Binary diversity single-carrier transmission method based on self-adaptive cyclic prefix
A cyclic prefix and single-carrier technology, applied in the field of satellite communication systems, can solve the problems of increasing frame length, reducing system efficiency, processing complexity, transmission delay and synchronous improvement, etc., to reduce additional overhead, algorithm complexity is low, self-adaptive powerful effect
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Embodiment 1
[0037] The transmission distance difference that needs to be compensated in a certain period of time (greater than 30min) between two satellite sending nodes is 0.96Km, when the transmission rate is 100Mbps, the required cyclic prefix length is 320, based on the adaptive cyclic prefix algorithm of the present invention The steps are:
[0038] (1) The sender sets the initial cyclic prefix length to CP=450, the step size to N=128, the statistical interval to 1s, the statistical parameter to the bit error rate BER, and the threshold value to 10 -6 ;
[0039] (2) When the BER in the i-th statistical interval is less than or equal to the threshold value, the receiving end feeds back 0 to the sending end, and the sending end reduces the CP according to the specified step size;
[0040] (3) When the BER threshold is within the i-th statistical interval, the receiving end feeds back 1 to the sending end, and the sending end increases the CP according to the specified step size;
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Embodiment 2
[0046] Figure 5 An embodiment of the present invention is given, including two satellite sending nodes and one satellite ground receiving station located at 60 degrees north latitude, and the parameters of each satellite are shown in Table 2.
[0047] Table 2
[0048] parameters
satellite 2
Semi-major axis (Km)
42164.2
42164.2
Eccentricity
0
0
Inclination (degrees)
2
5
ascending node right ascension (degrees)
100
100.1
Argument of perigee (degrees)
0
0
True anomaly (degrees)
0
90
Longitude Drift Rate
0
0
[0049] Figure 6 The mathematical model of the distance between the satellite ground receiving station and the satellite is given when a single satellite has an inclination angle, where O represents the center of the earth, U represents the user, and A, B, and C represent the satellites located above the equator and offset by an angle...
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