Secondary positioning reference signals for non-terrestrial networks in 5G new radio
Satellites in a non-terrestrial network may provide positioning reference signals (PRS) to user equipment (UE), with which the UE may determine its position using propagation delay difference measurements, such as Time Difference of Arrival (TDOA) measurement. Due to the large distances between satellites and the UE, the propagation delay differences in the PRS received from satellites may exceed half a radio frame, resulting in a frame level timing ambiguity in the differential measurements. The satellites transmit secondary PRS, along with primary PRS, that include timing information to resolve frame level timing ambiguity of the primary PRS. The positioning occasions in the secondary PRS, for example, may be aligned with corresponding positioning occasions primary PRS within each radio frame, and are transmitted with a periodicity that is an integer multiple (greater than 1) of that of the primary PRS to resolve the frame level timing ambiguity of the primary PRS.
1. A method for supporting positioning of a user equipment (UE) performed by the UE, comprising:
receiving primary positioning reference signals (PRS) from a plurality of satellites in a non-terrestrial network, wherein the primary PRS is transmitted periodically with one or more primary PRS positioning occasions per radio frame;
receiving secondary PRS from the plurality of satellites in the non-terrestrial network, wherein the secondary PRS is transmitted periodically with one or more secondary PRS positioning occasions per radio frame and provides timing information to resolve frame level timing ambiguity of the primary PRS; and
determining a Time Difference of Arrival (TDOA) measurement using the primary PRS received from a first satellite and a second satellite in the non-terrestrial network and the secondary PRS received from the first satellite and the second satellite, wherein the secondary PRS received from the first satellite and the second satellite resolve frame level timing ambiguity in the TDOA measurement caused by propagation delay difference between the first satellite and the UE and the second satellite and the UE exceeding half the radio frame.
2. The method of claim 1 , wherein each secondary PRS positioning occasion is aligned with a corresponding primary PRS positioning occasion within each radio frame.
3. The method of claim 1 , wherein a periodicity of the secondary PRS is an integer multiple of a periodicity of the primary PRS, wherein the integer multiple is greater than 1.
4. The method of claim 1 , wherein either a same number of secondary PRS positioning occasions are transmitted per radio frame as primary PRS positioning occasions, fewer secondary PRS positioning occasions are transmitted per radio frame than primary PRS positioning occasions, or more secondary PRS positioning occasions are transmitted per radio frame than primary PRS positioning occasions.
5. The method of claim 1 , wherein the timing information provided by the secondary PRS comprises information related to at least one of radio frame number or primary PRS burst index.
6. The method of claim 1 , further comprising receiving Radio Resource Control (RRC) configurations that provide parameters for the secondary PRS.
7. The method of claim 1 , wherein the primary PRS and the secondary PRS are multiplexed in time domain by transmitting the one or more primary PRS positioning occasions and the one or more secondary PRS positioning occasions in different symbols or are multiplexed in frequency domain by transmitting the one or more primary PRS positioning occasions and the one or more secondary PRS positioning occasions in a same symbol but with non-overlapping resource elements.
8. A user equipment (UE) configured to support positioning in a non-terrestrial network, comprising:
a wireless transceiver configured to wirelessly communicate with satellites in the non-terrestrial network;
at least one memory; and
at least one processor coupled to the wireless transceiver and the at least one memory, the at least one processor configured to:
receive primary positioning reference signals (PRS) from a plurality of satellites in the non-terrestrial network, via the wireless transceiver, wherein the primary PRS is transmitted periodically with one or more primary PRS positioning occasions per radio frame;
receive secondary PRS from the plurality of satellites in the non-terrestrial network, via the wireless transceiver, wherein the secondary PRS is transmitted periodically with one or more secondary PRS positioning occasions per radio frame and provides timing information to resolve frame level timing ambiguity of the primary PRS; and
determine a Time Difference of Arrival (TDOA) measurement using the primary PRS received from a first satellite and a second satellite in the non-terrestrial network and the secondary PRS received from the first satellite and the second satellite, wherein the secondary PRS received from the first satellite and the second satellite resolve frame level timing ambiguity in the TDOA measurement caused by propagation delay difference between the first satellite and the UE and the second satellite and the UE exceeding half the radio frame.
9. The UE of claim 8 , wherein each secondary PRS positioning occasion is aligned with a corresponding primary PRS positioning occasion within each radio frame.
10. CuThe UE of claim 8 , wherein a periodicity of the secondary PRS is an integer multiple of a periodicity of the primary PRS, wherein the integer multiple is greater than 1.
11. The UE of claim 8 , wherein either a same number of secondary PRS positioning occasions are transmitted per radio frame as primary PRS positioning occasions, fewer secondary PRS positioning occasions are transmitted per radio frame than primary PRS positioning occasions, or more secondary PRS positioning occasions are transmitted per radio frame than primary PRS positioning occasions.
12. The UE of claim 8 , wherein the timing information provided by the secondary PRS comprises information related to at least one of radio frame number or primary PRS burst index.
