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dc.contributor.authorJIANG, YFen_US
dc.contributor.authorLIN, YPen_US
dc.date.accessioned2014-12-08T15:04:57Z-
dc.date.available2014-12-08T15:04:57Z-
dc.date.issued1992-04-01en_US
dc.identifier.issn0018-9251en_US
dc.identifier.urihttp://dx.doi.org/10.1109/7.144574en_US
dc.identifier.urihttp://hdl.handle.net/11536/3470-
dc.description.abstractThree improved algorithms for strapdown attitude computation utilizing accumulated gyro increments from the previous and current update are developed and evaluated analytically under classical coning motion. The error criterion of Miller [6] is now derived directly from the rotation vector concept. The accuracy of updating rotation vector estimation can be improved at least two orders of magnitude as compared with those of conventional algorithms. The proposed algorithm is equivalent to increasing the number of gyro samples used in the conventional method and it requires less computer loading also.en_US
dc.language.isoen_USen_US
dc.titleIMPROVED STRAPDOWN CONING ALGORITHMSen_US
dc.typeArticleen_US
dc.identifier.doi10.1109/7.144574en_US
dc.identifier.journalIEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMSen_US
dc.citation.volume28en_US
dc.citation.issue2en_US
dc.citation.spage484en_US
dc.citation.epage490en_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:A1992JC43100017-
dc.citation.woscount21-
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