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Direct Kalman Filtering Approach for GPS/INS Integration

dc.contributor.authorQi, Honghui
dc.contributor.authorMoore, John
dc.date.accessioned2015-12-13T22:22:41Z
dc.date.available2015-12-13T22:22:41Z
dc.date.issued2002
dc.date.updated2015-12-11T07:58:11Z
dc.description.abstractWe present a novel Kalman filtering approach for GPS/INS integration. In the approach, GPS and INS nonlinearities are preprocessed prior to a Kalman filter. The GPS preprocessed data are taken as measurement input, while the INS preprocessed data are taken as additional information for the state prediction of the Kalman filter. The advantage of this approach, over the well-studied (extended) Kalman filtering approaches is that a simple and linear Kalman filter can be implemented to achieve significant computation saving with very competitive performance figures.
dc.identifier.issn0018-9251
dc.identifier.urihttp://hdl.handle.net/1885/72370
dc.publisherInstitute of Electrical and Electronics Engineers (IEEE Inc)
dc.sourceIEEE Transactions on Aerospace and Electronic Systems
dc.subjectKeywords: Computer simulation; Global positioning system; Inertial navigation systems; Sensor data fusion; State estimation; Data fusion Kalman filters; Kalman filtering
dc.titleDirect Kalman Filtering Approach for GPS/INS Integration
dc.typeJournal article
local.bibliographicCitation.issue2
local.bibliographicCitation.lastpage693
local.bibliographicCitation.startpage687
local.contributor.affiliationQi, Honghui, no formal affiliation
local.contributor.affiliationMoore, John, College of Engineering and Computer Science, ANU
local.contributor.authoruidMoore, John, u8202879
local.description.notesImported from ARIES
local.description.refereedYes
local.identifier.absfor090199 - Aerospace Engineering not elsewhere classified
local.identifier.ariespublicationMigratedxPub3213
local.identifier.citationvolume38
local.identifier.doi10.1109/TAES.2002.1008998
local.identifier.scopusID2-s2.0-0036544030
local.type.statusPublished Version

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