Optimization-based alignment for inertial navigation systems: Theory and algorithm

Inertial navigation system (INS) necessitates an alignment stage to determine the initial attitude at the very start. A novel alignment approach is devised by way of an optimization method, in contrast to the existing alignment methods, e.g., gyrocompassing and filtering techniques. This paper shows...

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Bibliographic Details
Published in:Aerospace science and technology Vol. 15; no. 1; pp. 1 - 17
Main Authors: Wu, Meiping, Wu, Yuanxin, Hu, Xiaoping, Hu, Dewen
Format: Journal Article
Language:English
Published: Issy-les-Moulineaux Elsevier SAS 01.01.2011
Elsevier
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ISSN:1270-9638, 1626-3219
Online Access:Get full text
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