Abstract:
Objectives To improve the leakage envelope phenomenon of BeiDou navigation satellite system-3 (BDS-3) signal in space accuracy (SISA) integrity parameter to the comprehensive ranging errors induced by the orbit radial and clock errors, an improved SISA parameter index conversion algorithm based on 395 d of historical data is proposed.
Methods The algorithm consists of two parts: SISAocb (SISA parameter associated with orbit radial and clock accuracy) and SISAoc1 (SISA parameter associated with satellite clock speed accuracy) algorithm optimization. In SISAocb value optimization, the root mean square maximum of orbit radial and clock comprehensive error of all satellites in history is taken as the minimum limit of SISAocb. In the optimization of SISAoc1 algorithm, the maximum of first-order coefficient extracted through clock error fitting is compared with SISAoc1 calculated by free value formula of independent variable to determine the constant N in the SISAoc1 parameters calculation formula.
Results By analyzing measured data of 8 months, the advantages of the proposed algorithm are verified. The new algorithm can achieve the zero leakage envelope of SISAoc parameters for satellite radial and clock errors (excluding significant anomalies in broadcast ephemeris for satellite abroad), and reduce the leakage envelope event of BDS-3 integrity parameter caused by unreasonable SISA broadcast values.
Conclusions The effective optimization algorithm and analysis results for BDS-3 SISAoc parameters can provide a valuable reference for the upgrading and construction of BDS-3 system integrity service.