Accurate Compensation of Attitude Angle Error in a Dual-Axis Rotation Inertial Navigation System

In the dual-axis rotation inertial navigation system (INS), besides the gyro error, accelerometer error, rolling misalignment angle error, and the gimbal angle error, the shaft swing angle and the axis non-orthogonal angle also affect the attitude accuracy. Through the analysis of the structure, we...

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Detalles Bibliográficos
Autores principales: Jiang, Rui, Yang, Gongliu, Zou, Rui, Wang, Jing, Li, Jing
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2017
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5375901/
https://www.ncbi.nlm.nih.gov/pubmed/28304354
http://dx.doi.org/10.3390/s17030615

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5375901/
https://www.ncbi.nlm.nih.gov/pubmed/28304354
http://dx.doi.org/10.3390/s17030615

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