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Error Analysis of the K-Rb-(21)Ne Comagnetometer Space-Stable Inertial Navigation System

According to the application characteristics of the K-Rb-(21)Ne comagnetometer, a space-stable navigation mechanization is designed and the requirements of the comagnetometer prototype are presented. By analysing the error propagation rule of the space-stable Inertial Navigation System (INS), the th...

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Detalles Bibliográficos
Autores principales: Cai, Qingzhong, Yang, Gongliu, Quan, Wei, Song, Ningfang, Tu, Yongqiang, Liu, Yiliang
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2018
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5855240/
https://www.ncbi.nlm.nih.gov/pubmed/29495274
http://dx.doi.org/10.3390/s18020670