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	Initial attitude estimation and installation errors calibration of the IMU for plane by SINS/CNS integration
	Yuan, W.; Gui, M.; Ning, X.
刊名	Lecture Notes in Electrical Engineering
	2018
卷号	458页码:123-130
关键词	Air navigation Calibration Gyroscopes Inertial navigation systems Navigation systems Units of measurement Attitude estimation Autonomous navigation Celestial measurements Horizontal velocity Inertial measurement unit Installation error Integrated navigation Strap-down inertial navigation systems Errors
ISSN号	9789811064449
DOI	10.1007/978-981-10-6445-6_14
URL标识	查看原文
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5934196
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Yuan, W.,Gui, M.,Ning, X.. Initial attitude estimation and installation errors calibration of the IMU for plane by SINS/CNS integration[J]. Lecture Notes in Electrical Engineering,2018,458:123-130.
APA	Yuan, W.,Gui, M.,&Ning, X..(2018).Initial attitude estimation and installation errors calibration of the IMU for plane by SINS/CNS integration.Lecture Notes in Electrical Engineering,458,123-130.
MLA	Yuan, W.,et al."Initial attitude estimation and installation errors calibration of the IMU for plane by SINS/CNS integration".Lecture Notes in Electrical Engineering 458(2018):123-130.

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