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Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems
This paper presents rich new families of relative orbits for spacecraft formation flight generated through the application of continuous thrust with only minimal intervention into the dynamics of the problem. Such simplicity facilitates implementation for small, low-cost spacecraft with only positio...
| Autores principales: | , , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
Springer Netherlands
2018
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| Materias: | |
| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7646313/ https://www.ncbi.nlm.nih.gov/pubmed/33184531 http://dx.doi.org/10.1007/s10569-017-9807-3 |