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

Published 2015 View Full Article

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Title
Optimal redundant sensor configuration for accuracy increasing in space inertial navigation system
Authors
Keywords
Inertial navigation system, Optimal configuration, Redundant sensor, Accuracy increasing, Reliability
Journal
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 47, Issue -, Pages 467-472
Publisher
Elsevier BV
Online
2015-10-20
DOI
10.1016/j.ast.2015.09.017

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