Method and apparatus for calibrating an antenna array

• US 5,455,592 A
• Filed: 09/13/1994
• Issued: 10/03/1995
• Est. Priority Date: 09/13/1994
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated (Northrop Grumman Corporation)
• Inventors: Huddle, James R.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/305,271
• Time in Patent Office: 385 Days
• Field of Search: 342/359, 342/360, 342/173, 342/174
• US Class Current: 342/359
• CPC Class Codes: H01Q 3/267 Phased-array testing or checking devices

Abstract

The invention is a method and apparatus for determining the errors in the orientation coordinates of an antenna array and the spacings of the antennas in the array using radio waves from one or more sources having known positions and an inertial system, the antenna array comprising at least two antennas. The method comprises the steps of placing the antenna array in one or more specified orientations relative to a reference coordinate system, measuring the phase of each radio wave received by each of the antennas in the antenna array from the one or more radio-wave sources for each orientation of the antenna array, and then determining the errors in the array orientation coordinates using the measured phases. The method also includes determining the errors in the spacings of the antennas in the array and determining the errors in the orientation coordinates of the reference coordinate system, in both cases using the measured phases. The invention also includes apparatus for practicing the method utilizing an inertial system for maintaining the reference coordinate system.

Claims

1. A method for determining the errors in the orientation coordinates of an antenna array in a known location using radio waves from one or more sources having known positions, the antenna array comprising at least two antennas, the orientation of the antenna array being with respect to a reference coordinate system established by a reference unit, the method comprising the steps:

placing the antenna array in one or more specified orientations relative to a reference coordinate system;

measuring the phase of each radio wave received by each of the antennas in the antenna array from the one or more radio-wave sources for each orientation of the antenna array;

determining the errors in the array orientation coordinates using the measured phases.

2. The method of claim 1 further comprising the step:

determining the errors in the spacings of the antennas in the array using the measured phases.

3. The method of claim 1 further comprising the step:

determining the errors in the orientation coordinates of the reference coordinate system using the measured phases.

4. The method of claim 1 wherein there is a plurality of radio-wave sources and one orientation of the antenna array.

5. The method claim 1 wherein there is one radio-wave source and there is a plurality of orientations of the antenna array.

6. The method of claim 5 wherein the number of antennas in the array are two and the number of orientations of the antenna array is four, the coordinate axes of the antenna array coordinate system being denoted by the symbols x, y, and z, the two antennas being on the x-axis, the first orientation corresponding to the direction of arrival of the radio wave being along the y-axis, the second orientation being the first orientation rotated ninety degrees about the y-axis, the third orientation being the second orientation rotated ninety degrees about the x-axis, the fourth orientation being the third orientation rotated ninety degrees about the y-axis.

7. The method of claim 5 wherein the number of antennas in the array are two and the number of orientations of the antenna array is four, the coordinate axes of the antenna array coordinate system being denoted by the symbols x, y, and z, the two antennas being on the x-axis, the first orientation corresponding to the direction of arrival of the radio wave being along the x-axis, the second orientation being the first orientation rotated ninety degrees about the z-axis, the third orientation being the first orientation rotated ninety degrees about the y-axis, the fourth orientation being the second orientation rotated ninety degrees about the y-axis.

8. The method of claim 5 wherein the number of antennas in the array are two and the number of orientations of the antenna array is four, the coordinate axes of the antenna array coordinate system being denoted by the symbols x, y, and z, the two antennas being on the x-axis, the first orientation corresponding to the direction of arrival of the radio wave being along the y-axis, the second orientation being the first orientation rotated ninety degrees about the z-axis, the third orientation being the first orientation rotated ninety degrees about the y-axis, the fourth orientation being the second orientation rotated ninety degrees about the y-axis.

9. The method of claim 1 wherein the step of determining the errors in the array orientation coordinates is performed by determining the errors in the orientation coordinates of one or more pairs of antennas that comprise the antenna array.

10. The method of claim 2 wherein the step of determining the errors in the spacings of the antennas in the array is performed by determining the errors in the spacings of one or more pairs of antennas that comprise the antenna array.

11. An apparatus for determining the errors in the orientation coordinates of an antenna array using radio waves from one or more sources having known positions, the antenna array comprising at least two antennas, the apparatus comprising:

a reference unit;

an orientation unit on which the antenna array is mounted, the orientation unit assuming an orientation relative to the reference unit in accordance with an orientation input;

a phase measuring unit which measures the phase of each radio wave received by each of the antennas in the antenna array from the one or more radio-wave sources;

a computer which provides a sequence of one or more predetermined orientation inputs to the orientation unit and obtains the measured phases for each orientation of the orientation unit from the phase measuring unit, computer determining the errors in the array orientation coordinates using the measured phase.

12. The apparatus of claim 11 wherein the computer also determines the errors in the spacings of the antennas in the antenna array using the measured phases.

13. The apparatus of claim 11 wherein the computer also determines the errors in the orientation coordinates of the reference unit using the measured phases.

14. The apparatus of claim 11 wherein there are a plurality of radio-wave sources and the computer supplies one orientation input to the orientation unit.

15. The apparatus of claim 11 wherein there is one radio-wave source and the computer supplies a plurality of orientation inputs to the orientation unit.

16. The apparatus of claim 15 wherein the number of antennas in the array are two and the number of orientation inputs supplied by the computer to the orientation unit is four, the coordinate axes fixed with respect to the orientation unit being denoted by the symbols x, y, and z, the two antennas being on the x-axis, the first orientation of the orientation unit corresponding to the direction of arrival of the radio wave being along the y-axis, the second orientation being the first orientation rotated ninety degrees about the y-axis, the third orientation being the second orientation rotated ninety degrees about the x-axis, the fourth orientation being the third orientation rotated ninety degrees about, the y-axis.

17. The apparatus of claim 15 wherein the number of antennas in the array are two and the number of orientation inputs supplied by the computer to the orientation unit is four, the coordinate axes fixed with respect to the orientation unit being denoted by the symbols x, y, and z, the two antennas being on the x-axis, the first orientation of the orientation unit corresponding to the direction of arrival of the radio wave being along the x-axis, the second orientation being the first orientation rotated ninety degrees about the z-axis, the third orientation being the first orientation rotated ninety degrees about the y-axis, the fourth orientation being the second orientation rotated ninety degrees about the y-axis.

18. The apparatus of claim 15 wherein the number of antennas in the array are two and the number of orientation inputs supplied by the computer to the orientation unit is four, the coordinate axes fixed with respect to the orientation unit being denoted by the symbols x, y, and z, the two antennas being on the x-axis, the first orientation of the orientation unit corresponding to the direction of arrival of the radio wave being along the y-axis, the second orientation being the first orientation rotated ninety degrees about the z-axis, the third orientation being the first orientation rotated ninety degrees about the y-axis, the fourth orientation being the second orientation rotated ninety degrees about the y-axis.

19. The apparatus of claim 11 wherein the computer determines the errors in the array orientation coordinates by determining the errors in the orientation coordinates of one or more pairs of antennas that comprise the antenna array.

20. The apparatus of claim 12 wherein the computer determines the errors in the spacings of the antennas in the antenna array by determining the errors in the spacings of one or more pairs of antennas that comprise the antenna array.