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dc.contributor.authorJIANG, YFen_US
dc.contributor.authorLIN, YPen_US
dc.date.accessioned2014-12-08T15:05:02Z-
dc.date.available2014-12-08T15:05:02Z-
dc.date.issued1992-01-01en_US
dc.identifier.issn0018-9251en_US
dc.identifier.urihttp://dx.doi.org/10.1109/7.135435en_US
dc.identifier.urihttp://hdl.handle.net/11536/3568-
dc.description.abstractA systematic analysis of the observability of an inertial navigation system (INS) in ground alignment with Bar-Itzhack and Berman's error model is presented. It is shown that the unobservable states are separately contained in two decoupled subspaces. The constraints on the selection of unobservable states are discussed. An estimation algorithm which is derived fully from the horizontal velocity outputs for computing the misalignment angles is provided. It reveals that the azimuth error can be entirely estimated from the estimates of leveling error and leveling error rate, without using gyro output signals explicitly.en_US
dc.language.isoen_USen_US
dc.titleERROR ESTIMATION OF INS GROUND ALIGNMENT THROUGH OBSERVABILITY ANALYSISen_US
dc.typeArticleen_US
dc.identifier.doi10.1109/7.135435en_US
dc.identifier.journalIEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMSen_US
dc.citation.volume28en_US
dc.citation.issue1en_US
dc.citation.spage92en_US
dc.citation.epage97en_US
dc.contributor.department電控工程研究所zh_TW
dc.contributor.departmentInstitute of Electrical and Control Engineeringen_US
dc.identifier.wosnumberWOS:A1992HP65400008-
dc.citation.woscount46-
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