This invention discloses a GNSS precise
orbit determination method,
system, and medium for situations involving sudden reduction in
ground station networks and
satellite rejection. It relates to the field of GNSS
orbit determination technology and solves the technical problems of precise
orbit determination methods, such as strong dependence on highly redundant
ground station networks,
observability degradation leading to multi-peak solution spaces under sudden reduction in
ground station networks, and the difficulty in simultaneously achieving continuous product output and reliable delivery. This invention includes: acquiring multi-
system, multi-frequency
pseudorange and
carrier phase observations from available ground stations and their quality indices; calculating rejection levels; training neural operator manifold priors to output a low-dimensional manifold distribution of orbit-
clock errors; constructing three types of closed invariants as truth-free supervision constraints; establishing a differentiable
observable renderer to output observation predictions and
heteroscedasticity uncertainties; using generative posterior
inference under prior manifold constraints to output multimodal posterior samples of orbits and
clock errors; providing integrity bounds and consistency certificates based on closed constraints and residual structure checks; and continuously outputting verifiable
ephemeris products under conditions of sudden reduction in ground
station networks or local rejection.