Positioning system and positioning method of global navigation satellite system (GNSS) monitoring station
A positioning system and monitoring station technology, applied in satellite radio beacon positioning system, radio wave measurement system, measuring device, etc., can solve the problem of out-of-synchronization of monitoring satellites, achieve high-precision positioning, ensure high precision, and ensure accuracy and computational efficiency effects
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Embodiment 1
[0075] In this example, figure 1 Shown is a positioning system of a GNSS monitoring station. The positioning system includes: multiple satellites, GNSS reference stations and GNSS monitoring stations. The GNSS reference station is connected to the GNSS monitoring station through a communication link. The GNSS monitoring station is specifically used for: The first satellite carrier signal of each of the satellites.
[0076] Determine the first ephemeris data and the first observation data according to the first satellite carrier signal, determine the first satellite position of each satellite according to the first ephemeris data, and determine the first carrier phase corresponding to the first satellite position according to the first observation data Observations.
[0077] Receive the ephemeris time of each satellite and the differential correction parameters corresponding to the ephemeris time in real time through the communication link; determine the correction value of th...
Embodiment 2
[0097] In this example, if image 3 Shown is a positioning method of a GNSS monitoring station, which is applied to a CNSS monitoring station. The CNSS monitoring station is connected with a CNSS reference station through a communication link. The positioning method includes the following specific steps:
[0098] Step 110. Respectively receive a first satellite carrier signal of each of the plurality of satellites.
[0099] Step 120: Determine the first ephemeris data and the first observation data according to the first satellite carrier signal, determine the first satellite position of each satellite according to the first ephemeris data, and determine the first satellite position corresponding to the first satellite position according to the first observation data A carrier phase observation.
[0100] Step 130, receiving the ephemeris time of each satellite and the differential correction parameters corresponding to the ephemeris time in real time through the communication...
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