Continuous carrier optical phase optometric measurement over coherent optical communication link

Patent metadata

Field	Value
Publication number	US-10148352-B1
Application number	US-201715646687-A
Country	US
Kind code	B1
Filing date	Jul 11, 2017
Priority date	Jul 11, 2017
Publication date	Dec 4, 2018
Grant date	Dec 4, 2018

Abstract

An apparatus for measuring a distance between a first and second terminal includes a frame counter for determining a number of data frames traversing a distance between the first terminal 105 and the second terminal, a frame bit counter for determining a number of data clock bits offset between a transmitted data frame and a concurrently received data frame, a data clock phase detector for determining a phase difference between an RF data clock for the transmitted data frame and an RF data clock for the concurrently received data frame, and an optical carrier phase detector for determining a phase difference between an optical carrier used to transmit the transmitted data frame and an optical carrier for the concurrently received data frame. The distance between the first and second terminal is determined from a round trip transit time T between the first and second terminals.

First claim

The invention claimed is:

1. An apparatus for measuring a distance between a first and second terminal comprising:
a frame counter for determining a number of data frames traversing a distance between the first terminal 105 and the second terminal;
a frame bit counter for determining a number of data clock bits offset between a transmitted data frame and a concurrently received data frame;
a data clock phase detector for determining a phase difference between an RF data clock for the transmitted data frame and an RF data clock for the concurrently received data frame; and
an optical carrier phase detector for determining a phase difference between an optical carrier used to transmit the transmitted data frame and an optical carrier for the concurrently received data frame,
wherein the distance between the first and second terminal is determined from a round trip transit time T between the first and second terminals expressed as:
T=N frame ×T frame +N bit ×T bit +ΔData Clock Phase+ΔCarrier Phase,

where N frame is the number of frames traversing the distance between the first terminal 105 and the second terminal 110 , T frame is the frame period, N bit is the number of RF data clock bits offset between the presently transmitted frame and the presently received data frame, T bit is the period of the RF data clock, Δ Data Clock Phase is the phase difference between the transmitted RF data clock and the received data clock, and Δ Carrier Phase is the phase difference between the transmitted optical carrier and the received optical carrier.

2. The apparatus of claim 1 , comprising an RF frequency synthesizer for generating the RF data clock.

3. The apparatus of claim 1 , comprising a pattern generator for generating data for the data frames.

4. The apparatus of claim 1 , comprising a source of communication data for generating data for the data frames.

5. The apparatus of claim 1 , comprising an optical frequency synthesizer for generating the optical carrier.

6. The apparatus of claim 1 , wherein the optical carrier is a coherent optical communications carrier.

7. The apparatus of claim 1 , wherein the first terminal is a ground terminal and the second terminal is a space terminal.

8. The apparatus of claim 1 , wherein the first and second terminals are located on different space craft.

9. The apparatus of claim 1 , wherein the first and second terminals are located on different terrestrial bodies.

10. A method for measuring a distance between a first and second terminal comprising:
determining a number of data frames traversing a distance between the first terminal 105 and the second terminal;
determining a number of data clock bits offset between a transmitted data frame and a concurrently received data frame;
determining a phase difference between an RF data clock for the transmitted data frame and an RF data clock for the concurrently received data frame;
determining a phase difference between an optical carrier used to transmit the transmitted data frame and an optical carrier for the concurrently received data frame; and
calculating the distance between the first and second terminal from a round trip transit time T between the first and second terminals expressed as:
T=N frame ×T frame +N bit ×T bit +ΔData Clock Phase+ΔCarrier Phase,

where N frame is the number of frames traversing the distance between the first terminal 105 and the second terminal 110 , T frame is the frame period, N bit is the number of RF data clock bits offset between the presently transmitted frame and the presently received data frame, T bit is the period of the RF data clock, Δ Data Clock Phase is the phase difference between the transmitted RF data clock and the received data clock, and Δ Carrier Phase is the phase difference between the transmitted optical carrier and the received optical carrier.

11. The method of claim 10 , comprising generating the RF data clock using an RF frequency synthesizer.

12. The method of claim 10 , comprising generating data for the data frames using a pattern generator.

13. The method of claim 10 , comprising generating data for the data frames using a source of communication data.

14. The method of claim 10 , comprising generating the optical carrier using an optical frequency synthesizer.

15. The method of claim 10 , wherein the optical carrier is a coherent optical communications carrier.

16. The method of claim 10 , comprising locating the first terminal terrestrially and locating the second terminal in space.

17. The method of claim 10 , comprising locating the first and second terminals on different space craft.

18. The method of claim 10 , comprising locating the first and second terminals on different terrestrial bodies.

Assignees

• Nasa

Inventors

• Yang Guangning
• Chen Jeffrey R

Classifications

• G08B13/08

  by opening, e.g. of door, of window, of drawer, of shutter, of curtain, of blind · CPC title

• G01S17/933

  of aircraft or spacecraft · CPC title

• B64G1/24

  Guiding or controlling apparatus, e.g. for attitude control · CPC title

• H04B10/079 Primary

  using measurements of the data signal · CPC title

• B64G3/00

  Observing or tracking cosmonautic vehicles · CPC title