Antenna for multipath satellite communication links

• US 5,552,798 A
• Filed: 08/23/1994
• Issued: 09/03/1996
• Est. Priority Date: 08/23/1994
• Status: Expired due to Term

• Current Assignee: Globalstar Incorporated
• Original Assignee: Globalstar Incorporated
• Inventors: Dietrich, Frederick J., Monte, Paul A.
• Primary Examiner(s): Hajec, Donald T.
• Assistant Examiner(s): Ho, Tan
• Application Number:
  US08/294,633
• Time in Patent Office: 742 Days
• Field of Search: 343/DIG. 2, 343/700 MS, 343/754, 343/893, 343/853, 343/725, 342/352, 342/354, 29/600
• US Class Current: 343/893
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 21/061 Two dimensional planar arrays
• CPC Class Codes: H01Q 21/29 Combinations of different interacting antenna units for giving a desired directional characteristic H01Q25/00 takes precedence
• CPC Class Codes: H04B 7/18541 for handover of resources
• CPC Class Codes: H04B 7/18571 for satellites; for fixed or mobile stations
• CPC Class Codes: H04B 7/195 Non-synchronous stations
• CPC Class Codes: Y10S 343/02 Satellite-mounted antenna

Abstract

An antenna (70) includes a first sub-structure (72) having a major plane that is oriented at a first angle (for example, 90°) with respect to an axis (normal) that is perpendicular to the surface of the earth. The antenna also includes a plurality (for example six) of second sub-structures (74) individual ones of which have a local major plane that is disposed at a second angle (for example, 45°) to the major plane of the first sub-structure. Each of the plurality of sub-structures have an outwardly pointing normal from the local major plane that is oriented at a third angle (for example, 60°) around the axis from an outwardly pointing normal of an adjacent one of the sub-structures. The outwardly pointing normal of each of the plurality of sub-structures is disposed so as to point away from the axis. At least one antenna element (76) is supported by the first sub-structure and by each of the plurality of second sub-structures. Antenna elements of the first sub-structure and at least some of the plurality of second sub-structures enable a spread spectrum communication between a terminal (13) and at least one low earth orbit satellite (12) over a range of elevation angles of the low earth orbit satellite.

Claims

1. An antenna system for coupling a terminal to a plurality of satellites of a constellation of low earth orbit satellites, each of the plurality of satellites being oriented, at any given time when in view of the terminal, at a particular elevation angle, comprising:

a first sub-structure having a major plane that is oriented at a first angle with respect to an axis that is perpendicular to the surface of the earth;

a plurality N of second sub-structures individual ones of which have a local major plane that is disposed at a second angle to said major plane of said first sub-structure, each of said plurality N of sub-structures having an outwardly pointing normal from said local major plane that is oriented at a third angle around said axis from an outwardly pointing normal of an adjacent one of said sub-structures, said outwardly pointing normal of each of said plurality N of sub-structures being disposed so as to point away from said axis; and

at least one antenna element supported by said first sub-structure and by each of said plurality N of second sub-structures, wherein antenna elements of said first sub-structure and at least some of said plurality N of second sub-structures enable a spread spectrum communication between said terminal and at least one low earth orbit satellite over a range of elevation angles of said low earth orbit satellite.

2. An antenna system as set forth in claim 1 wherein said first angle is approximately 90°

, and wherein said second angle is within a range of approximately 30°

to approximately 60°

.

3. An antenna system as set forth in claim 1 wherein said third angle is approximately 60°

, and wherein N is equal to six.

4. An antenna system as set forth in claim 1 wherein said third angle is approximately 45°

, and wherein N is equal to eight.

5. An antenna system as set forth in claim 1 wherein there are a plurality of said antenna elements that are supported by each of said sub-structures, and wherein individual ones of said plurality of antenna elements are spaced apart by a distance that is a function of a wavelength of interest.

6. An antenna system as set forth in claim 1 wherein there are a plurality of said antenna elements that are supported by each of said sub-structures, and wherein individual ones of said plurality of antenna elements are spaced apart by a distance within a range of approximately 0.5 λ

to approximately 0.8 λ

, wherein λ

is a wavelength of interest.

7. An antenna system as set forth in claim 1 and further comprising at least one reference antenna element that is oriented at said first angle with respect to said axis that is perpendicular to the surface of the earth.

8. An antenna system as set forth in claim 1 wherein said first sub-structure has a generally planar, polygonal shape, and wherein individual ones of said second sub-structures each have an edge that is adjacent to one edge of said first sub-structure.

