Method for rejecting abnormal satellites in satellite navigation positioning
A satellite navigation and satellite position technology, applied in the field of satellite positioning, can solve the problems of strong application limitations, high calculation amount, and huge calculation amount, and achieve stable and reliable results, low calculation amount, and low logic complexity.
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[0035] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention.
[0036] Such as figure 1 As shown, the abnormal elimination method in the satellite navigation positioning of the present invention comprises the following steps:
[0037] Step S1, in the information preparation stage, obtain observation data of all visible stars at fixed time intervals, demodulate the obtained observation data information, obtain pseudorange and ephemeris information, and store them locally.
[0038] Step S2, then, after preparing the ephemeris and pseudorange information, enter the positioning information preparation stage, check whether the ephemeris information stored locally is in the same update cycle, if so, select the same update cycle ...
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