Alignment and beam spreading for ground radial airborne radar

• US 5,442,364 A
• Filed: 07/22/1993
• Issued: 08/15/1995
• Est. Priority Date: 07/22/1993
• Status: Expired due to Fees

• Current Assignee: the united states of america as represented by the secretary of the navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Warejko, Stephen, Decker, Martin J., Lee, Henry E.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/094,957
• Time in Patent Office: 754 Days
• Field of Search: 342/372, 342/371, 342/157, 342/158, 342/140, 342/154, 342/25, 342/75, 342/76, 342/77, 342/81, 342/80, 342/191
• US Class Current: 342/372
• CPC Class Codes: G01S 13/42 Simultaneous measurement of distance and other co-ordinates indirect measurement G01S13/46
• CPC Class Codes: G01S 13/89 for mapping or imaging
• CPC Class Codes: G01S 7/2813 Means providing a modification of the radiation pattern for cancelling noise, clutter or interfering signals, e.g. side lobe suppression, side lobe blanking, null-steering arrays specially adapted to secondary radar systems G01S13/762; aerials or aerials systems H01Q21/29, H01Q25/00
• CPC Class Codes: H01Q 3/22 varying the orientation in accordance with variation of frequency of radiated wave

Abstract

A method and apparatus for controlling a radar beam emitted by a radar sym. The invention produces improved high resolution ground mapping by aligning the antenna isogain or isonull lines with the ground radial lines. The antenna axis is rolled by an angle determined from the geometric principles of the unit vectors along the ground radial lines. A new azimuth pointing angle is then computed and implemented. A new azimuth beamshape, azimuth beamwidth and azimuth beam spoiling factor are also computed and implemented.

Claims

1. A radar system comprising:

an antenna, said antenna producing a radar beam intersecting a ground plane to form an isogain line on said ground plane, said ground plane including a plurality of ground radial lines radiating from an origin point on said ground plane, said origin point being related to a navigational position of said radar system with respect to said ground plane, said isogain line having a corresponding ground radial line; and

beam steering means for controlling said antenna and for adjusting said radar beam to closely align said isogain line with said corresponding ground radial line to facilitate scan conversion to a television display format.

2. A radar system as in claim 1, wherein said antenna is an electronically scanned antenna.

3. A radar system as in claim 1, wherein said antenna is an electronically scanned phased array antenna.

4. A method of controlling an antenna of a radar system having both an azimuth axis and elevation axis wherein said antenna produces a radar beam intersecting a ground plane to form an isogain line on said ground plane, said ground plane including a plurality of ground radial lines radiating from an origin point on said ground plane, said origin point being related to a navigational position of said radar system with respect to said ground plane, said isogain line having a corresponding ground radial line, wherein said method comprises the step of steering said radar beam by rotating the antenna azimuth and elevation axes to closely align said isogain line with said corresponding ground radial line to facilitate scan conversion to a television display format.

5. The method as in claim 4, further comprising the step of electronically scanning said antenna.

6. The method as in claim 4, wherein said antenna is a phased array, further comprising the step of electronically scanning said antenna.

7. The method as in claim 4, wherein said antenna has an antenna axis, further comprising the step of performing roll stabilization by computing an antenna axis roll angle and rolling said antenna axis by said antenna axis roll angle.

8. The method as in claim 7 further comprising:

(a) computing an azimuth pointing angle for said radar beam;

(b) controlling said antenna to implement said azimuth pointing angle.

9. The method as in claim 8 further comprising:

(a) computing an azimuth beamshape for said radar beam;

(b) controlling said antenna to implement said azimuth beamshape.

10. The method as in claim 9 further comprising:

(a) computing an azimuth beamwidth for said radar beam;

(b) controlling said antenna to implement said azimuth beamwidth.

11. The method as in claim 10 further comprising:

(a) computing an azimuth spoiling factor for said radar beam; and

(b) controlling said antenna to implement said azimuth spoiling factor.

12. The method as in claim 7, wherein said antenna has an azimuth axis and an elevation axis, wherein for a ground radial line being mapped, said ground radial line having a corresponding near range unit vector point and a corresponding far range unit vector point in antenna space, said step of roll stabilization further comprising calculating said antenna axis roll angle by making a straight connecting line to connect said near range unit vector point and said far range unit vector point, said connecting line forming said antenna axis roll angel with said elevation axis.

13. The method as in claim 8 wherein said step of computing said azimuth pointing angle comprises setting said azimuth pointing angle to center azimuth coverage over said corresponding ground radial line.

14. The method as in claim 13, wherein said isogain line and its corresponding ground radial line has a maximum azimuth deviation in rolled antenna space, and wherein a near range unit vector corresponds to said corresponding ground radial line, said step of setting said azimuth pointing angle further comprises the steps of:

(a) transforming said near range unit vector into rolled antenna space to form a unit line-of-sight vector in the rolled antenna space, said unit line-of-sight vector in the rolled antenna space having an azimuth coordinate; and

(b) setting said azimuth pointing angle equal to said coordinate plus one-half of said maximum azimuth deviation.

15. The method as in claim 14 further comprising the step of using a doppler beam sharpening or synthetic aperture radar map mode for radar operation.

16. The method as in claim 9 wherein, after said step of roll stabilization, said antenna has a rolled antenna azimuth axis and a rolled antenna elevation axis, said step of computing said azimuth beamshape further comprises computing said azimuth beamshape as a function of the 3 dB beamwidth along said rolled antenna azimuth axis and the 3 dB beamwidth along said rolled antenna elevation axis.

