A satellite communication uplink closed-loop timing synchronization method based on synchronization frame
A technology of timing synchronization and satellite communication, which is applied in the field of satellite communication to achieve the effect of high timing synchronization accuracy
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Embodiment 1
[0033] Step 1: Estimate the transmission delay range of the cell, divide synchronization frames on the basis of downlink transmission frames, and group them in units of N frames. The fixed position in each synchronization frame is filled with synchronization frame number n, n=1, 2, ..., N, the selection criterion of N: the duration of N synchronization frames is greater than the maximum round-trip transmission delay of terminals in the cell. The gateway station periodically sends a synchronization frame, and the sending time of the synchronization frame numbered 1 is recorded as T 0 ;
[0034] Step 2: Terminal 2 performs downlink synchronization, and in the case of a random access requirement, detects a synchronization signal frame numbered 1 to trigger an uplink random access signal transmission process.
[0035] Step 3: The transmission timing of the gateway station synchronous frame group is as follows Figure 5 As shown, at time T1, the gateway station receives an uplink...
Embodiment 2
[0049] Implementation example 2: Considering the satellite communication system deployed in our country covering Asia, the ground is in different locations, such as Beijing, Guangzhou, and Lhasa, and three gateway stations are deployed as the ground control nodes of the satellite. Assuming that 60 near-Earth polar satellites are launched, the orbital height is 1175km, and the satellite radial velocity is 6.1km / s to realize the satellite communication system covering Asia. The patent of the present invention will now be described by taking the Beijing gateway station G1 and the cell covered by the beam of the connected satellite S1 as an example. In this example, it includes: the gateway station G1 on the ground, the satellite S1 in space orbit, and the terminal 1 and terminal 2 within the coverage of the satellite beam as examples to illustrate the patent of the invention:
[0050] Step 1: The gateway station establishes a connection with the satellite: 1, and the satellite S1...
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