One-Step Initial Alignment Algorithm for SINS in the ECI Frame Based on the Inertial Attitude Measurement of the CNS

To solve the problem of high-precision and fast initial alignment for the Strapdown Inertial Navigation System (SINS) under both dynamic and static conditions, the high-precision attitude measured by the celestial navigation system (CNS) is used as the reference information for the initial alignment...

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Detalles Bibliográficos
Autores principales: Tang, Jun, Bian, Hongwei, Ma, Heng, Wang, Rongying
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9315486/
https://www.ncbi.nlm.nih.gov/pubmed/35890803
http://dx.doi.org/10.3390/s22145123

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9315486/
https://www.ncbi.nlm.nih.gov/pubmed/35890803
http://dx.doi.org/10.3390/s22145123

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