Construction of a consistent semianalytic theory of a planetary or moon orbiter perturbed by a third body
- 1 September 1982
- journal article
- research article
- Published by Springer Nature in Celestial Mechanics and Dynamical Astronomy
- Vol. 28 (1-2) , 155-169
- https://doi.org/10.1007/bf01230668
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- First order semianalytic satellite theory with recovery of the short period terms due to third body and zonal perturbationsActa Astronautica, 1981
- Perturbation Methods in Non-Linear SystemsPublished by Springer Nature ,1972