GLONASS satellite orbit calculating method and system thereof
A technology of satellite orbit and calculation method, which is applied in the field of GLONASS satellite navigation system, and can solve the problems of high-efficiency positioning, long integration time, and occupation of CPU resources, etc.
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[0050] Such as figure 1 , a kind of GLONASS high-efficiency orbit calculation system described in the present invention mainly has four components: a positioning receiver, a time judgment module, a GLONASS step-length integral orbit calculation module and a GLONASS high-efficiency orbit calculation module. The time judging module has the function of judging whether the reference time of the GLONASS satellite broadcast ephemeris has changed, and comparing the reference time with the satellite's current time value. When the satellite reference time changes, the time judgment module selects the GLONASS step-length integral orbit calculation module, and calculates the position and speed of the GLONASS satellite through multiple Runge-Kutta method integration; when the satellite reference time does not change, the time judgment module is faster than the satellite The size of the reference time and satellite launch time, if the current time is just greater than the reference time an...
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