Cargando…
A Gyroless Algorithm with Multi-Hypothesis Initialization for Projectile Navigation
Projectiles are subjected to a high acceleration shock at launch (20,000 g and higher) and can spin very fast. Thus, the components of onboard navigation units must therefore withstand such constraints in addition to being inexpensive. This makes only a few inertial sensors suitable for projectiles...
Autores principales: | Jardak, Nabil, Adam, Ronan, Changey, Sébastien |
---|---|
Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2021
|
Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8617698/ https://www.ncbi.nlm.nih.gov/pubmed/34833563 http://dx.doi.org/10.3390/s21227487 |
Ejemplares similares
-
LSTM-Based Projectile Trajectory Estimation in a GNSS-Denied Environment †
por: Roux, Alicia, et al.
Publicado: (2023) -
Treatment of Extended Kalman Filter Implementations for the Gyroless Star Tracker
por: Critchley-Marrows, Joshua J. R., et al.
Publicado: (2022) -
The Potential of LEO Satellite-Based Opportunistic Navigation for High Dynamic Applications
por: Jardak, Nabil, et al.
Publicado: (2022) -
Practical Use of Starlink Downlink Tones for Positioning
por: Jardak, Nabil, et al.
Publicado: (2023) -
The role of initial speed in projectile impacts into light granular media
por: Huang, Kai, et al.
Publicado: (2020)