Research on In-Flight Alignment for Micro Inertial Navigation System Based on Changing Acceleration using Exponential Function

In order to guarantee the stable flight of a guided projectile, it is difficult to realize in-flight alignment for the micro inertial navigation system (MINS) during its short flight time. In this paper, a method based on changing acceleration using exponential function is proposed. First, double-ve...

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Detalles Bibliográficos
Autores principales: Xu, Yun, Zhou, Tong
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2018
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6356345/
https://www.ncbi.nlm.nih.gov/pubmed/30598021
http://dx.doi.org/10.3390/mi10010024

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6356345/
https://www.ncbi.nlm.nih.gov/pubmed/30598021
http://dx.doi.org/10.3390/mi10010024

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