Occultation timing observables added to radiometric tracking reduce LUMIO's transverse and normal position uncertainties by roughly 40-50% in covariance simulations.
V oyager 2 navigation to Uranus and Neptune,
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Stellar occultations in support of the LUMIO orbit determination
Occultation timing observables added to radiometric tracking reduce LUMIO's transverse and normal position uncertainties by roughly 40-50% in covariance simulations.