Tomographic loss factor estimation

• US 10,274,602 B2
• Filed: 07/14/2015
• Issued: 04/30/2019
• Est. Priority Date: 07/14/2014
• Status: Active Grant

• Current Assignee: Iposi, Inc.
• Original Assignee: Iposi, Inc.
• Inventors: Lee, Richard M., Kurby, Christopher Neil, Derbez, Eric
• Primary Examiner(s): Nguyen, Chuong P
• Application Number:
  US14/798,611
• Publication Number:
  US 20180074204A1
• Time in Patent Office: 1,386 Days
• Field of Search: 34235759, 34235761
• CPC Class Codes: G01S 19/21 Interference related issues ; Issues related to cross-correlation, spoofing or other methods of denial of service
• CPC Class Codes: G01S 19/22 Multipath-related issues
• CPC Class Codes: G01S 19/42 Determining position
• CPC Class Codes: H04B 1/7113 Determination of path profile
• CPC Class Codes: H04B 17/104 of other parameters, e.g. DC offset, delay or propagation times
• CPC Class Codes: H04B 17/23 Indication means, e.g. displays, alarms, audible means
• CPC Class Codes: H04B 17/26 using historical data, averaging values or statistics
• CPC Class Codes: H04B 17/27 for locating or positioning the transmitter
• CPC Class Codes: H04B 17/318 Received signal strength
• CPC Class Codes: H04B 17/382 for resource allocation, admission control or handover
• CPC Class Codes: H04B 17/391 Modelling the propagation channel
• CPC Class Codes: H04B 2001/70724 featuring pilot assisted reception
• CPC Class Codes: H04B 2201/709718 Determine interference

Abstract

Determination of a signal loss profile relative to a receiver based on measured signal power of a sounding signal from a sounding transmitter having a known signal power in free space relative to the receiver. The signal loss profile may include a plurality of signal loss values corresponding to a plurality of received sounding signals at the receiver. In an embodiment, the sounding signal may comprise a GNSS navigational signal (e.g., a GPS signal). The signal loss profile may be used to extrapolate signal loss for a transmitter collocated with the receiver. In turn, the signal loss profile may be used in conjunction with a shared spectrum system to model a signal propagation from the collocated transmitter when determining allocation of a shared spectrum resource of the shared spectrum system.

Claims

1. A method for determining a signal power loss relative to a receiver, the method comprising:

obtaining measured received power levels for each of a plurality of sounding signals from one or more sounding transmitters as measured at a stationary receiver located within a structure, wherein the one or more sounding transmitter is at a known location relative to the receiver upon transmission of a sounding signal and the plurality of sounding signals pass through at least a portion of the structure;

determining a direction of incidence relative to the receiver based at least in part on the known location of the sounding transmitter relative to the receiver for each of the plurality of sounding signals received at the receiver;

calculating a signal loss value for each of the plurality of sounding signals based at least in part on the measured receiver power level of each of the plurality of sounding signals and a corresponding known signal power level relative to the receiver in free space;

generating a signal loss profile for the receiver based at least on the signal loss values and the corresponding direction of incidence of each of the plurality of sounding signals relative to the receiver; and

extrapolating the signal loss values calculated for the plurality of sounding signals broadcast at a sounding frequency to determine a projected signal loss for a transmission frequency of a transmitter collocated with the receiver based on known loss relationships between the sounding frequency and the transmission frequency, wherein the transmitter utilizes a transmission frequency different than the sounding frequency of the plurality of sounding signals.

2. The method of claim 1, wherein at least two of the plurality of sounding signals have a different direction of incidence relative to the receiver.

3. The method of claim 1, wherein the signal loss profile includes at least a two dimensional representation of signal loss values at corresponding directions of incidence relative to the receiver.

4. The method of claim 1, wherein the signal loss profile comprises a plurality of pixels having an area defined relative to the receiver, wherein each pixel has an associated statistical signal loss value corresponding to the signal loss values that are associated with the direction of incidences within the pixel.

5. The method of claim 4, wherein the statistical signal loss value for a given pixel comprises a statistically derived measure based on at least one sounding signal received at a direction of incidence within the pixel.

6. The method of claim 5, wherein the statistically derived measure comprises a mean signal loss value of each signal loss values with a direction of incidence within the pixel.

7. The method of claim 6, wherein the statistically derived measure comprises a standard deviation for the plurality of signal loss values derived with directions of incidence within the pixel.

8. The method of claim 4, wherein each pixel is defined by a range of azimuth angles and a range of elevation angles relative to the receiver, wherein each pixel comprises a range of azimuth angles of at least about 0.5 degrees and not greater than about 20 degrees and a range of elevation angles of at least about 0.5 degrees and not greater than about 20 degrees.

9. The method of claim 1, wherein the signal loss value comprises a carrier to thermal noise power ratio.

10. The method of claim 1, wherein the sounding transmitter comprises a GNSS space vehicle and the sounding signal comprises a navigational signal broadcast by the GNSS space vehicle, wherein the navigational signals include ephemeris data regarding the GNSS space vehicle and the known location of the sounding transmitter relative to the receiver is determined based on the ephemeris data.

