Abstract
AbstractThe merits of a perturbation theory based on a mean-to-osculating transformation that is purely periodic in the fast angle are investigated. The exact separation of the perturbed Keplerian dynamics into purely short-period effects and long-period mean frequencies is achieved by a non-canonical transformation, which, therefore, cannot be obtained by Hamiltonian methods. For this case, the evolution of the mean elements strictly adheres to the average behavior of the osculating orbit. However, due to the unavoidable truncation of perturbation solutions, the fact that this kind of theory confines in the mean variations the long-period terms of the semimajor axis, how tiny they may be, can have adverse effects in the accuracy of long-term semi-analytic propagations based on it.
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modeling and Simulation
Reference39 articles.
1. Arnas, D.: Analytic transformation from osculating to mean elements under J2 perturbation (2022). https://doi.org/10.48550/arXiv.2212.08746
2. Bhat, R.S., Frauenholz, R.B., Cannell, P.E.: TOPEX/POSEIDON orbit maintenance maneuver design. In: Astrodynamics 1989, American Astronautical Society. Univelt, Inc., P.O. Box 28130, San Diego, California 92198, USA, pp. 645–670 (1990)
3. Breakwell, J.V., Vagners, J.: On error bounds and initialization in satellite orbit theories. Celest. Mech. 2, 253–264 (1970). https://doi.org/10.1007/BF01229499
4. Brouwer, D.: Solution of the problem of artificial satellite theory without drag. Astron. J. 64, 378–397 (1959). https://doi.org/10.1086/107958
5. Brouwer, D., Clemence, G.M.: Methods of Celestial Mechanics. Academic Press, New York and London (1961)
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献