Configurable backing structure for a reflector antenna and corrective synthesis for mechanical adjustment thereof

Patent metadata

Field	Value
Publication number	US-9337544-B2
Application number	US-201414148618-A
Country	US
Kind code	B2
Filing date	Jan 6, 2014
Priority date	Jan 7, 2013
Publication date	May 10, 2016
Grant date	May 10, 2016

Abstract

A reflector support system is provided that includes a backing structure having a plurality of struts. The backing structure may have a plurality of hubs, each of the plurality of hubs may be configured to couple to two or more of the plurality of struts, each of the plurality of hubs may be configured to couple to another one of the plurality of hubs using one of the plurality of struts, each of the plurality of struts is configured to couple to at least two of the plurality of hubs. The backing structure may have a plurality of feet, each of the plurality of feet configured to couple to a corresponding one of the plurality of hubs, the plurality of feet are configured to couple to a reflector. In addition, a synthesis for mechanical adjustment of the reflector support system is provided.

First claim

What is claimed is the following:

1. An antenna reflector support apparatus, comprising:
a backing structure comprising:
a plurality of struts;
a plurality of hubs, each of the plurality of hubs configured to couple to two or more of the plurality of struts, each of the plurality of hubs is configured to couple to another one of the plurality of hubs using one of the plurality of struts, each of the plurality of struts is configured to couple to at least two of the plurality of hubs; and
a plurality of feet, each of the plurality of feet configured to couple to a corresponding one of the plurality of hubs, the plurality of feet are configured to couple to a reflector, and each of at least one or more of the plurality of feet comprising:
a post;
a fitting coupled to the post; and
a base coupled to the fitting, the fitting comprises a movable ball joint to allow each of the at least one or more of the plurality of feet to tilt when each of the at least one or more of the plurality of feet is attached to the reflector,

wherein the plurality of struts and the plurality of hubs are configured to allow the backing structure to have a grid structure.

2. The antenna reflector support apparatus of claim 1 , wherein the distance between the reflector and the backing structure is adjustable.

3. The antenna reflector support apparatus of claim 1 , wherein each of the at least one or more of the plurality of feet comprises a doubler.

4. The antenna reflector support apparatus of claim 1 , wherein the moveable ball joint is fixable to prevent each of the at least one or more of the plurality of feet from tilting when each of the at least one or more of the plurality of feet is attached to the reflector.

5. The antenna reflector support apparatus of claim 1 , wherein the plurality of hubs and the plurality of struts form a backing truss, and the backing truss is spherical.

6. The antenna reflector support apparatus of claim 1 , wherein each of the plurality of hubs is coplanar with each other.

7. The antenna reflector support apparatus of claim 1 , wherein each of the plurality of hubs is configured to accept four or more of the plurality of struts.

8. The antenna reflector support apparatus of claim 1 , wherein:
each of the plurality of struts has the same shape and size as the other one of the plurality of struts,
each of the plurality of feet has the same shape and size as the other one of the plurality of feet,
each of the plurality of hubs configured to be formed at an outer edge of the backing structure has the same shape and size as the other one of the plurality of hubs configured to be formed at an outer edge of the backing structure, and
each of the plurality of hubs configured to be formed within an inner portion of the backing structure has the same shape and size as the other one of the plurality of hubs configured to be formed within an inner portion of the backing structure.

9. The antenna reflector support apparatus of claim 1 , wherein each of the plurality of struts is rigid, each of the plurality of hubs is rigid, and each of the plurality of feet is rigid.

10. The antenna reflector support apparatus of claim 1 , wherein:
each of the plurality of hubs is attached to two or more of the plurality of struts,
each of the plurality of hubs is attached to another one of the plurality of hubs using one of the plurality of struts,
each of the plurality of struts is attached to at least two of the plurality of hubs,
each of the plurality of feet is attached to a corresponding one of the plurality of hubs,
the plurality of feet are attached to the reflector,
the backing structure comprises a grid structure,
a bottom shape of the backing structure, at the bottom of the plurality of feet, substantially conforms to the outer shape of the reflector,
at least one of the plurality of hubs located at an edge of the backing structure is attached to a first location of a corresponding one of the plurality of feet, and at least one of the plurality of hubs located within an inner portion of the backing structure is attached to a second location of a corresponding one of the plurality of feet, wherein a distance between the first location and the reflector is greater than a distance between the second location and the reflector.

11. A method, comprising:
forming a backing structure, comprising:
a plurality of struts;
a plurality of hubs coupled to the plurality of struts; and
a plurality of feet coupled to the plurality of hubs, the plurality of feet coupled to a reflector;
mounting photogrammetry targets to a surface of the reflector;
measuring a point cloud using the mounted photogrammetry targets;
calculating an error surface of the reflector surface based on the measured point cloud;
calculating adjustment amplitudes based on the calculated error surface; and
adjusting the distance between the plurality of feet and the reflector based on the adjustment amplitudes.

12. The method of claim 11 , further comprising:
calculating a predicted surface based on the adjustment amplitudes; and
comparing the calculated error surface with the calculated predicted surface.

13. The method of claim 11 , wherein the calculating adjustment amplitudes comprises using deviation matrices, wherein the deviation matrices are calculated using a finite element model of the backing structure and the reflector.

14. The method of claim 11 , wherein the calculating an error surface comprises using quintic pseudosplines.

15. The method of claim 11 , further comprising measuring a radiation pattern to confirm the adjusting the distance between the plurality of feet and the reflector based on the adjustment amplitudes.

Assignees

• Lockheed Corp

Inventors

• Theunissen Wilhelmus H
• Talley Eric
• Brokaw William D
• Sturges James Howard
• Cantor Nathaniel David

Classifications

• H01Q15/148

  with means for varying the reflecting properties (H01Q15/147 takes precedence) · CPC title

• H01Q15/14 Primary

  Reflecting surfaces; Equivalent structures {(electromagnetic shields H01Q1/526)} · CPC title

• H01Q1/12

  Supports; Mounting means · CPC title

• Y10T29/49769

  Using optical instrument [excludes mere human eyeballing] · CPC title

• H01Q15/147

  provided with means for controlling or monitoring the shape of the reflecting surface (for scanning H01Q3/01; aerials or aerial systems providing multiple beamwidths H01Q25/002) · CPC title