Orbital perturbation coupling of primary oblateness and solar radiation pressure
Martin Lara, Elena Fantino, Roberto Flores

TL;DR
This paper analyzes how solar radiation pressure couples with Earth's oblateness to influence spacecraft orbits, deriving a Hamiltonian model that identifies stable configurations and bifurcation conditions for long-term orbit maintenance.
Contribution
It introduces a Hamiltonian framework for the coupled effects of radiation pressure and oblateness, providing analytical tools for understanding and predicting stable orbit regimes.
Findings
Identification of three parameter regimes with distinct dynamical behaviors
Derivation of fixed points corresponding to frozen orbits
Analytical expressions for bifurcation lines separating regimes
Abstract
Solar radiation pressure can have a substantial long-term effect on the orbits of high area-to-mass ratio spacecraft, such as solar sails. We present a study of the coupling between radiation pressure and the gravitational perturbation due to polar flattening. Removing the short-period terms via perturbation theory yields a time-dependent two-degree-of-freedom Hamiltonian, depending on one physical and one dynamical parameter. While the reduced model is non-integrable in general, assuming coplanar orbits (i.e., both Spacecraft and Sun on the equator) results in an integrable invariant manifold. We discuss the qualitative features of the coplanar dynamics, and find three regions of the parameters space characterized by different regimes of the reduced flow. For each regime, we identify the fixed points and their character. The fixed points represent frozen orbits, configurations for…
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