Decoupled and coupled moons' ephemerides estimation strategies -- Application to the JUICE mission
arXiv:2308.06779 · doi:10.1016/j.pss.2022.105531
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 performances of the two state estimation methods for the JUICE test case. To this end, we used both decoupled and coupled models on simulated JUICE radiometric data. We compared the resulting covariances for the Galilean moons' states, and showed that the decoupled approach yields slightly lower formal errors for the moons' tangential positions. On the other hand, the coupled model can reduce the state uncertainties by more than one order of magnitude in the radial direction. It also proved more sensitive to the dynamical coupling between Io, Europa and Ganymede, allowing the solutions for the first two moons to fully benefit from JUICE orbital phase around Ganymede. However, many issues remain to be solved before a concurrent estimation strategy can be successfully applied to reconstruct the moons' dynamics over long timescales. Nonetheless, our analysis highlights promising ephemerides improvements and thus motivates future efforts to reach a coupled state solution for the Galilean moons.
References in corpus (15)
- The third realization of the International Celestial Reference Frame by very long baseline interferometry
- Resonance locking as the source of rapid tidal migration in the Jupiter and Saturn moon systems
- Spacecraft VLBI and Doppler tracking: algorithms and implementation
- On the contribution of PRIDE-JUICE to Jovian system ephemerides
- Planetary Radio Interferometry and Doppler Experiment (PRIDE) technique: A test case of the Mars Express Phobos fly-by
- Powering the Galilean Satellites with Moon-Moon Tides
- Desaturation Maneuvers and Precise Orbit Determination for the BepiColombo Mission
- Expected Precision of Europa Clipper Gravity Measurements
- A semi-analytical model of the Galilean satellites' dynamics
- Planetary Radio Interferometry and Doppler Experiment (PRIDE) of the JUICE mission
- APPROX -- Mutual approximations between the Galilean moons. The 2016-2018 observational campaign
- Propagation and Estimation of the Dynamical Behaviour of Gravitationally Interacting Rigid Bodies
- First stellar occultation by the Galilean moon Europa and upcoming events between 2019 and 2021
- Recovery of Bennu's Orientation for the OSIRIS-REx Mission: Implications for the Spin State Accuracy and Geolocation Errors
- Analytical framework for mutual approximations -- Derivation and application to Jovian satellites
Cited by in corpus (5)
- Planetary Radio Interferometry and Doppler Experiment (PRIDE) of the JUICE mission
- Combining astrometry and JUICE -- Europa Clipper radio science to improve the ephemerides of the Galilean moons
- Spacecraft VLBI tracking to enhance stellar occultations astrometry of planetary satellites
- Contribution of PRIDE VLBI products to the joint JUICE-Europa Clipper moons' ephemerides solution
- The Lense-Thirring effect on the Galilean moons of Jupiter