On analytic modeling of Lunar perturbations of artificial satellites of the Earth
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Publication:1824438
DOI10.1007/BF00051484zbMath0682.70025MaRDI QIDQ1824438
Publication date: 1989
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
method of averagingclassical series expansionsMoon's direct gravitational force on artificial Earth satellites
Computational methods for problems pertaining to mechanics of particles and systems (70-08) Differential geometric methods (tensors, connections, symplectic, Poisson, contact, Riemannian, nonholonomic, etc.) for problems in mechanics (70G45) Orbital mechanics (70M20)
Related Items (14)
The dynamical structure of the MEO region: long-term stability, chaos, and transport ⋮ Bifurcation of Lunisolar Secular Resonances for Space Debris Orbits ⋮ A new method for computing the spectrum of the gravitational perturbations on satellite orbits ⋮ Analytical development of the lunisolar disturbing function and the critical inclination secular resonance ⋮ Nekhoroshev estimates for the orbital stability of Earth's satellites ⋮ Resonances in the Earth's space environment (invited article) ⋮ Dynamics of Resonances and Equilibria of Low Earth Objects ⋮ Third-body perturbation in the case of elliptic orbits for the disturbing body ⋮ Towards a sustainable exploitation of the geosynchronous orbital region ⋮ An efficient algorithm for orbital evolution of artificial satellite ⋮ An analytical theory for avoidance collision between space debris and operating satellites in LEO ⋮ On analytic modeling of Lunar perturbations of artificial satellites of the Earth ⋮ Reduced motion equations of an axisymmetric body spinning on a horizontal surface via Lie symmetries ⋮ Luni-solar effects of geosynchronous orbits at the critical inclination
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