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	Fine alignment method for rotary strapdown inertial navigation system based on augmented state [基于状态量扩维的旋转式捷联惯导系统精对准方法]
	Ye, W.; Zhai, F.; Cai, C.; Li, J.
刊名	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
	2019
卷号	45页码:912-918
关键词	Air navigation Errors Inertial navigation systems Kalman filters Navigation Observability Alignment methods Attitude alignments Initial alignment Installation error Key technologies Navigation accuracy Scale factor errors Strap-down inertial navigation systems Alignment
ISSN号	10015965
DOI	10.13700/j.bh.1001-5965.2018.0545
URL标识	查看原文
收录类别	EI
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5918508
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Ye, W.,Zhai, F.,Cai, C.,等. Fine alignment method for rotary strapdown inertial navigation system based on augmented state [基于状态量扩维的旋转式捷联惯导系统精对准方法][J]. Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,2019,45:912-918.
APA	Ye, W.,Zhai, F.,Cai, C.,&Li, J..(2019).Fine alignment method for rotary strapdown inertial navigation system based on augmented state [基于状态量扩维的旋转式捷联惯导系统精对准方法].Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,45,912-918.
MLA	Ye, W.,et al."Fine alignment method for rotary strapdown inertial navigation system based on augmented state [基于状态量扩维的旋转式捷联惯导系统精对准方法]".Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics 45(2019):912-918.

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