Cargando…
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...
| Autores principales: | , |
|---|---|
| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
MDPI
2018
|
| Materias: | |
| 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 |