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dc.contributor.authorClements, Emily B
dc.contributor.authorMendenhall, Jeffrey A.
dc.contributor.authorCaplan, David O.
dc.contributor.authorCahoy, Kerri
dc.date.accessioned2020-03-10T14:16:16Z
dc.date.available2020-03-10T14:16:16Z
dc.date.issued2019-01
dc.identifier.issn2327-4123
dc.identifier.urihttps://hdl.handle.net/1721.1/124133
dc.description.abstractIn contrast to large-budget space missions, risk-tolerant platforms such as nanosatellites may be better positioned to exchange moderate performance uncertainty for reduced cost and improved manufacturability. New uncertainty-based systems engineering approaches such as multidisciplinary optimization require the use of integrated performance models with input distributions, which do not yet exist for complex systems, such as laser communications (lasercom) payloads. In this paper, we present our development of a statistical, risk-tolerant systems engineering approach and apply it to nanosatellite-based design and architecture problems to investigate whether adding a statistical element to systems engineering enables improvements in performance, manufacturability, and cost. The scope of this work is restricted to a subset of nanosatellite-based lasercom systems, which are particularly useful given current momentum to field Earth-observing nanosatellite constellations and increasing challenges for data retrieval. We build uncertainty-based lasercom performance models for a low Earth orbiting (LEO) system being developed at MIT called the Nanosatellite Optical Downlink Experiment (NODE) as a reference architecture. Compared with a more traditional, deterministic systems engineering,we find our new Lasercom Uncertainty Modeling and Optimization Simulation (LUMOS) approach yields significant benefits including a lasercom downlink design with a 59% reduction in ground station diameter and a 46% reduction in space terminal power for equivalent probabilities of a LEO-ground system delivering 500 Gb/day. While we focus on a nanosatellite lasercom application, the process for characterizing the input distributions and modeling performance is generalizable to other lasercom systems or space systems.en_US
dc.publisherA. Deepak Publishingen_US
dc.relation.isversionofhttps://jossonline.com/letters/lasercom-uncertainty-modeling-and-optimization-simulation-lumos-a-statistical-approach-to-risk-tolerant-systems-engineering-for-small-satellites/en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourceProf. Cahoy via Barbara Williamsen_US
dc.titleLasercom Uncertainty Modeling and Optimization Simulation (LUMOS): a Statistical Approach to Risk-tolerant Systems Engineering for Small Satellitesen_US
dc.typeArticleen_US
dc.identifier.citationClements, E. et al. (2019): JoSS, Vol. 8, No. 1, pp. 815-836en_US
dc.contributor.departmentLincoln Laboratoryen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.relation.journalJournal of Small Satellitesen_US
dc.eprint.versionAuthor's final manuscripten_US
dc.type.urihttp://purl.org/eprint/type/JournalArticleen_US
eprint.statushttp://purl.org/eprint/status/PeerRevieweden_US
dspace.date.submission2019-08-02T18:18:25Z
mit.journal.volume8en_US
mit.journal.issue1en_US
mit.licenseOPEN_ACCESS_POLICY
mit.metadata.statusComplete


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