Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems.

Arnot CS, McInnes CR, McKay RJ, Macdonald M, Biggs J

Open source

DOI
10.1007/s10569-017-9807-3
Published
2018
Container
Celestial mechanics and dynamical astronomy
Publisher
Not recorded
Open access
yes

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BibTeX

@article{allodium:10.1007/s10569-017-9807-3,
  title = {Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems.},
  author = {Arnot CS and McInnes CR and McKay RJ and Macdonald M and Biggs J},
  year = {2018},
  journal = {Celestial mechanics and dynamical astronomy},
  doi = {10.1007/s10569-017-9807-3},
  url = {https://doi.org/10.1007/s10569-017-9807-3}
}

RIS

TY  - JOUR
TI  - Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems.
AU  - Arnot CS
AU  - McInnes CR
AU  - McKay RJ
AU  - Macdonald M
AU  - Biggs J
PY  - 2018
JO  - Celestial mechanics and dynamical astronomy
DO  - 10.1007/s10569-017-9807-3
UR  - https://doi.org/10.1007/s10569-017-9807-3
ER  - 

APA

CS, A., CR, M., RJ, M., M, M., & J, B. (2018). Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems.. Celestial mechanics and dynamical astronomy. https://doi.org/10.1007/s10569-017-9807-3

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