2101.05340
SEMI-ANALYTICAL ESTIMATES FOR THE ORBITAL STABILITY OF EARTH’S SATELLITES
Irene De Blasi, Alessandra Celletti, Christos Efthymiopoulos
correctmedium confidence
- Category
- Not specified
- Journal tier
- Specialist/Solid
- Processed
- Sep 28, 2025, 12:55 AM
- arXiv Links
- Abstract ↗PDF ↗
Audit review
The candidate reproduces the paper’s three core claims with the same logic: (A) J2 is neither convex nor quasi-convex while satisfying the three-jet test; the geolunisolar normal form is non-convex but quasi-convex (Tables 6–9 and Definition 10/11). (B) The semimajor-axis stability time bound T2 follows from dL/dt = −∂H/∂λ and a sup-norm/mean-value estimate (eqs. (47)–(52)). (C) In the resonant normal form, I1+I2 is exactly conserved, implying near-conservation of I ≈ (e^2+i^2)/2 up to the remainder (eqs. (53)–(56)). Minor discrepancies are purely expository (e.g., “det A ≡ 0” vs. “≈ 0 within precision” and the dimensionality of u in the three-jet test).
Referee report (LaTeX)
\textbf{Recommendation:} minor revisions
\textbf{Journal Tier:} specialist/solid
\textbf{Justification:}
The manuscript combines high-order normal forms with concrete sup-norm bounds to deliver long-term stability estimates for orbits across practically relevant altitudes, and it documents non-degeneracy properties indicative of Nekhoroshev-type behavior. The methodology is standard but carefully implemented; numerical evidence is convincing. Small clarifications (numerical precision for det A in J2; vector dimensionality in the three-jet test) would further improve readability.