Cargando…
The Optimal Design of Modulation Angular Rate for MEMS-Based Rotary Semi-SINS
In previous studies, the semi-strapdown inertial navigation system (SSINS), based on microelectromechanical system (MEMS) sensors, had realized cross-range measurement of attitude information of high-spinning projectiles through construction of a “spin reduction” platform of the roll axis. However,...
Autores principales: | Zhang, Jiayu, Li, Jie, Che, Xiaorui, Zhang, Xi, Hu, Chenjun, Feng, Kaiqiang, Xu, Tingjin |
---|---|
Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2019
|
Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6412288/ https://www.ncbi.nlm.nih.gov/pubmed/30744194 http://dx.doi.org/10.3390/mi10020111 |
Ejemplares similares
-
Optimal Rotational Angular Velocity Determination Method Based on Compound Rotary Semi-Strapdown Inertial Navigation System
por: Zhang, Chenming, et al.
Publicado: (2022) -
Analysis and Compensation of Modulation Angular Rate Error Based on Missile-Borne Rotation Semi-Strapdown Inertial Navigation System
por: Zhang, Jiayu, et al.
Publicado: (2018) -
Angular Rate Optimal Design for the Rotary Strapdown Inertial Navigation System
por: Yu, Fei, et al.
Publicado: (2014) -
Roll Angular Rate Measurement for High Spinning Projectiles Based on Redundant Gyroscope System
por: Mi, Jing, et al.
Publicado: (2020) -
Optimization of a New High Rotary Missile-Borne Stabilization Platform
por: Wei, Xiaokai, et al.
Publicado: (2019)