Pulse radar and components therefor

• US 5,083,130 A
• Filed: 03/08/1991
• Issued: 01/21/1992
• Est. Priority Date: 10/31/1983
• Status: Expired due to Fees

• Current Assignee: Apostle G. Cardiasmenos
• Original Assignee: Apostle G. Cardiasmenos
• Inventors: Cardiasmenos, Apostle G.
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US07/666,826
• Time in Patent Office: 319 Days
• Field of Search: 342/52, 342/54, 342/175, 342/188, 343/721, 343/756, 343/909
• US Class Current: 342/188
• CPC Class Codes: G01S 13/282 using a frequency modulated carrier wave G01S13/286 takes precedence
• CPC Class Codes: G01S 7/02 of systems according to group G01S13/00
• CPC Class Codes: G01S 7/024 using polarisation effects in waveguides H01P1/165; for aerials H01Q, e.g. H01Q15/22, H01Q15/24, H01Q19/195
• CPC Class Codes: G01S 7/026 involving the transmission of elliptically or circularly polarised waves
• CPC Class Codes: G01S 7/034 Duplexers switching devices for waveguides H01P1/10; transmit-receive switching in transceivers H04B1/44
• CPC Class Codes: G01S 7/285 Receivers
• CPC Class Codes: H01P 1/161 sustaining two independent orthogonal modes, e.g. orthomode transducer combining or separating polarisations and frequencies H01P1/2131
• CPC Class Codes: H01P 1/2131 with combining or separating polarisations
• CPC Class Codes: H01Q 15/12 functioning also as polarisation filter polarisation converters H01Q15/242
• CPC Class Codes: H01Q 19/195 wherein a reflecting surface acts also as a polarisation filter or a polarising device
• CPC Class Codes: H01Q 21/245 provided with means for varying the polarisation polarising devices H01Q15/24; tracking by comparing linear polarisation compounds G01S3/146; reducing depolarisation effects H04B7/00; polarisation diversity H04B7/10
• CPC Class Codes: H01Q 3/16 for varying relative position of primary active element and a reflecting device
• CPC Class Codes: H01Q 3/20 wherein the primary active element is fixed and the reflecting device is movable
• CPC Class Codes: H01Q 3/26 varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture H01Q3/12, H01Q3/22, H01Q3/24 take precedence
• CPC Class Codes: H03D 9/0633 mounted on a stripline circuit

Abstract

A pulse radar for operation at 94 GHz and higher frequencies is shown to include an antenna, a diplexer and first detector that are each optically fed so that radio frequency signals may be, when transmitting, passed through the diplexer to the antenna and, when receiving, from the antenna through the diplexer to the first detector.

Claims

1. An apparatus comprising:

(a) means, responsive to a first beam of radio frequency (RF) energy having an electric field and a first path of propagation and responsive to a second beam of RF energy having an electric field orthogonal to the electric field of the first beam of RF energy and a second path of propagation, for passing the first beam of RF energy through said means and for reflecting the second beam of RF energy from said means; and

(b) means, disposed in the path of the first and the second beams of RF energy, for rotating the electric field of the beam of RF energy in a direction and for rotating the electric field of the second beam of RF energy in the same direction.

2. The apparatus as recited in claim 1 wherein the rotating means rotates the electric fields of the first and the second beams of RF energy 45 degrees.

3. The apparatus as recited in claim 2 further comprising second means, disposed in the path of propagation of the first and the second beams of RF energy, for reflecting the path of the first and the second beam of RF energy and for passing a third beam of RF energy through said second means.

4. The apparatus as recited in claim 3 further comprising means, disposed in the path of propagation of the first, the second and the third beams of RF energy, for changing the second and the third beams of RF energy from circular polarization to linear polarization and for changing the first beam of RF energy from linear polarization to circular polarization.

5. The apparatus as recited in claim 4 further comprising a plurality of lens disposed in the path of the first beam of RF energy.

6. An apparatus comprising:

(a) a first polarization grid, the first polarization grid being inclined at an angle of 45°

to an axis of a beam of radio frequency (RF) energy having the axis and a direction of polarization, the first polarization grid having parallel conductors disposed orthogonally to the direction of polarization of the beam; and

(b) a Faraday rotator disposed in the path of the beam of RF energy, the Faraday rotator adapted to rotate the polarization of the beam by 45°

to produce a rotated beam of RF energy.