17. The method as in claim 4, said isogain line and corresponding ground radial line having a maximum azimuth deviation, said antenna having an antenna axis, further comprising the steps of:

(a) selecting a line-by line doppler beam sharpening map processed mode for radar operation;

(b) selecting fan beams for the type of radar beam;

(c) performing roll stabilization by computing an antenna axis roll angle and rolling said antenna axis by said antenna axis roll angle, wherein after roll stabilization said atenna having a rolled antenna azimuth axis;

(d) setting an azimuth beamwidth equal to the 3 dB beamwidth along said rolled antenna azimuth axis plus said maximum azimuth deviation in rolled antenna space; and

(e) setting an azimuth spoiling factor equal to said azimuth beamwidth divided by the 3 dB beamwidth along said rolled antenna azimuth axis.

18. The method as in claim 4 further comprising the steps of:

(a) performing roll stabilization by computing an antenna axis roll angle and rolling said antenna azimuth and elevation axis by said antenna axis roll angle, said antenna having a rolled antenna azimuth axis after roll stabilization;

(b) selecting a synthetic aperture radar mapping mode for operation of said radar system, wherein said radar beam intersects said ground plane forming a map area having a total azimuth axis coverage and a total elevation axis coverage;

(c) computing an azimuth beamwidth as a function of said total azimuth axis coverage and said total elevation axis coverage;

(d) comparing the 3 dB beamwidth along said rolled antenna azimuth axis to said computed azimuth beamwidth;

(e) selecting pencil beam and setting said an azimuth beamwidth equal to the 3 dB beamwidth along said rolled antenna azimuth axis when the 3 dB beamwidth along said rolled antenna azimuth axis is greater than or equal to said computed azimuth beamwidth; and

(f) selecting a fan beam and setting an azimuth spoiling factor equal to said azimuth beamwidth divided by the 3 dB beamwidth along said rolled antenna azimuth axis when the 3 dB beamwidth along said rolled antenna azimuth axis is less than said computed azimuth beamwidth.

19. A radar system operating in monopulse ground mapping mode comprising:

an antenna, said antenna producing at least one radar beam, each such radar beam intersecting a ground plane to form an isonull line on said ground plane, said ground plane including a plurality of ground radial lines radiating from an origin point on said ground plane, said origin point being related to a navigational position of said radar system with respect to said ground plane, said isonull line having a corresponding ground radial line; and

beam steering means for controlling said antenna and for adjusting said radar beam to closely align said isonull line with said corresponding ground radial line to facilitate scan conversion to a television display format.

20. A radar system as in claim 19, wherein said antenna is an electronically scanned antenna.

21. A radar system as in claim 19, wherein said antenna is an electronically scanned phased array antenna.

22. A method of controlling an antenna of an radar system operating in monopulse ground mapping mode wherein said antenna produces at least one radar beam, each such radar beam having an azimuth and elevation beamshape, each such radar beam intersecting a ground plane to form an isonull line on said ground plane, said ground plane including a plurality of ground radial lines radiating from an origin point on said ground plane, said origin point being related to a navigational position of said radar system with respect to said ground plane, said isonull line having a corresponding ground radial line, wherein said method comprises the step of steering said radar beam to closely align said isonull line with said corresponding ground radial line to facilitate scan conversion to a television display format.

23. The method as in claim 22, further comprising the step of electronically scanning said antenna.

24. The method as in claim 22, wherein said antenna is a phased array, further comprising the step of electronically scanning said antenna.

25. The method as in claim 22, wherein said antenna includes an antenna axis, further comprising the step of performing roll stabilization by computing an antenna axis roll angle and rolling said antenna axis by said antenna axis roll angle.

26. The method as in claim 25 further comprising the steps of:

(a) computing an azimuth pointing angle for said radar beam; and

(b) controlling said antenna to implement said azimuth pointing angle.

27. The method as in claim 25, said antenna having an azimuth monopulse axis and an elevation monopulse axis, wherein for a ground radial line having a corresponding near range unit vector point and a corresponding far range unit vector point in antenna space, said step of performing roll stabilization further comprises computing said antenna axis roll angle by making a straight connecting line to connect said near range unit vector point and said far range unit vector point, said connecting line forming said antenna axis roll angle with said elevation monopulse axis.

28. The method as in claim 25, said antenna having an azimuth monopulse axis and an elevation monopulse axis, further comprising the steps of:

(a) selecting said azimuth monopulse axis for monopulse ground map processing and setting said antenna axis roll angle equal to zero when said computed antenna axis roll angle is equal to or between -π

/4 and π

/4;

(b) selecting said elevation monopulse axis for monopulse ground map processing and setting sad antenna axis roll angle equal to -π

/2 when the antenna axis roll angle is between -3π

/4 and -π

/4 or equal to -3π

/4;

(c) selecting said elevation monopulse axis for monopulse ground map processing and setting said antenna axis roll angle equal to π

/2 when the antenna axis roll angle is between π

/4 and 3π

/4 or equal to 3π

/4; and

(d) selecting said azimuth monopulse axis for monopulse ground map processing and setting said antenna axis roll angle equal to π

when the antenna axis roll angle is less than -3π

/4 or greater than 3π

/4.

29. The method as in claim 26, wherein said isonull line and corresponding ground radial line have a maximum azimuth deviation, and a near range unit vector corresponds to said ground radial line, said step of computing said azimuth pointing angle further comprises the steps of:

(a) transforming said near range unit vector into rolled antenna space to form a unit line-of-sight vector in the rolled antenna space, said unit line-of-sight vector in the rolled antenna space having an azimuth coordinate; and

(b) setting said azimuth pointing angle equal to said azimuth coordinate.

30. The method as in claim 26 wherein the azimuth beamshape is selected to be pencil beam.