Dynamics of artificial satellite orbits with tesseral resonances including the effects of luni- solar perturbations

DOI10.1080/02681119708806247zbMath0943.70017OpenAlexW2005389463MaRDI QIDQ4237735

Kathleen C. Howell, Todd A. Ely

Publication date: 1 June 1999

Published in: Dynamics and Stability of Systems (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/02681119708806247

zbMATH Keywords

luni-solar perturbationseccentric and inclined satellite orbitseffect of Earth potentialgeopotential tesseral harmonicsgravity terms

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20) Nonlinear resonances for nonlinear problems in mechanics (70K30)

Related Items (12)

The dynamical structure of the MEO region: long-term stability, chaos, and transport ⋮ Proper elements for space debris ⋮ Bifurcation of Lunisolar Secular Resonances for Space Debris Orbits ⋮ Analytical development of the lunisolar disturbing function and the critical inclination secular resonance ⋮ Nekhoroshev estimates for the orbital stability of Earth's satellites ⋮ Element sets for high-order Poincaré mapping of perturbed Keplerian motion ⋮ Resonances in the Earth's space environment (invited article) ⋮ Dynamics of Resonances and Equilibria of Low Earth Objects ⋮ On the dynamics of space debris: 1:1 and 2:1 resonances ⋮ On the predictability and robustness of Galileo disposal orbits ⋮ An efficient algorithm for orbital evolution of artificial satellite ⋮ Dynamical investigation of minor resonances for space debris

Cites Work

• Regular and chaotic dynamics.
• Luni-solar effects of geosynchronous orbits at the critical inclination
• A note on Hansen's coefficients in satellite theory
• Unnamed Item

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