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Synthesizing an algorithm to control the angular motion of spacecraft equipped with an aeromagnetic deorbiting system
It is known that the synthesis of the relevant control law is performed and appropriate control devices are selected for specific tasks of controlling relative spacecraft motion. Flywheels, control moment gyroscopes, electromagnetic devices with permanent magnets and micro-jet engines are used as ac...
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| Main Authors: | , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
PC Technology Center
2020-02-01
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| Colecção: | Eastern-European Journal of Enterprise Technologies |
| Assuntos: | |
| Acesso em linha: | http://journals.uran.ua/eejet/article/view/192813 |
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