Antenna stabilization and enhancement by rotation of antenna feed

• US 4,786,912 A
• Filed: 07/07/1986
• Issued: 11/22/1988
• Est. Priority Date: 07/07/1986
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Unisys Corporation
• Inventors: Shestag, Lowell N., Brown, Ralph A.
• Primary Examiner(s): Sikes, William L.
• Assistant Examiner(s): Johnson, Doris J.
• Application Number:
  US06/882,839
• Time in Patent Office: 869 Days
• Field of Search: 343/757, 343/758, 343/761, 343/766, 343/882, 343/786, 343/781 CA
• US Class Current: 343/761
• CPC Class Codes: H01Q 1/18 Means for stabilising antennas on an unstable platform
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 3/08 for varying two co-ordinates of the orientation
• CPC Class Codes: H01Q 3/18 wherein the primary active element is movable and the reflecting device is fixed

Abstract

An antenna system wherein the feed assembly is rotated to provide spatial polarization stabilization with respect to vehicle movement so that orthogonal polarizations can be used simultaneously.

Claims

1. An antenna system comprising,

support means (101, 102) comprising an open-ended yoke means mounted on a base wherein the support means is rotatable about an axis thereof extending vertically from said base and through said yoke means,

first drive means (151) for selectively rotating said support means about said axis of said support means,

reflector means (105) comprising a reflector dish for reflecting signals from a feed assembly pivotally mounted on said support means,

second drive means (110) for selectively rotating said reflector means about an axis of said reflector means,

feed assembly means (111, 112, 113) mounted in said support means adjacent to said reflector means,

said feed assembly means including means for generating an RF signal and a horn for transmitting said RF signal,

third drive means (117) for selectively rotating said feed assembly means about an axis of said feed assembly means,

sub-reflector means mounted adjacent to and spaced from said reflector dish in a skewed fashion relative to said reflector dish, and

stepper motor means arranged to drive said sub-reflector means in a rotary fashion about an axis of said sub-reflector means.

2. The antenna system recited in claim 1 wherein,

said support means rotates about a first axis,

said reflector means rotates about a second axis, and

said feed assembly means rotates about a third axis,

wherein said first, second and third axes are respective axes of said antenna system and,

wherein each of said support means, said reflector means, and said feed assembly means can rotate about the respective axis independently of each other.

3. The antenna system recited in claim 1 including, electromagnetic lens means mounted adjacent to said feed assembly means to produce increased gain in the operation of said feed assembly mens.

4. The antenna system recited in claim 1 wherein,

said first, second and third drive means each comprise motor drive means.

5. The antenna system recited in claim 1 including,

first, second and third synchronizer means arranged to detect the position of said support means, said reflector means and said feed assembly means respectively.

6. The antenna system recited in claim 5 including,

control means connected to each of said first, second and third drive means and to each of said first, second and third synchronizer means to determine the positions thereof and the related components of the antenna system.

7. The antenna system recited in claim 1 including,

platform means on which said antenna system is mounted and arranged for three-degrees of motion.

8. An antenna system comprising,

support means (101, 102),

first drive means (151) for selectively rotating said support means about an axis of said support means whereby said support means rotates about a first axis,

said support means includes a rotatable base and an upstanding, substantially U-shaped yoke extending above said base,

said first axis of said support means passes axially through said rotatable base and between the arms of said U-shaped yoke,

reflector means (105) pivotally mounted on said support means,

said reflector means comprises a reflector dish for reflecting signals from said feed assembly,

an elevation strut mounted in rotary joints adjacent the ends of the arms of said upstanding yoke,

said elevation strut connected to support said reflector means along the axis about which said reflector means is selectively rotated,

second drive means (110) for selectively rotating said reflector means about an axis of said reflector means whereby said reflector means rotates about a second axis,

feed assembly means (111, 112, 113) mounted in said support means adjacent to said reflector means and operative to produce an RF signal to be reflected by said reflector means,

a rotatable mounting means at said elevation strut for mounting said feed assembly means thereto,

said feed assembly includes an RF signal feed means,

signal coupler means connected to said RF signal feed means, and

transition means connected between said signal coupler means and said RF signal feed means,

third drive means (117) for selectively rotating said feed assembly means about an axis of said feed assembly means whereby said feed assembly means rotates about a third axis,

said first, second and third axes are respective axes of said antenna system whereby each of said support means, said reflector means, and said feed assembly means can rotate about the respective axis independently of each other,

first, second and third synchronizer means mounted in said antenna system and arranged to detect the position of said support means, said reflector means and said feed assembly means respectively, and

control means connected to each of said first, second and third drive means and to each of said first, second and third synchronizer means in order to supply drive control signals to the respective drive means in response to operation of the respective synchronizer means.