GLONASS almanac parameter estimation method used for satellite navigation
A technology of parameter estimation and satellite navigation, applied in the field of satellite navigation, can solve the problem of low accuracy of satellite position and velocity prediction, and achieve the effect of comprehensive GLONASS almanac parameters, simple fitting formula and high prediction accuracy
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[0038] The present invention will be described in detail below with reference to the accompanying drawings and examples.
[0039] The invention provides a method for estimating GLONASS almanac parameters used in satellite navigation. According to the satellite orbit data of a certain arc segment (generally referring to the valid period of GLONASS almanac parameters), a group of six satellite orbits based on the method of least squares estimation is used for fitting. Then, according to the physical meaning of the satellite orbit parameters and the definition of the GLONASS almanac parameters, the satellite motion state information of the GLONASS satellite at the time when the GLONASS satellite crosses the ascending node from south to north is calculated from the group of estimated orbit parameters (represented by the orbital element number ).
[0040] Specific steps include:
[0041] Step 1, establish the GLONASS almanac parameter fitting algorithm model, the state equation an...
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