A Novel Rotation Scheme for MEMS IMU Error Mitigation Based on a Missile-Borne Rotation Semi-Strapdown Inertial Navigation System

In previous research, a semi-strapdown inertial navigation system (SSINS), based on micro-electro-mechanical system (MEMS) sensors, was able to realize over-range measurement of the attitude information of high-rotation missiles by constructing a single axis “spin reduction” platform. However, the M...

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Detalles Bibliográficos
Autores principales: Jing, Zhengyao, Li, Jie, Zhang, Xi, Feng, Kaiqiang, Zheng, Tao
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2019
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6479492/
https://www.ncbi.nlm.nih.gov/pubmed/30970555
http://dx.doi.org/10.3390/s19071683

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6479492/
https://www.ncbi.nlm.nih.gov/pubmed/30970555
http://dx.doi.org/10.3390/s19071683

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