The application discloses a high-precision time offset autonomous calculation method and
system based on
satellite speed v and gravity acceleration g. By establishing a closed correlation between the gravity
field strength and the
orbital speed, the traditional multi-parameter relativistic time correction model is simplified to a closed-form calculation depending on only two in-
orbit measurable physical quantities, without the need for input of orbital
radius, universal gravitational constant, earth
mass, external
ephemeris, etc. The application has outstanding originality, simple calculation, strong autonomy and reliable precision, can realize a daily cumulative
time error of less than 1 ns, is suitable for low-
orbit satellites, navigation satellites,
constellation systems and various high-reliability time service scenarios, has a wide application range and high industrial value, and can significantly improve the autonomous time service capability of a
spacecraft and the stability of a
time system.