Method and system for determining water vapor profile using GPS signals

• US 7,739,048 B2
• Filed: 06/18/2007
• Issued: 06/15/2010
• Est. Priority Date: 06/18/2007
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Tillotson, Brian J., Ross, Tamaira E.
• Primary Examiner(s): Feliciano; Eliseo Ramos
• Assistant Examiner(s): HENSON, MISCHITA L
• Application Number:
  US11/764,465
• Publication Number:
  US 20080312836A1
• Time in Patent Office: 1,093 Days
• Field of Search: 702 2- 5, 702/32, 702/72, 702/92, 702 94- 95, 702/99, 702/130, 702/150, 702154-155, 702/159, 701213-216
• US Class Current: 702/3
• CPC Class Codes: G01K 11/00 Measuring temperature based upon physical or chemical changes not covered by groups G01K3/00, G01K5/00, G01K7/00 or G01K9/00
• CPC Class Codes: G01S 19/14 specially adapted for specific applications
• CPC Class Codes: G01W 1/04 giving only separate indications of the variables measured

Abstract

A system and method for obtaining weather related information for a portion of the Earth'"'"'s atmosphere between a predetermined surface portion of the Earth and an airborne object located over the predetermined surface portion, and operating at a known altitude, using position locating signals from a space vehicle. In one exemplary implementation the space vehicle transmits a first position locating signal. The first position locating signal is received by the airborne object directly from the space vehicle. A second position locating signal from the space vehicle is received by the airborne object after being reflected from the predetermined surface portion at a known angle. Phase information from the first and second position locating signals is used to determine a refractivity of the atmosphere between the predetermined surface portion and the airborne object. The refractivity is used to determine weather related information for the atmosphere.

Claims

1. A method for obtaining weather related information for a portion of the Earth'"'"'s atmosphere between a predetermined surface portion of the Earth and a moving airborne object located over the predetermined surface portion, using a position locating signal from a space vehicle, the method comprising:

receiving a first position locating signal at the moving airborne object while at a known, predetermined elevation above said predetermined surface portion of the Earth, said first position locating signal being received by the moving airborne object directly from said space vehicle;

receiving a second position locating signal at the moving airborne object while at said known, predetermined elevation, said second position locating signal being reflected from said predetermined surface portion at a known angle before being received by the moving airborne object;

using phase information pertaining to a phase of each of said first and second position locating signals to determine a refractivity of said atmosphere between said predetermined surface portion and said moving airborne object; and

using said refractivity to determine weather related information for said atmosphere.

2. The method of claim 1, wherein using said refractivity to determine weather related information comprises using said refractivity to determine temperature information.

3. The method of claim 1, wherein using said refractivity to determine weather related information comprises using said refractivity to determine precipitable water vapor (PWV) in said atmosphere.

4. The method of claim 1, wherein receiving said first position locating signal and receiving said second position locating signal comprises receiving said position locating signals at an aircraft operating at said predetermined altitude above said surface of the Earth.

5. The method of claim 4, wherein receiving said position locating signals at an aircraft comprises:

receiving said first position locating signal at a first antenna of said aircraft that is located adjacent a crown of a fuselage of said aircraft; and

receiving said second position locating signal at a second antenna of said aircraft that is located adjacent an underbody portion of said fuselage of said aircraft.

6. The method of claim 1, wherein using said phase information comprises:

determining a phase of said received first position locating signal;

determining a phase of said received second position locating signal;

determining an absolute phase difference between said first and second position locating signals; and

using said phase difference to determine said refractivity.

7. The method of claim 1, wherein using said phase information comprises:

using said phase information to determine a Doppler shift between said first and second position locating signals; and

using said Doppler shift to determine said refractivity.

8. The method of claim 1, wherein receiving said second position locating signal after said second position locating signal has been reflected from the surface of the Earth comprises receiving said second position locating signal after said second position locating signal has been reflected from a body of water.

9. The method of claim 8, further comprising considering waves existing in the body of water in determining a phase of said second position locating signal, and using said phase of said second position locating signal to assist in determining said refractivity.

