A method and device for determining information sending time
A technology for sending information and determining methods, which is applied in the field of communication, and can solve problems such as poor system reliability, inability to determine whether the current time has reached the synchronization cycle, lack of solutions, etc., and achieve the effect of improving system reliability
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Embodiment 1
[0190] Embodiment 1. Synchronization processing: when the UE can obtain the current time, the absolute reference time method is used to determine the synchronization subframe.
[0191] When the configuration processing is synchronous processing, the configuration period cfgPeriod is the synchronization period syncPeriod, and the configuration offset OffsetIndicator is the synchronization configuration offset syncOffsetIndicator.
[0192] It is assumed that the absolute start time T of the synchronization signal (ie, the preset information) set by the system is sent ref 685.374ms, T ref It is the configured or pre-configured reference time, that is, the absolute reference time. The synchronization period is 200ms, and the syncOffsetIndicator configured in the system information is 101.
[0193] Suppose the UE can obtain the current time T through GNSS or system information current is 1186.875ms, then substitute the above parameters according to the synchronization subframe c...
Embodiment 2
[0199] Embodiment 2: Synchronization processing: least common multiple time method, the UE can directly obtain the current time:
[0200] see Figure 4 , when the configuration processing is synchronous processing, the configuration period cfgPeriod is the synchronization period syncPeriod, and the configuration offset OffsetIndicator is the synchronization configuration offset syncOffsetIndicator. The system timing period sysPeriod is 10240ms.
[0201] Assume that the synchronization period syncPeriod is 200ms, and the syncOffsetIndicator obtained from the system information is 101.
[0202] Assumption 1: UE can obtain the current time T through GNSS or system information current 20701.5ms, the absolute start time T of the synchronization signal transmission set by the system ref is 0.5ms, the processing is as follows:
[0203] Step 1: VFN coefficient a=10240mod syncPeriod=40;
[0204] Step 2: The least common multiple of 10240 and syncPeriod Y=[10240, syncPeriod]=10240*...
Embodiment 3
[0225] Embodiment 3. Synchronization processing: least common multiple time method, the UE cannot obtain the current time:
[0226] When the configuration processing is synchronous processing, the configuration period cfgPeriod is the synchronization period syncPeriod, and the configuration offset OffsetIndicator is the synchronization configuration offset syncOffsetIndicator. The system timing period sysPeriod is 10240ms.
[0227] Assume that the synchronization period syncPeriod is 200ms, and the syncOffsetIndicator obtained from the system information is 101.
[0228] Assumption 1: Assume that the parameters are as follows:
[0229] The UE obtains a VFN of 2 from system information, or from other UE transmission information;
[0230] The UE obtains DFN 22 and DFN subframe 1 from system information, or other UE transmission information or from the local oscillator;
[0231] The calculation process is as follows:
[0232] Step 1: VFN coefficient a=10240mod syncPeriod=40; ...
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