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Modeling and Analysis of Micro-Spacecraft Attitude Sensing with Gyrowheel
This paper proposes two kinds of approaches of angular rate sensing for micro-spacecraft with a gyrowheel (GW), which can combine attitude sensing with attitude control into one single device to achieve a compact micro-spacecraft design. In this implementation, during the three-dimensional attitude...
| Autores principales: | , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
MDPI
2016
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| Materias: | |
| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5017486/ https://www.ncbi.nlm.nih.gov/pubmed/27548178 http://dx.doi.org/10.3390/s16081321 |