Beidou receiver and warm start method thereof
A receiver and hot start technology, which is applied in the field of Beidou navigation, can solve the problems of long startup time of the warm start technology, cannot meet the requirements and influences of the quick start of the Beidou receiver, and achieve the goal of realizing fast positioning after starting up and improving the time for the first positioning Effect
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Embodiment 1
[0051] see figure 1 , which is a schematic flow chart of the Beidou receiver hot start method provided in Embodiment 1 of the present invention, specifically as follows:
[0052] Step 10, the Beidou receiver obtains the time T' when the local satellite signal is received r .
[0053] We know that what satellite positioning needs is the precise position of the satellite participating in the positioning at the current moment and the distance from the satellite to the user at the current moment. In order to calculate the satellite position, we need the valid ephemeris and the transmission time T of the satellite signal t ; In order to get the distance from the satellite to the user, we use the ranging method based on TOA, we need to know the sending time T of the satellite signal t and local reception time T r . The ephemeris can be stored in the memory of the receiver, and the local time can be recorded by the RTC unit of the receiver. Therefore, if you want to locate quick...
Embodiment 2
[0087] see image 3 The embodiment of the present invention provides a Beidou receiver, including a receiving time unit 100, a transmitting time estimating unit 200, a last positioning calculation unit 300, a transmitting time reconstruction unit 400, an error adjustment unit 500, and a calculating and positioning unit 600, specifically as follows:
[0088] The receiving time unit 100 is used to obtain the time T' of receiving satellite signals locally r .
[0089] The transmission moment estimation unit 200 is used for receiving the satellite signal locally according to the moment T' r Calculate roughly estimated satellite signal launch time T te .
[0090] The last positioning calculation unit 300 is used to roughly estimate the satellite signal transmission time T according to the satellite te Calculate the distance and propagation time from the satellite to the last location of the user.
[0091] The launch time reconstruction unit 400 is used to reconstruct the sate...
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