9. An antenna system as set forth in claim 1, and further comprising means for selectively outputting a signal received from at least one antenna element that is disposed upon one of said first sub-structure and said plurality N of second sub-structures.

10. An antenna system as set forth in claim 1, and further comprising means for selectively inputting a signal to at least one antenna element that is disposed upon one of said first sub-structure and said plurality N of second sub-structures.

11. An antenna system as set forth in claim 1, wherein said first angle is approximately 90°

, and wherein individual ones of said plurality N of second sub-structures are oriented so as to generally face north (N), northeasat (NE), southeast (SE), south (S), southwest (SW) and northwest (NW), or subsets of these azimuthal orientations.

12. A communication system, comprising:

a constellation of low earth orbit satellites individual ones of which each comprise means for receiving at least one communication feeder link from at least one ground station and means for transmitting the received at least one communication feeder as a downlink transmission to a plurality of terrestrially located terminals; and

at least one ground station including means for transmitting said at least one communication feeder link to at least one of said satellites and further comprising means for coupling said at least one feeder link to a terrestrially located communications system;

wherein

each of the plurality of satellites is oriented, at any given time when in view of one of said terminals, at a particular elevation angle;

characterized in that said terminal comprises,

an antenna that is comprised of a first sub-structure having a major plane that is oriented at a first angle with respect to an axis that is perpendicular to the surface of the earth;

a plurality N of second sub-structures individual ones of which have a local major plane that is disposed at a second angle to said major plane of said first sub-structure, each of said plurality N of sub-structures having an outwardly pointing normal from said local major plane that is oriented at a third angle around said axis from an outwardly pointing normal of an adjacent one of said sub-structures, said outwardly pointing normal of each of said plurality N of sub-structures being disposed so as to point away from said axis; and

at least one antenna element supported by said first sub-structure and by each of said plurality N of second sub-structures, wherein antenna elements of said first sub-structure and at least some of said plurality N of second sub-structures enable a spread spectrum communication to occur between said terminal and at least one low earth orbit satellite over a range of elevation angles of said low earth orbit satellite.

13. A communication system as set forth in claim 12 wherein said antenna is further comprised of at least one reference antenna element that is oriented at said first angle with respect to said axis that is perpendicular to the surface of the earth, and wherein said terminal further includes a multiple-finger spread spectrum receiver having inputs coupled to said plurality of antenna elements and to said at least one reference antenna element, said receiver including means for allocating one of said fingers for receiving said spread spectrum communication from said at least one low earth orbit satellite, and for allocating at least one other one of said fingers for receiving a synchronizing signal that is received through said at least one reference antenna element from at least one other of said low earth orbit satellites.

14. A communication system as set forth in claim 12 and further comprising means for selecting as an output of said antenna an output of antenna elements associated with one of said first and second sub-structures, said selecting means being responsive to at least one of a predicted position of said at least one satellite and a received signal strength that is measured at said first and second sub-structures.

15. A communication system as set forth in claim 12 and further comprising means for selecting as an output of said antenna an output of antenna elements associated with one of said first and second sub-structures, said selecting means being responsive at least to a track direction and to an elevation angle of said at least one satellite.

16. A communication system as set forth in claim 12 and further comprising means for selecting, as an output of said antenna, an output of antenna elements associated with one of said first and second sub-structures so as to switch the reception of said spread spectrum communication from said at least one low earth orbit satellite to said at least one other one of said low earth orbit satellites.

17. A communication system as set forth in claim 12, wherein said first angle is approximately 90°

, and wherein individual ones of said plurality N of second sub-structures are oriented so as to face generally north (N), northeast (NE), southeast (SE), south (S), southwest (SW) and northwest (NW), or subsets of these azimuthal orientations.

18. A communication system as set forth in claim 12, and further comprising a communication system control means that is bidirectionally coupled to said at least one ground station through a data link.

19. A communication system as set forth in claim 12, wherein said at least one ground station further comprises:

means for determining if said spread spectrum communication is to be operated in a diversity reception mode at the terminal and, if yes, for routing said spread spectrum communication simultaneously through a plurality of said low earth orbit satellites.

20. A method for operating a terminal to receive a communication from at least one satellite of a plurality of low earth orbit satellites, each of the plurality of satellites being oriented, at any given time when in view of the terminal, at a particular elevation angle and at a particular azimuth angle, comprising the steps of:

for a first range of elevation angles and azimuth angles, selecting a first portion of an antenna structure to receive the communication, the first portion being disposed at a first angle with respect to an axis that is normal to the surface of the earth;

for a second range of elevation angles and azimuth angles, selecting a second portion of the antenna structure to receive the communication, the second portion being disposed at a second angle with respect to the axis that is normal to the surface of the earth.

