The invention provides a low-
orbit navigation
constellation autonomous
orbit determination method and
system under a weak inter-
satellite topological structure, and relates to the technical field of
satellite orbit determination, and the method comprises the steps: obtaining various
observation data of an inter-
satellite link on a predetermined orbit, and carrying out the preprocessing of the various
observation data; establishing a synchronous observation equation of orbit and
clock correction parameters by adopting a segmented linear polynomial satellite
clock correction modeling method, generating orbit,
clock correction and related error parameters combining satellite-borne GNSS and inter-satellite
link data, and forecasting; based on an
error analysis result, multiple key features are extracted from the generated orbit,
clock error and related error parameters to serve as input of a parameter prediction model, and a parameter
time sequence of four types of prediction including
relative weight, inter-satellite link hardware
delay, low-orbit satellite
clock error and unmodeled error is obtained through output; and uploading the predicted parameter
time sequence and the broadcast
ephemeris to a main satellite together, and transmitting to each sub-satellite by the main satellite through an inter-satellite link to realize distributed autonomous
orbit determination of the sub-satellites.