the author's academic department as part of an electronic thesis pilot project. The certified thesis is available in the Institute Archives and Special Collections.en_US
dc.description"June 2013." Cataloged from department-submitted PDF version of thesisen_US
dc.descriptionIncludes bibliographical references (p. 197-204).en_US
dc.description.abstractSRAM-based FPGAs are highly attractive for space applications due to their in-flight reconfigurability, decreased development time and cost, and increased design and testing flexibility. The Xilinx Virtex-5QV is the first commercially available Radiation Hardened By Design (RHBD) SRAM-based FPGA; however, not all of its internal components are hardened against radiation-induced errors. This thesis examines and quantifies the additional considerations and techniques designers should employ with a RHBD SRAM-based FPGA in a space-based processing system to achieve high operational reliability. Additionally, this work presents the application of some of these techniques to the embedded avionics design of the REXIS imaging payload on the OSIRIS-REx asteroid sample return mission.en_US
dc.description.statementofresponsibilityby Frank Hall Schmidt, Jr.en_US
dc.format.extent204 p.en_US
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/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleFault tolerant design implementation on radiation hardened by design SRAM-Based FPGAsen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc862235047en_US


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