Method for evaluating ionospheric differential corrections of satellite navigation signals
A technology for satellite navigation signals and differential correction numbers, which is applied in the field of satellite navigation signals and can solve problems such as the influence and restriction of calculation accuracy, and the insufficient use of the ionospheric delay time-domain slowly changing characteristics.
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[0064] The present invention relates to a satellite navigation signal ionospheric differential correction estimation method, in particular to a satellite navigation signal ionospheric differential correction estimation method based on weighted Kalman filtering, see figure 1 As shown, the steps are as follows:
[0065] Step 1. According to the continuous tracking observation of the satellite by the ground reference station, the position of the ionospheric penetration point formed thereby is calculated, and the vertical delay of the ionosphere at each penetration point is extracted from the observations, and then these penetration points are used to The ionospheric vertical delay on the penetration point is used as an observation to construct a filtering model, which is the basis for the filter to be estimated, and the filtering model includes a state model and a measurement model. The state model is constructed through the slow-varying characteristics of the ionospheric delay, ...
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