A Dynamic Attitude Measurement System Based on LINS

A dynamic attitude measurement system (DAMS) is developed based on a laser inertial navigation system (LINS). Three factors of the dynamic attitude measurement error using LINS are analyzed: dynamic error, time synchronization and phase lag. An optimal coning errors compensation algorithm is used to...

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Detalles Bibliográficos
Autores principales: Li, Hanzhou, Pan, Quan, Wang, Xiaoxu, Zhang, Juanni, Li, Jiang, Jiang, Xiangjun
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2014
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4208163/
https://www.ncbi.nlm.nih.gov/pubmed/25177802
http://dx.doi.org/10.3390/s140916082

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4208163/
https://www.ncbi.nlm.nih.gov/pubmed/25177802
http://dx.doi.org/10.3390/s140916082

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