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Efficient and robust data collection using compact micro hardware, distributed bus architectures and optimizing software

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dc.contributor.author Chau, Savio
dc.contributor.author Vatan, Farrokh
dc.contributor.author Randolph, Vincent
dc.contributor.author Baroth, Edmund C.
dc.date.accessioned 2007-02-22T16:44:17Z
dc.date.available 2007-02-22T16:44:17Z
dc.date.issued 2006-07-09
dc.identifier.citation 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,Sacramento, California, July 9-12, 2006 en
dc.identifier.clearanceno 06-1617
dc.identifier.uri http://hdl.handle.net/2014/40120
dc.description.abstract In a conventional space system, the most cable intensive area in a spacecraft is probably the wiring to sensors. This is mainly because of the multitude of sensors, but it is also because of the centralized point-to-point architecture of these systems. Therefore, the first step toward cable reduction is to eliminate the large number of cables required by the centralized point-to-point architecture. There are two general approaches: distributed architecture and wireless network. This paper provides a survey of the technologies in these two areas. Careful trade studies have to be performed among the technologies for specific system design. en
dc.description.sponsorship NASA/JPL en
dc.format.extent 423595 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2006. en
dc.subject disributed bus hardware en
dc.subject micro hardware en
dc.subject sensor validation en
dc.title Efficient and robust data collection using compact micro hardware, distributed bus architectures and optimizing software en
dc.type Preprint en


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