Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influence of the Luni-Solar Gravity, in Rotating and Inertial Cartesian Reference Frames
Crossref DOI link: https://doi.org/10.1007/978-3-030-64657-8_3
Published Online: 2021-04-13
Published Print: 2021
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Kéchichian, Jean Albert
Text and Data Mining valid from 2021-01-01
Version of Record valid from 2021-01-01
Chapter History
First Online: 13 April 2021