Optimal redundant sensor configuration for accuracy increasing in space inertial navigation system

标题
Optimal redundant sensor configuration for accuracy increasing in space inertial navigation system
作者
关键词
Inertial navigation system, Optimal configuration, Redundant sensor, Accuracy increasing, Reliability
出版物
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 47, Issue -, Pages 467-472
出版商
Elsevier BV
发表日期
2015-10-20
DOI
10.1016/j.ast.2015.09.017

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