Completeness support information parameter generation method and system suitable for Beidou
A technology that supports information and integrity, applied in the field of satellite navigation, can solve the problems of lack of long-term stable navigation data, short operation time of Beidou system, large integrity risk, etc., and achieve the effect of reducing integrity risk.
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Embodiment 1
[0067] Such as figure 1 As shown in the flow chart, this embodiment provides a method for generating integrity support information parameters suitable for Beidou, and the method includes the following steps:
[0068] S1. Set the initial sampling time and sampling interval, sample the satellite observation data of each orbit of the Beidou system according to the sampling interval within the sampling time, and obtain the satellite observation data sets of each orbit of the Beidou; take 15 minutes as the sampling interval, Select 10 days of satellite data as the Beidou orbit satellite observation data set;
[0069] S2. Calculate the user distance error URE by using the satellite observation data in the Beidou orbit satellite observation data set to obtain the initial sample data set;
[0070] In specific implementation, such as figure 2 In the flow chart shown, step S2 specifically includes:
[0071] S21. Eliminate the abnormal observation data in the Beidou orbit satellite o...
Embodiment 2
[0140] Corresponding to Embodiment 1, the present invention also provides a system for generating integrity support information parameters suitable for Beidou.
[0141] In addition, the method of embodiment 1 of the present invention can also be by means of Figure 5 The architecture shown for Beidou integrity support information parameter generation system is implemented. Such as Figure 5 As shown, the integrity support information parameter generation system may include a satellite observation data acquisition module 1, a satellite observation data set processing module 2, an FCM classification module 3, a data set expansion module 4, a Beidou broadcast URA acquisition module 5, and a URA evaluation module 6 and information sending module 7; some modules can also have subunits for realizing its functions, for example, abnormal data removal unit 2-1 and URE calculation unit 2-2 can also be included in satellite observation data set processing module 2; The expansion module...
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