ERROR ANALYSIS OF QUATERNION TRANSFORMATIONS

doi:10.1109/7.85036

完整後設資料紀錄

DC 欄位	值	語言
dc.contributor.author	YEON, FJ	en_US
dc.contributor.author	YU, PL	en_US
dc.date.accessioned	2014-12-08T15:05:12Z	-
dc.date.available	2014-12-08T15:05:12Z	-
dc.date.issued	1991-07-01	en_US
dc.identifier.issn	0018-9251	en_US
dc.identifier.uri	http://dx.doi.org/10.1109/7.85036	en_US
dc.identifier.uri	http://hdl.handle.net/11536/3743	-
dc.description.abstract	Three transformation formulas are derived that related the quaternions to the direction cosine matrix used in strapdown inertial systems. Transformation errors associated with these formulas are fully analyzed. The drift errors evaluated under constant angular velocity have been shown to vary slightly among three different transformations. It is shown that the skew errors in three transformation schemes are not all intrinsically zero. Yet the scale errors may differ largely by two orders of magnitude among transformation schemes. This may become a selection criteria for selection of attitude transformation schemes.	en_US
dc.language.iso	en_US	en_US
dc.title	ERROR ANALYSIS OF QUATERNION TRANSFORMATIONS	en_US
dc.type	Article	en_US
dc.identifier.doi	10.1109/7.85036	en_US
dc.identifier.journal	IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS	en_US
dc.citation.volume	27	en_US
dc.citation.issue	4	en_US
dc.citation.spage	634	en_US
dc.citation.epage	639	en_US
dc.contributor.department	電控工程研究所	zh_TW
dc.contributor.department	Institute of Electrical and Control Engineering	en_US
dc.identifier.wosnumber	WOS:A1991GB87400006	-
dc.citation.woscount	1	-
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