10. The method of claim 8, further comprising receiving an additional position locating signal at the moving airborne object while the airborne object is at a known, predetermined elevation above the body of water and

said additional positional locating signal being reflected from said body of water at a different angle than said second position locating signal, and using said first and second position locating signals and said additional position locating signal to account for changes in a level of said body of water.

11. A method for determining a refractivity of a portion of the Earth'"'"'s atmosphere above a body of water using signals from a Global Positioning System (GPS) space vehicle, the method comprising:

receiving a first GPS signal at an airborne mobile platform that is operating at a known, predetermined altitude above the body of water, said first GPS signal being received directly from said GPS system;

receiving a second GPS signal at said airborne mobile platform after second portion of said GPS signal is reflected from said body of water at a known angle;

using phase information pertaining to said first and second GPS signals to determine a difference in phase between said received first and second GPS signals;

using said phase difference to determine a refractivity of said atmosphere between said body of water and said airborne mobile platform; and

using said refractivity to determine at least one of precipitable water vapor (PWV) and temperature of said atmosphere between said body of water and said airborne mobile platform.

12. The method of claim 11, wherein using said phase difference comprises:

using said phase difference to determine a Doppler shift between said first and second GPS signals; and

using said Doppler shift to determine said refractivity.

13. The method of claim 11, further comprising considering an effect of waves existing in said body of water when determining said phase difference.

14. The method of claim 11, further comprising using additional position locating signals from a different space vehicle, or from the same space vehicle when it has moved to a different elevation angle,

receiving a first one of the additional position locating signals at the moving airborne object while at a known, predetermined elevation above a second predetermined surface portion of the Earth, said first one of the additional position locating signals being received by the moving airborne object directly from said space vehicle;

receiving a second one of the additional position locating signals at the moving airborne object while at said known, predetermined elevation, said second one of the additional position locating signals being reflected from said second predetermined surface portion at a different angle than said second position locating signal, and using said second position locating signal and said second one of said additional position locating signal to account for changes in a level of said body of water.

15. The method of claim 11, wherein the operation of using phase information comprises considering an altitude of said mobile platform and an elevation of said GPS satellite relative to said mobile platform in determining distances that said first and second GPS signals travel to said mobile platform.

16. A system for determining weather related information using position locating signals from a space vehicle, the system comprising:

a moving airborne mobile platform having at least one antenna;

a receiver system in communication with said antenna, that receives;

a first position locating signal, while said mobile platform is operating at a known, predetermined elevation above a surface of the Earth, said first position locating signal being received directly from said space vehicle; and

a second position locating signal while operating at said known, predetermined elevation, said second position locating signal being reflected from said surface of the Earth at a known angle before being received by said receiver system;

a processor responsive to said position locating signals received by said antenna that determines phase information pertaining to said first and second position locating signals and uses said phase information to approximate a refractivity of a portion of the Earth'"'"'s atmosphere between said surface and said airborne mobile platform, said refractivity useable for determining weather related information for said portion of the Earth'"'"'s atmosphere between said surface and said airborne mobile platform.

17. The system of claim 16, wherein said weather related information comprises at least one of precipitable water vapor (PWV) and temperature.

18. The system of claim 16, wherein said processor uses said phase information to determine a phase difference between said first and second position locating signals.

19. The system claim 16, wherein said surface of the Earth comprises a body of water, and wherein said antenna receives said second position locating signal after said second position locating signal is reflected from said body of water.

20. The system of claim 16, wherein:

said antenna comprises first and second antennas;

said first antenna being located adjacent a crown of a fuselage of said airborne mobile platform and receiving only said first position locating signal; and

said second antenna being located on an undersurface of said fuselage of said airborne mobile platform and receiving only said second position locating signal.

21. The system of claim 16, wherein said processor uses an altitude of said airborne mobile platform and an elevation angle of said space vehicle, relative to said airborne mobile platform, to assist in computing said phase difference.