Cargando…
Efficiency of Hysteresis Rods in Small Spacecraft Attitude Stabilization
A semiempirical method for predicting the damping efficiency of hysteresis rods on-board small satellites is presented. It is based on the evaluation of dissipating energy variation of different ferromagnetic materials for two different rod shapes: thin film and circular cross-section rods, as a fun...
Autores principales: | Farrahi, Assal, Sanz-Andrés, Ángel |
---|---|
Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Hindawi Publishing Corporation
2013
|
Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC3899716/ https://www.ncbi.nlm.nih.gov/pubmed/24501579 http://dx.doi.org/10.1155/2013/459573 |
Ejemplares similares
-
Chaos in attitude dynamics of spacecraft
por: Liu, Yanzhu, et al.
Publicado: (2013) -
Spacecraft attitude determination and control
por: Wertz, James
Publicado: (1978) -
Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics
por: Wang, Chunbao, et al.
Publicado: (2019) -
Fundamentals of spacecraft attitude determination and control
por: Markley, F. Landis
Publicado: (2014) -
Fundamentals of spacecraft attitude determination and control
por: Markley, F Landis, et al.
Publicado: (2014)