A New In-Flight Alignment Method with an Application to the Low-Cost SINS/GPS Integrated Navigation System

The optimization-based alignment (OBA) methods, which are implemented by the optimal attitude estimation using vector observations—also called double-vectors—have proven to be effective at solving the in-flight alignment (IFA) problem. However, the traditional OBA methods are not applicable for the...

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Detalles Bibliográficos
Autores principales: Lu, Zhenglong, Li, Jie, Zhang, Xi, Feng, Kaiqiang, Wei, Xiaokai, Zhang, Debiao, Mi, Jing, Liu, Yang
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7014501/
https://www.ncbi.nlm.nih.gov/pubmed/31963286
http://dx.doi.org/10.3390/s20020512

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