7. The apparatus as recited in claim 6 further comprising a second polarization grid in the path of the rotated beam of RF energy, the second polarization grid being inclined at an angle of 45°

to the axis of the rotated beam and having parallel conductive strips disposed in parallel with the direction of polarization of the rotated beam of RF energy to reflect the rotated beam.

8. The apparatus as recited in claim 7 further comprising a quarter wave plate disposed in the path of the reflected rotated beam of RF energy to change the polarization of the reflected rotated beam to circularly polarized.

9. The apparatus as recited in claim 8 further comprising a plurality of lens disposed in the path of the beam of RF energy.

10. A radar seeker for a missile comprising:

(a) means, responsive to a first beam of radio frequency (RF) energy having an electric field and a first path of propagation and responsive to a second beam of RF energy having an electric field orthogonal to the electric field of the first beam of RF energy and a second path of propagation, for passing the first beam of RF energy through said means and for reflecting the second beam of RF energy; and

(b) means, disposed in the path of the first and the second beam of RF energy, for rotating the electric field of the first beam in a direction by 45° and

for rotating the electric field of the second beam of RF energy in a similar direction by 45°

.

11. The radar seeker as recited in claim 10 further comprising second means, disposed in the path of propagation of the first and the second beams of RF energy for reflecting the path of the first and the second beam of RF energy and for passing a third beam of RF energy through said second means.

12. The radar seeker as recited in claim 11 further comprising means, disposed in the path of propagation of the first, the second and the third beams of RF energy, for changing the second and the third beams of RF energy from circular polarization to linear polarization and for changing the first beam of RF energy from linear polarization to circular polarization.

13. The radar seeker as recited in claim 12 further comprising a plurality of lens disposed in the path of the first beam of RF energy.

15. The radar as recited in claim 13 wherein the diplexer means comprises:

(a) means, responsive to the first beam of linearly polarized RF energy having an electric field and a first path of propagation, for passing the first beam of linearly polarized RF energy through said means and responsive to a second beam of linearly polarized RF energy having an electric field orthogonal to the electric field of the first beam of linearly polarized RF energy and a second path of propagation, for reflecting the path of propagation of the second beam of linearly polarized RF energy; and

(b) means, disposed in the path of the first and the second beams of linearly polarized RF energy by 45°

.

14. A radar comprising

(a) means for providing a first beam of linearly polarized radio frequency (RF energy;

(b) diplexer means having a first, a second, a third and a fourth port, such diplexer means being responsive to the first beam incident on the first port, for converting the first beam to an initially convergent beam of circularly polarized RF energy out of the second port and, also being responsive to a second divergent beam of circularly polarized RF energy reflected from targets and incident on the second port, for converting in accordance with the direction of polarization of the RF energy in the second divergent beam, said energy to a second and a third beam of linearly polarized RF energy out of a respective one of the third and fourth ports; and

(c) antenna means, responsive to the initially convergent beam of circularly polarized RF energy out of the second port and to RF energy reflected from targets, for collimating and directing the initially convergent beam of circularly polarized RF energy out of the second port and for providing the second divergent beam of circularly polarized RF energy.

16. The radar as recited in claim 14 wherein the diplexer means comprises second means, disposed in the path of propagation of the first and the second beams of linearly polarized RF energy for reflecting the path of the first and the second beams of linearly polarized RF energy and for passing the third beam of linearly polarized energy through said second means.

17. The radar as recited in claim 16 further comprising means, disposed in the path of propagation of the first, the second and the third beams of linearly polarized RF energy, for changing the second and the third beams of RF energy from circular polarization to linearly polarization and for changing the first beam of linearly polarized RF energy from linear polarization to circular polarization.

18. The radar as recited in claim 16 further comprising a plurality of lens disposed in the path of the first beam of linearly polarized RF energy.

19. A method of operating a millimeter-wave seeker comprising the step of:

optically coupling a first radio frequency signal from a transmitter to a focal plane of an antenna and a second radio frequency signal from the focal plane of the antenna to a radio frequency mixer array

wherein the optically coupling step comprises the steps of;

(a) rotating an electric field of the first radio frequency signal by 45°

degrees;

(b) rotating an electric field of the second radio frequency signal by 45 degrees; and

(c) reflecting the second radio frequency signal toward the radio frequency mixer.

20. The method as recited in claim 19 further comprising the step of reflecting the first radio frequency signal toward the focal plane of the antenna and the second radio frequency signal from the focal plane of the antenna.