A Three-Stage Accelerometer Self-Calibration Technique for Space-Stable Inertial Navigation Systems

As a specific force sensor, the tri-axis accelerometer is one of the core instruments in an inertial navigation system (INS). During navigation, its measurement error directly induces constant or alternating navigation errors of the same order of magnitude. Moreover, it also affects the estimation a...

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Detalles Bibliográficos
Autores principales: Wu, Qiuping, Wu, Ruonan, Han, Fengtian, Zhang, Rong
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2018
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6164698/
https://www.ncbi.nlm.nih.gov/pubmed/30200366
http://dx.doi.org/10.3390/s18092888

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6164698/
https://www.ncbi.nlm.nih.gov/pubmed/30200366
http://dx.doi.org/10.3390/s18092888

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