Artificial satellites orbits in 2:1 resonance: GPS constellation

Author:

Sampaio J.C.,Neto A.G.S.,Fernandes S.S.,Vilhena de Moraes R.,Terra M.O.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Tesseral harmonic perturbations of an artificial satellite;Garfinkel;Astron. J.,1965

2. Along-track oscillations of a satellite due to tesseral harmonics;Gedeon;AIAA J.,1967

3. An analytical treatment of resonance effects on satellite orbits;Lane;Celestial Mech.,1988

4. A solution of the ideal resonance problem for the case of libration;Jupp;Astron. J.,1969

5. Long-term evolution of artificial satellite orbits due to resonant tesseral harmonics;Ely;J. Astronaut. Sci.,1996

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2. Averaged model to study long-term dynamics of a probe about Mercury;Celestial Mechanics and Dynamical Astronomy;2018-01-18

3. Dynamical investigation of minor resonances for space debris;Celestial Mechanics and Dynamical Astronomy;2015-07-25

4. Comparison of mean and osculating stability in the vicinity of the (2:1) tesseral resonant surface;Acta Astronautica;2015-06

5. On the Dynamics of Space Debris: 1:1 and 2:1 Resonances;Journal of Nonlinear Science;2014-09-10

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