Pages that link to "Item:Q2028712"
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The following pages link to Hamiltonian perturbation solutions for spacecraft orbit prediction. The method of Lie transforms (Q2028712):
Displaying 13 items.
- Symmetric reduction and Hamilton-Jacobi equation of rigid spacecraft with a rotor (Q398237) (← links)
- Orbit propagation with Lie transfer maps in the perturbed Kepler problem (Q1405361) (← links)
- Brouwer's satellite solution redux (Q2052953) (← links)
- A deep dive into the \(2g+h\) resonance: separatrices, manifolds and phase space structure of navigation satellites (Q2073341) (← links)
- Closed-form perturbation theory in the restricted three-body problem without relegation (Q2138494) (← links)
- Element sets for high-order Poincaré mapping of perturbed Keplerian motion (Q2203841) (← links)
- Nekhoroshev estimates for the orbital stability of Earth's satellites (Q2688284) (← links)
- Applications of the Hamilton — Jacobi theory to the optimisation of orbital transfer (Q4374236) (← links)
- On mean elements in artificial-satellite theory (Q6171490) (← links)
- Analytical investigation about long-lifetime science orbits around Galilean moons (Q6546541) (← links)
- Free and forced inclinations of orbits perturbed by the central body's oblateness and an inclined third body (Q6546544) (← links)
- Higher-order composition of short- and long-period effects for satellite analytical ephemeris computation (Q6591773) (← links)
- Nonlinear effects of the central body oblateness on the coplanar dynamics of solar sails (Q6610862) (← links)
