The application provides a
satellite autonomous continuous maneuvering
orbit determination method with adaptive
process noise, and aims at the problem of
orbit determination accuracy reduction of a
satellite in a maneuvering process.The method is based on innovation, and adaptively adjusts
process noise in a non-maneuvering stage and a maneuvering stage, so that the
estimation accuracy reduction problem caused by fixed
noise parameters is solved, and the filter can more accurately represent the dynamic state of the
system.In a
Gaussian noise, compared with a traditional
unscented particle filter, the APNUPF exhibits better
orbit determination accuracy during the maneuvering, and even if the state mutates, the APNUPF can still maintain high-precision
orbit determination.In addition, in order to meet the actual
engineering requirements, the robustness and reliability of the method for
satellite autonomous continuous maneuvering
orbit determination are comprehensively verified under non-
Gaussian noise conditions.