Satellite communications system having frequency addressable high gain downlink beams

• US 4,823,341 A
• Filed: 08/14/1986
• Issued: 04/18/1989
• Est. Priority Date: 08/14/1986
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Rosen, Harold A.
• Primary Examiner(s): Cangialosi, Salvatore
• Application Number:
  US06/896,982
• Time in Patent Office: 978 Days
• Field of Search: 370/104, 370/75, 455/12, 455/33
• US Class Current: 370/325
• 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 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/2041 Spot beam multiple access
• CPC Class Codes: Y02D 30/70 in wireless communication networks

Abstract

A satellite communications employs separate subsystems for providing broadcast and point-to-point two-way communications using the same assigned frequency band. The broadcast and point-to-point subsystems employ an integrated satellite antenna system which uses a common reflector (12). The point-to-point subsystem achieves increased communication capacity through the reuse of the assigned frequency band over multiple, contiguous zones (32, 34, 36, 38) covering the area of the earth to be serviced. Small aperture terminals in the zones are serviced by a plurality of high gain downlink fan beams (29) steered in the east-west direction by frequency address. A special beam-forming network (98) provides in conjunction with an array antenna (20) the multiple zone frequency address function. The satellite (10) employs a filter interconnection matrix (90) for connecting earth terminals in different zones in a manner which permits multiple reuse of the entire band of assigned frequencies. A single pool of solid state transmitters allows rain disadvantaged users to be assigned higher than normal power at minimum cost. The intermodulation products of the transmitters are geographically dispersed.

Claims

1. A satellite communications system for communicatively interconnecting a plurality of terminal sites distributed over an area of the earth, comprising:

an earth orbiting satellite; and

frequency responsive means carried by said satellite for forming a plurality of beams of electromagnetic radiation between said area on the earth and said satellite with each beam of radiation having a carrier frequency, said beam forming means including an array of radiating elements and an antenna for producing all of said beams, said beams being arranged in at least two groups thereof respectively covering two essentially contiguous zones within said area, the beams in said groups thereof intersecting said area on the earth in seriatim along an arc with the position of each of said beams along said arc being determined by the carrier frequency of the beam, said groups of beams being arranged essentially end-to-end along said arc, the beams in each group thereof being carried by the same preselected set of frequencies such said set of frequencies is reused by said beams.

2. The satellite communications system of claim 1, wherein the carrier frequencies of immediately adjacent portions of two contiguous zones serviced by two respectively associated beams are sufficiently different in frequency to prevent communication interference therebetween.

3. The satellite communications system of claim 1, wherein said preselected set of frequencies includes a first range of up-link carrier frequencies and a second range of down-link carrier frequencies.

4. The satellite communications system of claim 3, including means for selecting the up-link carrier frequency for an uplink terminal site as a function of the location of the downlink terminal site along said arc which is intended to receive communications signals from said up-link terminal site.

5. The satellite communications system of claim 1, wherein the number of beams formed using downlink carrier frequencies is equal to the number of beams formed using the uplink carrier frequencies.

6. The satellite communications system of claim 3, wherein said uplink carrier frequencies are arranged in a a plurality of frequency bands defining a set of uplink channels and said downlink carrier frequencies are arranged in a a plurality of frequency bands defining downlink channels respectively associated with said uplink channels, said system including means carried by said satellite for interconnected said uplink channels with said downlink channels in a preselected pattern such that uplink beams signals on each of said uplink channels is delivered to a downlink terminal site on a preselected downlink channel.

7. The satellite communications system of claim 6, wherein said interconnecting means includes:

at least one input for receiving signals over said uplink channels,

a plurality of outputs, and

means connected between said inputs and said outputs for separating said uplink channels and for routing each of said separated uplink channels with a preselected one of said outputs.

8. The satellite communications system of claim 7, wherein said separating and routing means includes a plurality of frequency filters for respectively filtering said uplink channels.

9. The satellite communications system of claim 1, wherein said beam forming means includes:

a first plurality of lines for respectively carrying transmit signals to be transmitted to earth by said beams;

a second plurality of spaced apart lines intersecting said first plurality of lines at crossover points, each of said second plurality of lines being electromagnetically coupled with each of said first plurality of lines at said crossover points such that a portion of the energy of each of the transmit signals carried by each of the first plurality of lines is transferred to each of said second plurality of lines, each of said second plurality of lines having an output for outputting all of said transmit signals.

10. The satellite communications system of claim 9, wherein the distance between adjacent ones of said crossover points and the width of each of said plurality of lines is preselected to produce a desired shift in the phase of said transmit signals.

11. The satellite communications system of claim 9, wherein said second plurality of lines extend essentially radially from a reference point such that said second plurality of lines diverge from each other.

12. The satellite communications system of claim 11, wherein said first plurality of lines extend circumferentially about said reference point and are radially spaced relative to said reference point such that the distance between adjacent crossover points increases with increasing radial distance of the crossover points from said reference point.

13. The satellite communications system of claim 9, wherein said first plurality of lines includes a plurality of transmission lines for conveying electromagnetic energy and said second plurality of lines includes a plurality of electromagnetic energy waveguides.

14. The satellite communications system of claim 13, wherein each of said transmission lines is coupled with each of said waveguides by an electromagnetic wave crossguide coupler.

15. The satellite communications systems of claim 9, wherein at least two of said first plurality of lines are substantially contiguous to each other.

16. The satellite communications system of claim 9, wherein at least two of said first plurality of lines are spaced from each other.

17. A method of communicatively interconnecting a plurality of terminal sites in an area on the earth using an earth orbiting communications satellite, comprising the steps of:

(A) forming a first plurality of beams of electromagnetic radiation in an arc between said satellite and the earth and covering a first zone of said area and arranged in seriatim, said beams in said first plurality thereof respectively having carrier frequencies defining a preselected set; and

,

(B) forming a second plurality of beams of electromagnetic radiation in said arc between said satellite and the earth and covering a second zone of said area essentially contiguous to said first zone and arranged in seriatim, said first and second pluralities of beams being arranged essentially end-to-end along said arc, said beams in said second plurality thereof respectively having the same carrier frequencies as said first plurality of said beams, such that said preselected set of frequencies is reused, each of said beams in said first and second pluralities thereof being formed such that the position of the beam along said arc is determined by the carrier frequency of the beam.

18. The method of claim 17, wherein:

step (A) and (B) each include the steps of forming a plurality of uplink beams of electromagnetic radiation respectively having a set of uplink carrier frequencies, and forming a plurality of downlink beams of electromagnetic radiation respectively having a set of downlink carrier frequencies, and

said method further includes the step of selecting the uplink carrier frequency for an uplink terminal site as a function of the location of the downlink terminal site in either of said zones which is intended to receive communication signals from an uplink terminal site.

19. The method of claim 18, including the steps of:

assigning uplink and downlink channels to groups of carrier frequencies respectively in said uplink and downlink carrier frequencies, and

interconnecting said uplink channels with said downlink channels in a preselected pattern such that uplink signals on each of said uplink channels is delivered to a downlink terminal site on a preselected downlink channel.

20. The method of claim 17, including the step of selecting carrier frequencies respectively in immediately adjacent portions of contiguous zones which are substantially different in frequency whereby to prevent communication interference therebetween.