Local Observability Analysis of Star Sensor Installation Errors in a SINS/CNS Integration System for Near-Earth Flight Vehicles

Strapdown inertial navigation system/celestial navigation system (SINS/CNS) integrated navigation is a fully autonomous and high precision method, which has been widely used to improve the hitting accuracy and quick reaction capability of near-Earth flight vehicles. The installation errors between S...

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Detalles Bibliográficos
Autores principales: Yang, Yanqiang, Zhang, Chunxi, Lu, Jiazhen
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2017
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5298740/
https://www.ncbi.nlm.nih.gov/pubmed/28275211
http://dx.doi.org/10.3390/s17010167

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5298740/
https://www.ncbi.nlm.nih.gov/pubmed/28275211
http://dx.doi.org/10.3390/s17010167

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