21. A method as set forth in claim 20 and further comprising a step of, for a third range of elevation angles and azimuth angles, selecting a third portion of the antenna structure to receive the communication, the third portion being disposed at the first angle with respect to the axis that is normal to the surface of the earth.

22. A method as set forth in claim 20 wherein the first angle is within a range of approximately 30°

to approximately 60°

, and wherein the second angle is either within the range of approximately 30°

to approximately 60°

or is approximately 90°

.

23. A method as set forth in claim 20 and further comprising the simultaneously executed steps of receiving and tracking a synchronizing signal from at least one other satellite of the plurality of satellites.

24. A method as set forth in claim 23 wherein the received communication is a spread spectrum communication, and wherein the steps of receiving and tracking include a step of locking to a synchronizing channel that is transmitted by the at least one other satellite.

25. A method as set forth in claim 20 wherein the steps of selecting each employ satellite ephemeris data to predict a position of the at least one satellite.

26. A method as set forth in claim 20 wherein the steps of selecting each employ a magnitude of a signal that is received from the at least one satellite.

27. A method for operating a terminal to transmit a communication to at least one satellite of a plurality of low earth orbit satellites, each of the plurality of satellites being oriented, at any given time when in view of the terminal, at a particular elevation angle and at a particular azimuth angle, comprising the steps of:

for a first range of elevation angles and azimuth angles, selecting a first portion of an antenna structure to transmit the communication, the first portion being disposed at a first angle with respect to an axis that is normal to the surface of the earth; and

for a second range of elevation angles and azimuth angles, selecting a second portion of the antenna structure to transmit the communication, the second portion being disposed at a second angle with respect to the axis that is normal to the surface of the earth.

28. A method as set forth in claim 27 and further comprising a step of, for a third range of elevation angles, selecting a third portion of the antenna structure to transmit the communication, the third portion being disposed at the first angle with respect to the axis that is normal to the surface of the earth.

29. A method as set forth in claim 27 wherein the first angle is within a range of approximately 30°

to approximately 60°

, and wherein the second angle is either within the range of approximately 30°

to approximately 60°

or is approximately 90°

.

30. A method as set forth in claim 27 wherein the steps of selecting each employ satellite ephemeris data to predict a position of the at least one satellite.

31. A method as set forth in claim 27 wherein the steps of selecting each employ a magnitude of a signal that is received from the at least one satellite.

32. A method for operating a terminal to receive a communication from at least one satellite of a plurality of low earth orbit satellites, each of the plurality of satellites being oriented, at any given time when in view of the terminal, at a particular elevation angle and at a particular azimuth angle, comprising the steps of:

for a first predicted range of elevation angles and azimuth angles of the at least one satellite, selecting a first portion of an antenna structure to receive the communication, the first portion being disposed at a first angle with respect to an axis that is normal to the surface of the earth; and

for a second predicted range of elevation angles and azimuth angles of the at least one satellite, selecting a second portion of the antenna structure to receive the communication, the second portion being disposed at a second angle with respect to the axis that is normal to the surface of the earth.

33. A method as set forth in claim 32 wherein the first angle is within a range of approximately 30°

to approximately 60°

, and wherein the second angle is either within the range of approximately 30°

to approximately 60°

or is approximately 90°

.

34. A method for operating a terminal to receive a communication from at least one satellite of a plurality of low earth orbit satellites, each of the plurality of satellites being oriented, at any given time when in view of the terminal, at a particular elevation angle and at a particular azimuth angle, comprising the steps of:

measuring a signal strength of a signal received from the at least one satellite with at least one of a plurality of antennas individual ones of which are oriented to receive a satellite transmission from a satellite disposed within a range of elevation angles and azimuth angles, wherein certain ones of the ranges of elevation angles and azimuth angles overlap one another;

for a first range of elevation angles and azimuth angles of the at least one satellite wherein the measured signal strength exceeds a predetermined threshold value, selecting a first antenna to receive the communication, the first antenna being oriented at a first angle with respect to an axis that is normal to the surface of the earth; and

for a second range of elevation angles and azimuth angles of the at least one satellite wherein the measured signal strength exceeds the predetermined threshold value, selecting a second antenna to receive the communication, the second antenna being oriented at a second angle with respect to the axis that is normal to the surface of the earth.

35. A method as set forth in claim 34 wherein the first angle is within a range of approximately 30°

to approximately 60°

, and wherein the second angle is either within the range of approximately 30°

to approximately 60°

or is approximately 90°

.