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

According to the application characteristics of the K-Rb-21Ne 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 thre...

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Bibliographic Details
Main Authors: Qingzhong Cai, Gongliu Yang, Wei Quan, Ningfang Song, Yongqiang Tu, Yiliang Liu
Format: Article
Language:English
Published: MDPI AG 2018-02-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/18/2/670