A relative delay control method between high-precision satellite navigation signals
A satellite navigation signal and relative time delay technology, applied in the field of satellite navigation signal generation, can solve problems such as not meeting the synchronization requirements, and achieve the effect of improving positioning accuracy and convergence time
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[0080] The invention provides a method for controlling relative time delay between satellite navigation signals, comprising the following steps:
[0081] Let the two signal generation clock frequency be 122.76MHz (period is about T 1 =8.146ns) and 163.68MHz (the period is about T 2 =6.109ns), then its greatest common divisor frequency is 40.92MHz, then T y = M·T 1 = N·T 2 = 3·T 1 = 4·T 2 = 24.44ns.
[0082] calculate
[0083] [x(1), ind(1)]=min{abs[1T 1 -[0 1 2 … N]·T 2 ]}
[0084] [x(2), ind(2)]=min{abs[2T 1 -[0 1 2 … N]·T 2 ]}
[0085] ...
[0086] [x(M-1), ind(M-1)]=min{abs[(M-1)T 1 -[0 1 2 … N]·T 2 ]}
[0087] There are tables:
[0088]
[0089] The minimum absolute value of the first line is 2.037, and the minimum absolute value of the second line is -2.035, so the adjusted threshold of this step is 2.035 / 2=1.017ns, that is, the maximum precision is 1.017ns.
[0090] Generate two pseudo-random codes at these two clock frequencies, and use a third-part...
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