A Strap-Down Inertial Navigation/Spectrum Red-Shift/Star Sensor (SINS/SRS/SS) Autonomous Integrated System for Spacecraft Navigation

This paper presents a new Strap-down Inertial Navigation System/Spectrum Red-Shift/Star Sensor (SINS/SRS/SS) system integration methodology to improve the autonomy and reliability of spacecraft navigation using the spectrum red-shift information from natural celestial bodies such as the Sun, Jupiter...

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Detalles Bibliográficos
Autores principales: Gao, Zhaohui, Mu, Dejun, Zhong, Yongmin, Gu, Chengfan
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2018
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6069388/
https://www.ncbi.nlm.nih.gov/pubmed/29949905
http://dx.doi.org/10.3390/s18072039

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6069388/
https://www.ncbi.nlm.nih.gov/pubmed/29949905
http://dx.doi.org/10.3390/s18072039

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