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dc.contributor.advisorAndrew J. Staugler and Peter M. Kachmar.en_US
dc.contributor.authorLong, Stephen Michael, Ensignen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2010-04-28T17:10:22Z
dc.date.available2010-04-28T17:10:22Z
dc.date.copyright2003en_US
dc.date.issued2003en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/54618
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (p. 109).en_US
dc.description.abstractThe traditional approach to simulation-based system design results in a stovepiped development process where subsystems are developed independently and integration requirements are then levied on the system architecture. For applications like the MK6 Life Extension program, where a modular system architecture is the primary design goal, this method of simulation-based design is inadequate. Sponsored by the System Engineering System Design and Analysis Group at the Draper Laboratory, this thesis proposes an alternate top-down approach to simulation-based design, where the system architecture is established first, and the system is developed in an integrated fashion. Through this approach, the modularity requirements are then levied on the subsystems according to the integrated system architecture. In this thesis, a system-level simulation concept is developed via this approach to facilitate analysis of key guidance system design issues and evaluation of integrated system requirements. The simulation concept, which utilizes existing modeling and simulation tools, is validated through the design of a candidate guidance system and its usefulness is illustrated via selected guidance system modularity studies.en_US
dc.description.statementofresponsibilityby Stephen Michael Long.en_US
dc.format.extent109 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.titleSimulation methods for the development of modular strategic guidance systemsen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc601570509en_US


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