13. The UE of claim 8 , wherein the at least one processor is further configured to receive, via the wireless interface, Radio Resource Control (RRC) configurations that provide parameters for the secondary PRS.
14. The UE of claim 8 , wherein the primary PRS and the secondary PRS are multiplexed in time domain by transmitting the one or more primary PRS positioning occasions and the one or more secondary PRS positioning occasions in different symbols or are multiplexed in frequency domain by transmitting the one or more primary PRS positioning occasions and the one or more secondary PRS positioning occasions in a same symbol but with non-overlapping resource elements.
15. A method for supporting positioning of a user equipment (UE) performed by a satellite in a non-terrestrial network, comprising:
transmitting primary positioning reference signals (PRS), wherein the primary PRS is transmitted periodically with one or more primary PRS positioning occasions per radio frame; and
transmitting secondary PRS, wherein the secondary PRS is transmitted periodically with one or more secondary PRS positioning occasions per radio frame and provides timing information to resolve frame level timing ambiguity of the primary PRS;
wherein the secondary PRS resolves frame level timing ambiguity in Time Difference of Arrival (TDOA) measurements determined by the UE using the primary PRS and the secondary PRS from the satellite with primary PRS and secondary PRS from a second satellite that is caused by propagation delay difference between the satellite and the UE and between the second satellite and the UE exceeding half of the radio frame.
16. The method of claim 15 , wherein each secondary PRS positioning occasion is aligned with a corresponding primary PRS positioning occasion within each radio frame.
17. The method of claim 15 , wherein a periodicity of the secondary PRS is an integer multiple of a periodicity of the primary PRS, wherein the integer multiple is greater than 1.
18. The method of claim 15 , wherein either a same number of secondary PRS positioning occasions are transmitted per radio frame as primary PRS positioning occasions, fewer secondary PRS positioning occasions are transmitted per radio frame as primary PRS positioning occasions, or more secondary PRS positioning occasions are transmitted per radio frame as primary PRS positioning occasions.
19. The method of claim 15 , wherein the timing information provided by the secondary PRS comprises information related to at least one of a radio frame number or a primary PRS burst index.
20. The method of claim 15 , further comprising transmitting Radio Resource Control (RRC) configurations that provide parameters for the secondary PRS.
21. The method of claim 15 , wherein the primary PRS and the secondary PRS are multiplexed in time domain by transmitting the one or more primary PRS positioning occasions and the one or more secondary PRS positioning occasions in different symbols or are multiplexed in frequency domain by transmitting the one or more primary PRS positioning occasions and the one or more secondary PRS positioning occasions in a same symbol but with non-overlapping resource elements.
22. The method of claim 15 , wherein the primary PRS and the secondary PRS are quasi co-located.
23. A satellite in a non-terrestrial network configured to support positioning of a user equipment (UE), comprising:
a wireless transceiver configured to wirelessly communicate with the UE;
at least one memory; and
at least one processor coupled to the wireless transceiver and the at least one memory, the at least one processor configured to:
transmit primary positioning reference signals (PRS) via the wireless transceiver, wherein the primary PRS is transmitted periodically with one or more primary PRS positioning occasions per radio frame; and
transmit secondary PRS via the wireless transceiver, wherein the secondary PRS is transmitted periodically with one or more secondary PRS positioning occasions per radio frame and provides timing information to resolve frame level timing ambiguity of the primary PRS;
wherein the secondary PRS resolves frame level timing ambiguity in Time Difference of Arrival (TDOA) measurements determined by the UE using the primary PRS and the secondary PRS from the satellite with primary PRS and secondary PRS from a second satellite that is caused by propagation delay difference between the satellite and the UE and between the second satellite and the UE exceeding half of the radio frame.
24. The satellite of claim 23 , wherein each secondary PRS positioning occasion is aligned with a corresponding primary PRS positioning occasion within each radio frame.
25. The satellite of claim 23 , wherein a periodicity of the secondary PRS is an integer multiple of a periodicity of the primary PRS, wherein the integer multiple is greater than 1.
26. The satellite of claim 23 , wherein either a same number of secondary PRS positioning occasions are transmitted per radio frame as primary PRS positioning occasions, fewer secondary PRS positioning occasions are transmitted per radio frame as primary PRS positioning occasions, or more secondary PRS positioning occasions are transmitted per radio frame as primary PRS positioning occasions.
27. The satellite of claim 23 , wherein the timing information provided by the secondary PRS comprises information related to at least one of a radio frame number or a primary PRS burst index.
28. The satellite of claim 23 , the at least one processor is further configured to transmit Radio Resource Control (RRC) configurations that provide parameters for the secondary PRS.
29. The satellite of claim 23 , wherein the primary PRS and the secondary PRS are multiplexed in time domain by transmitting the one or more primary PRS positioning occasions and the one or more secondary PRS positioning occasions in different symbols or are multiplexed in frequency domain by transmitting the one or more primary PRS positioning occasions and the one or more secondary PRS positioning occasions in a same symbol but with non-overlapping resource elements.
30. The satellite of claim 23 , wherein the primary PRS and the secondary PRS are quasi co-located.