Apparatus for time synchronizing based on common view of multiple satellites and filtering and method thereof
A time synchronization and common viewing technology, applied in the field of satellite navigation, can solve the problems of being vulnerable to damage, vulnerable to high mountains, blocked by tall buildings, and unusable
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Embodiment 1
[0060] A time synchronization device based on multi-satellite common viewing and α-β filtering, such as figure 1 As shown, it includes: a connected time synchronization module installed in two pseudolite stations; the time synchronization module includes: a multi-channel receiver module, a communication module, an information processing and clock correction module, wherein the multi-channel receiver module communicates with the The satellite is connected, and the multi-channel receiver module is connected to the communication module through the information processing and clock correction module; the two time synchronization modules are connected through their respective communication modules;
[0061] Among them, the multi-channel receiver is responsible for the extraction of the pseudo-range of the current observation satellite and the calculation of the message, the information processing and clock correction module is responsible for the accurate estimation of the clock diff...
Embodiment 2
[0064] A time synchronization method based on multi-satellite common view and α-β filtering, such as figure 2 shown, including:
[0065] Step 1. Use the multi-channel receivers of the two pseudolite stations A and B to capture, track and measure the navigation satellites observed respectively, and obtain the position of the measured satellite and the pseudolite positions relative to the pseudolite stations A and B. distance, and calculate the relative clock error of the pseudolite station;
[0066] By observing the locations of the two pseudolites respectively, the observations of pseudolite stations A and B at the same time t are obtained: the satellite position of satellite i at time t and pseudoranges and
[0067] Assume that the clock errors observed by pseudolite stations A and B through satellite i at time t are respectively δt iA and δt iB , by correcting the errors and delays of the pseudo-range observations, the clock errors of the two pseudolite stations A ...
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