11. The method of claim 10, further comprising locating the receiver using the navigational signal.

12. The method of claim 1, wherein the direction of incidence comprises an elevation angle and an azimuth angle defining a direction extending between the sounding transmitter and the receiver.

13. The method of claim 1, further comprising:

determining if the sounding signal is a direct wave from the sounding transmitter or a multipath wave from the sounding transmitter at least in part based on an analysis of the sounding signal characteristics at the receiver.

14. The method of claim 1, wherein the sounding signals are received at the receiver using a time spread approach to signal acquisition to acquire a plurality of sounding signals over a defined period, wherein the defined period comprises a plurality of coherent or non-coherent integration intervals.

15. The method claim 14, wherein the defined period is at least greater than one hour.

16. The method of claim 1, wherein the sounding frequency of the sounding signals is less than the transmission frequency of the transmission frequency of the collocated transmitter.

17. The method of claim 16, wherein the signal loss value calculated for the sounding signal is equated to the projected signal loss for the transmission frequency of the transmitter.

18. The method of claim 1, further comprising:

sending the signal loss value and the associated direction of incidence to a shared spectrum controller.

19. The method of claim 18, further comprising:

receiving, from the shared spectrum controller, an assignment of one or more transmission parameters for use in connection with a transmitter collocated with the receiver in a shared spectrum regime is wherein the assignment at least in part based on the signal loss value and the associated direction of incidence.

20. The method of claim 1, wherein the plurality of sounding transmitters comprise at least a first sounding transmitter corresponding to a first satellite vehicle type and at least a second sounding transmitter corresponding to a second satellite vehicle type, wherein signal reception coverage of the first sounding transmitter is different than the signal reception coverage of the second sounding transmitter relative to the receiver.

21. The method of claim 20, wherein the first satellite vehicle type is a navigational satellite and the second satellite vehicle type is a communications satellite.

22. A system for determining a signal power loss relative to a receiver disposed within a structure, the system comprising:

a stationary receiver disposed within a structure that is operable to receive a plurality of sounding signals at a measured received power level, each of the plurality of sounding signals having a direction of incidence relative to the receiver from one or more sounding transmitter at a known location relative to the receiver, wherein the sounding signal passes through at least a portion of the structure, and wherein the direction of incidence is determined at least in part on the known location of the sounding transmitter relative to the receiver upon transmission of a sounding signal;

a loss determination module, executed by a processor in operative communication with the receiver, that is operative to;

calculate a signal loss value for each of the plurality of sounding signals based on the measured received power level and a known signal power level of the sounding signal relative to the receiver in free space,

generate a signal loss profile for the receiver based at least in part on the signal loss value and the corresponding direction of incidence of each of the plurality of sounding signals relative to the receiver, and

extrapolate the signal loss value calculated for each of the sounding signals at a sounding frequency to determine a projected signal loss for a transmission frequency of a transmitter collocated with the receiver based on known loss relationships between the sounding frequency and the transmission frequency.

23. The system of claim 22, wherein at least two of the plurality of sounding signals have a different direction of incidence relative to the receiver.

24. The system of claim 22, wherein the signal loss profile includes at least a two dimensional representation of signal loss values at corresponding directions of incidence relative to the receiver.

25. The system of claim 22, wherein the signal loss profile comprises a plurality of pixels having an area defined relative to the receiver, wherein each pixel has an associated statistical signal loss value corresponding to the signal loss values that are associated with the direction of incidences within the pixel.

26. The system of claim 25, wherein the statistical signal loss value for a given pixel comprises a statistically derived measure based on at least one sounding signal received at a direction of incidence within the pixel.

27. The system of claim 25, wherein each pixel is defined by a range of azimuth angles and a range of elevation angles relative to the receiver, wherein each pixel comprises a range of azimuth angles of at least about 0.5 degrees and not greater than about 20 degrees and a range of elevation angles of at least about 0.5 degrees and not greater than about 20 degrees.

28. The system of claim 22, wherein the signal loss value comprises a carrier to thermal noise power ratio.

29. The system of claim 22, wherein the sounding transmitter comprises a GNSS space vehicle and the sounding signal comprises a navigational signal broadcast by the GNSS space vehicle, wherein the navigational signals include ephemeris data regarding the GNSS space vehicle and the known location of the sounding transmitter relative to the receiver is determined based on the ephemeris data.

30. The system of claim 29, wherein the loss determination module is operative to locate the receiver using the navigational signal.

31. The system of claim 22, wherein the sounding frequency of the sounding signal is less than the transmission frequency of the transmission frequency of the collocated transmitter.

32. The system of claim 31, wherein the signal loss value calculated for the sounding signal is equated to the projected signal loss for the transmission frequency of the transmitter.

33. The system of claim 22, wherein the loss determination module is operative to send the signal loss value and the associated direction of incidence to a shared spectrum controller.

34. The system of claim 33, further comprising:

a transmitter collocated with the receiver that receives, from the shared spectrum controller, an assignment of one or more transmission parameters for use in connection with the transmitter collocated with the receiver in a shared spectrum regime is wherein the assignment at least in part based on the signal loss value and the associated direction of incidence.