In-Flight Alignment of Integrated SINS/GPS/Polarization/Geomagnetic Navigation System Based on Federal UKF

As a common integrated navigation system, the strapdown inertial navigation system (SINS)/global positioning system (GPS) can estimate velocity and position errors well. Many auxiliary attitude measurement systems can be used to improve the accuracy of attitude angle errors. In this paper, the in-fl...

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Detalles Bibliográficos
Autores principales: Cao, Songyin, Gao, Honglian, You, Jie
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9416158/
https://www.ncbi.nlm.nih.gov/pubmed/36015743
http://dx.doi.org/10.3390/s22165985

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9416158/
https://www.ncbi.nlm.nih.gov/pubmed/36015743
http://dx.doi.org/10.3390/s22165985

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