Cargando…
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...
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 |
Ejemplares similares
-
Systematic Calibration for Ultra-High Accuracy Inertial Measurement Units
por: Cai, Qingzhong, et al.
Publicado: (2016) -
Accurate Compensation of Attitude Angle Error in a Dual-Axis Rotation Inertial Navigation System
por: Jiang, Rui, et al.
Publicado: (2017) -
Constraints on axion-like dark matter from a SERF comagnetometer
por: Bloch, Itay M., et al.
Publicado: (2023) -
A Three-Stage Accelerometer Self-Calibration Technique for Space-Stable Inertial Navigation Systems
por: Wu, Qiuping, et al.
Publicado: (2018) -
Analysis and Suppression of Nonlinear Error of Pendulous Integrating Gyroscopic Accelerometer at Instrument Level
por: Zhou, Xiaojun, et al.
Publicado: (2023)