Multiple beam satellite antenna with preferred polarization distribution

• US 4,232,321 A
• Filed: 11/24/1978
• Issued: 11/04/1980
• Est. Priority Date: 11/24/1978
• Status: Expired due to Term

• Current Assignee: Bell Telephone Laboratories, Inc. (Nokia Corporation)
• Original Assignee: Bell Telephone Laboratories, Inc. (Nokia Corporation)
• Inventors: Ohm, Edward A.
• Primary Examiner(s): Lieberman, Eli
• Application Number:
  US05/963,461
• Time in Patent Office: 711 Days
• Field of Search: 343/DIG. 2, 343/777, 343/778, 343/779, 343/781 CA, 343/853, 343/854, 343/100 ST, 343/100 PE
• US Class Current: 343/778
• CPC Class Codes: H01Q 25/00 Antennas or antenna systems providing at least two radiating patterns arrangements for changing or varying the orientation or the shape of the directional pattern H01Q3/00
• CPC Class Codes: H04B 7/10 Polarisation diversity; Directional diversity
• CPC Class Codes: H04B 7/2041 Spot beam multiple access
• CPC Class Codes: Y10S 343/02 Satellite-mounted antenna

Abstract

Microwave energy feed elements for launching essentially linearly polarized beams in a satellite communications system are oriented in the satellite'"'"'s antenna so that the polarization directions of the feed elements form a rim and spoke configuration. The vertical polarizations are arranged to extend radially from a point on the antenna'"'"'s focal surface which images the point on the surface of the celestial body directly below the satellite. Horizontal polarizations are arranged concentrically about the subsatellite image point. Electromagnetic energy launched from the feed elements will reach the surface of the earth at planes of incidence which are locally vertical and horizontal, thereby minimizing cross-polarization coupling between the orthogonally polarized signals due to such energy passing through precipitation.

Claims

1. In a satellite communications system, a method of transmitting electromagnetic energy from a satellite to a remote receiving area on the surface of a celestial body which results in a reduced amount of cross-polarization coupling along the transmission path, the satellite being in orbit directly above a subsatellite point (51) on the celestial body and comprises an antenna arrangement comprising (a) at least a main reflector aperture, a feed and a focal surface disposed transversely about the feed axis, the focal surface being comprised of a plurality of focal points, each of which corresponds to a respective point in the remote receiving area and a projection of the subsatellite point (50) on the focal surface and (b) plural feed elements disposed on the focal surface, the method comprising the step of:

(a) energizing one or more feed elements (e.g., 113,

     114) for transmitting at least one beam of electromagnetic energy comprising any combination of a first and a second direction of essentially linear polarization which are orthogonal to one another toward the portions of the receiving area on the celestial body associated with the particular points on the focal surface where the energized feed elements are disposed,

CHARACTERIZED IN THAT

the method comprises the further step of;

(b) in performing step (a), energizing the one or more feed elements for transmitting the at least one beam of electromagnetic energy so that when the first direction of polarization is used by any particular one of the energized feed elements, the first direction is aligned parallel to a line on the focal surface connecting the corresponding subsatellite point and the point where the particular feed element is disposed (60-66), and when the second direction of polarization is used by any particular one of the feed elements, the second direction is aligned orthogonal to the line on the focal surface connecting the corresponding subsatellite point and the point on the focal surface where the particular feed element is disposed (70-73).

2. The method of claim 1

CHARACTERIZED IN THAT

the method comprises the further step of:

(c) in performing step (b), producing the at least one beam of electromagnetic energy from the combined energies produced by a separate cluster (e.g.,

     10) of adjacent feed elements (e.g., 113, 112,

     114) for each beam, each of which feed elements being energized to produce energy in dominant (115) and higher order (116) modes of operation and aligned with any combination of the first and second polarization directions.

3. The method of claim 2 wherein the feed elements are disposed in a near field region close to the focal surface of the antenna, and launch electromagnetic energy to a distant target in a far field of the antenna

CHARACTERIZED IN THAT

the method comprises the further step of:

(d) in performing step (c), arranging the feed elements with respect to the antenna structure to achieve selectable amounts of phase shifts to preselected ones of the modes of operation in the far field of the antenna with respect to the phase of such modes in the near field of the antenna.

4. The method of claim 3

CHARACTERIZED IN THAT

the method comprises the further step of:

(e) in performing step (d), arranging the feed elements with respect to the antenna structure to achieve phase reversal of selectable ones of the higher order modes of operation in the far field of the antenna (e.g., E'"'"'₁₁₆) with respect to the phase of such higher order modes in the focal region of the antenna (e.g., E₁₁₆) to achieve alignment in the far field of the polarization direction of the composite electromagnetic beam with any combination of locally vertical and horizontal planes of incidence at the receiving area on the celestial body in the far field.

5. In a satellite communication system of the type wherein a predetermined zone on the surface of a celestial body in the far field is illuminated by a plurality of electromagnetic energy beams produced by an array of feed elements disposed near the focal surface of a satellite antenna, adjacent ones of which feed elements illuminate respectively associated contiguous areas within the predetermined zone and capable of launching electromagnetic energy in any combination of first and second essentially linear, orthogonal directions of polarization, an arrangement for producing a plurality of composite beams, each of which is composed of the combined illumination of a cluster (e.g., 10) of plural, adjacent feed elements (e.g., 113, 112, 114),

CHARACTERIZED IN THAT

the arrangement comprises

means capable of energizing each feed element in a cluster (e.g., 10) to launch a respective beam of electromagnetic energy so that when the first direction of polarization is used by any particular one of the energized feed elements, the first direction is aligned parallel to a line on the focal surface connecting an image of a subsatellite point directly below the satellite and the point where the particular feed element is disposed (e.g., 60), and when the second direction of polarization is used by any particular one of the feed elements, the second direction is aligned orthogonal to the line on the focal surface connecting the imaged subsatellite point and the point on the focal surface where the particular feed element is disposed (e.g., 71).

6. The arrangement of claim 5

CHARACTERIZED IN THAT

the arrangement comprises

means in the feed elements for launching electromagnetic energy while operating in both a dominant mode (115) and predetermined ones of higher order modes (116) of operation and aligned with any combination of the first and second polarization directions.

7. The arrangement of claim 6

CHARACTERIZED IN THAT

the arrangement further comprises

means for achieving phase reversal of selectable ones of the higher order modes in the far field (E'"'"'₁₁₆) with respect to the phase of such higher order modes in the near field (E₁₁₆) so as to achieve alignment of the directions of polarization in the far field with a selectable combination of locally vertical and horizontal planes of incidence on the predetermined zone.