Decoupled and coupled moons' ephemerides estimation strategies -- Application to the JUICE mission
M. Fayolle, D. Dirkx, V. Lainey, L.I. Gurvits, P.N.A.M. Visser

TL;DR
This paper compares decoupled and coupled strategies for estimating the ephemerides of moons, demonstrating that coupled methods can significantly reduce uncertainties and better account for dynamical interactions, especially for the Galilean moons during the JUICE mission.
Contribution
It provides an explicit formulation for the coupled estimation approach and compares its performance with the decoupled method using simulated data for the JUICE mission.
Findings
Coupled approach reduces radial uncertainties by over an order of magnitude.
Decoupled approach yields slightly lower tangential position errors.
Coupled method is more sensitive to moons' dynamical interactions.
Abstract
When reconstructing natural satellites' ephemerides from space missions' tracking data, the dynamics of the spacecraft and natural bodies are often solved for separately, in a decoupled manner. Alternatively, the ephemeris generation and spacecraft orbit determination can be performed concurrently. This method directly maps the available data set to the estimated parameters' covariances while fully accounting for all dynamical couplings. It thus provides a statistically consistent solution to the estimation problem, whereas this is not directly ensured with the decoupled strategy. For the Galilean moons in particular, the JUICE mission provides a unique opportunity for ephemerides improvement. For such a dynamically coupled problem, choosing between the two strategies will be influential. This paper provides a detailed, explicit formulation for the coupled approach, before comparing the…
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