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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...
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| Publicado no: | Celest Mech Dyn Astron |
|---|---|
| Main Authors: | , , , , |
| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Springer Netherlands
2018
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| Assuntos: | |
| Acesso em linha: | https://ncbi.nlm.nih.gov/pmc/articles/PMC7646313/ https://ncbi.nlm.nih.gov/pubmed/33184531 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.1007/s10569-017-9807-3 |
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