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dc.contributor.advisorDavid W. Miller and Michael C. Johnson.en_US
dc.contributor.authorHan, Christopher J. (Christopher Jinhyun)en_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2011-11-18T20:57:44Z
dc.date.available2011-11-18T20:57:44Z
dc.date.copyright2011en_US
dc.date.issued2011en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/67186
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2011.en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (p. 117-120).en_US
dc.description.abstractHoppers have recently emerged as a viable means for planetary exploration, and as with any new vehicle, significant testing is required to validate guidance, navigation, and control (GNC) algorithms. Furthermore, the structure, organization, and timing of the real-time software must be planned before software development begins in order to design an architecture which can match the needs and requirements of the vehicle as they evolve throughout its lifecycle. These issues are compounded in an academic environment, where software knowledge is not necessarily present and must be obtained and practiced before it can be applied. In addition, high student turnover rates can result in difficulty retaining institutional knowledge of the working software and causes further development delays while new students are trained. These problems were addressed by the TALARIS software team by implementing a flexible, modular software solution in LabVIEW on the National Instruments Real-Time Input/Output (RIO) board. After a brief introduction to the TALARIS testbed, the theory of flexibility and modularity is described as applied to the TALARIS software. In particular, the unique FPGA + PowerPC architecture and its importance to precise, real-time GNC execution are explored. Various software modules are isolated and analyzed, and several test cases are presented to illustrate the benefits of modular software with regard to development time, testing procedure, and debugging. Examples from software development, actuator characterization, and test campaigns illustrate the gradual evolution of the prototype software. Finally, a discussion of the conclusions from the work and future work is presented.en_US
dc.description.statementofresponsibilityby Christopher J. Han.en_US
dc.format.extent137 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.titleDevelopment of modular real-time software for the TALARIS lunar hopper testbeden_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc758505113en_US


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