Satellite navigation text processing method and GPS receiver
A GPS receiver and message processing technology, applied in the field of navigation and communication, can solve the problems of long frame synchronization time, delay of the first positioning time of the GPS receiver, and speed up the speed of satellite ephemeris analysis, and achieve the effect of speeding up the speed.
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no. 1 example
[0049] see figure 1 , the first embodiment of a satellite message processing method in the embodiment of the present invention includes:
[0050] S1: Perform complete frame synchronization processing on the captured and tracked first satellite;
[0051] In this embodiment, when it is necessary to navigate the boot to determine the coordinate position, it is first necessary to perform complete frame synchronization processing on the captured and tracked first satellite. It should be noted that the aforementioned complete frame synchronization processing can be performed on the captured For the first satellite tracked, normal frame synchronization is completed by searching for 8-bit synchronization code and word check in the received navigation bits. The first satellite tracked refers to the satellite tracked by the receiver after it is powered on.
[0052] S2: Perform verification frame synchronization processing on the satellites captured and tracked in the follow-up;
[00...
no. 2 example
[0058] The above is a detailed description of the process of the navigation message processing method, and the following will describe in detail the process of the subsequent capture and tracking of the satellites for verification frame synchronization processing, please refer to figure 2 , the second embodiment of a satellite navigation message processing method in the embodiment of the present invention includes:
[0059] 201. Determine the startup mode of the receiver, if it is a cold startup, then execute step 202, if it is a warm startup, then execute step 203;
[0060] In this embodiment, when it is necessary to navigate the boot to determine the coordinate position, it is first necessary to determine the boot mode of the receiver. If it is a cold boot, go to step 202, and if it is a warm boot, go to step 203.
[0061] 202. Carry out satellite capture and tracking in sequence according to the PRN number;
[0062] When it is judged that the starting mode of the receiver...
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