Reconfigurable multiplexer

• US 4,688,259 A
• Filed: 12/11/1985
• Issued: 08/18/1987
• Est. Priority Date: 12/11/1985
• Status: Expired due to Term

• Current Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Original Assignee: Ford Aerospace & Communications Corporation
• Inventors: Edridge, Michael J.
• Primary Examiner(s): NOT, DEFINED
• Assistant Examiner(s): Seidenglanz, Elissa
• Application Number:
  US06/807,717
• Time in Patent Office: 615 Days
• Field of Search: 455/12, 455/17, 455/25, 455/132, 455/133, 333/24.1, 333/1.1, 333/126, 333/129, 333/132, 333/134, 333/136, 343/361
• US Class Current: 455/13.3
• CPC Class Codes: H01P 1/213 combining or separating two or more different frequencies H01P1/215 takes precedence
• CPC Class Codes: H04B 7/18534 for enhancing link reliablility, e.g. satellites diversity
• CPC Class Codes: H04B 7/208 Frequency-division multiple access [FDMA]

Abstract

A dynamically reconfigurable multiplexer (7) has applicability in a space diversity communications system or a polarization reuse communications system. Multiplexer (7) may be situated on board a communications satellite or at the control nexus of a terrestrial microwave communications system. Multiplexer (7) comprises a set of N series-connected field reversible circulators (51). Coupled to one of the three ports of each circulator (51) is a channelizing filter (53), followed by an output isolator (54) and a high power amplifier (55). The electromagnetic energy rotating within each circulator (51) is commanded to move in either a clockwise or counter-clockwise direction, depending upon whether it is desired to access the channel (52) corresponding to said circulator (51) via a first energy source (1) or second energy source (2). An input isolator (43, 44) associated with each antenna (1, 2) absorbs unwanted energy emanating from the opposing antenna (2, 1).

Claims

1. A reconfigurable multiplexer comprising a string of N series-connected field reversible circulators, where N is a positive integer;

wherein

a first end of the string is coupled to a first source of electromagnetic energy, and a second end of the string is coupled to a second source of electromagnetic energy;

coupled to each circulator is a channelizing filter, wherein the N channelizing filters divide the electromagnetic energy from the two sources into a set of N frequency channels; and

the direction of rotation of electromagnetic energy within each circulator is selectively chosen so that selected ones of the N channels are assigned to the first source while selected others of the N channels are assigned to the second source.

2. The multiplexer of claim 1 wherein each source comprises an antenna;

and the two antennas point in different directions.

3. The multiplexer of claim 1 wherein each source comprises an antenna;

wherein the two antennas point in substantially the same direction and are disposed to receive electromagnetic signals that have mutually orthogonal polarizations.

4. The multiplexer of claim 1 wherein each source comprises an antenna, a receiver, and an isolator;

wherein the isolator absorbs extraneous signals emanating from the opposing source.

5. The multiplexer of claim 1 wherein each circulator is a three-port device;

and the direction of circulation of electromagnetic energy from port-to-port within the device is controlled by means of a ferrite switch.

6. The multiplexer of claim 1 situated on board a communications satellite.

7. The multiplexer of claim 1 wherein each channel comprises a channelizing filter, an output isolator, and a high power amplifier.

8. The multiplexer of claim 1 wherein each filter has an input port at which the impedance is substantially equal to the characteristic impedance of the transmission medium that couples the circulators together, within the bandwidth of the channel associated with that filter.