Multiport amplifiers (MPAs) using output filtering to improve performance over life

• US 10,320,064 B2
• Filed: 11/29/2016
• Issued: 06/11/2019
• Est. Priority Date: 02/04/2016
• Status: Active Grant

• Current Assignee: Maxar Space LLC (Galileo Parent, Inc.)
• Original Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Inventors: Vaddiparty, Subrahmanyam V., Tu, Zheng, Gallagher, Vijaya Korwar
• Primary Examiner(s): Smith, Graham P
• Application Number:
  US15/364,115
• Publication Number:
  US 20170229765A1
• Time in Patent Office: 924 Days
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 21/24 Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction circularly polarised patch antennas H01Q9/0428; circularly polarised horns H01Q13/0241; cross-polarised horns H01Q13/0258; polarisation converters H01Q15/242; cross-polarised rear feeds H01Q19/136; crossed polarisation dual antenna H01Q25/001
• CPC Class Codes: H03F 2200/294 the amplifier being a low noise amplifier [LNA]
• CPC Class Codes: H03F 2203/21157 A filter circuit being added at the output of a power amplifier stage
• CPC Class Codes: H03F 3/211 using a combination of several amplifiers H03F3/60 takes precedence
• CPC Class Codes: H04B 2001/0408 with power amplifiers
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays

Abstract

A payload subsystem of a satellite includes a plurality of transmit antenna feeds, a plurality of frequency filters, and a power amplification arrangement including a plurality of power amplifiers. The power amplification arrangement has at least one multiport amplifier, the multiport amplifier including a plurality of output ports, each output port coupled with a respective one of the plurality of transmit antenna feeds by way of a respective one of the plurality of frequency filters.

Claims

1. A payload subsystem of a satellite, comprising:

a plurality of transmit antenna feeds, a plurality of frequency filters, and a power amplification arrangement including a plurality of power amplifiers, the power amplification arrangement having at least one multiport amplifier, the multiport amplifier including a plurality of output ports, wherein;

each output port is coupled with a respective one of the plurality of transmit antenna feeds; and

each antenna feed is coupled with a single respective output port by way of a respective one of the plurality of frequency filters.

2. The payload subsystem of claim 1, wherein the payload subsystem is configured to operate at a frequency band of Ku band or higher.

3. The payload subsystem of claim 1, wherein the power amplification arrangement is configured to exhibit a ratio of carrier-to-isolation (C/I), between adjacent ones of the plurality of transmit antenna feeds, of at least 30 dB.

4. The payload subsystem of claim 3, wherein the power amplification arrangement exhibits a C/I, between adjacent ones of the plurality of transmit antenna feeds, of at least 30 dB irrespective of whether calibration of gain and phase variations over life and compensation for the gain and phase variations is performed.

5. The payload subsystem of claim 4, wherein calibration of the gain and phase variations over life and compensation for the gain and phase variations is avoided.

6. The payload subsystem of claim 3, wherein the transmit antenna feeds correspond to a coverage map comprising a plurality of coverage regions, wherein adjacent coverage regions are diverse in one or both of channel center frequency and antenna polarization.

7. The payload subsystem of claim 6, wherein the antenna polarization is diverse in one or both of linear polarization type and circular polarization type.

8. The payload subsystem of claim 1, wherein:

the payload subsystem further includes a digital channelizer configured to process a plurality of input signals and to create reconfigurable channels to route the plurality of input signals to a plurality of digital channelizer output ports; and

the plurality of digital channelizer output ports are communicatively coupled to the at least one multiport amplifier.

9. The payload subsystem of claim 8, wherein the at least one multiport amplifier includes a plurality of identical or nearly identical fixed power high power amplifiers (HPAs) whose inputs are communicatively coupled to the plurality of digital channelizer output ports.

10. The payload subsystem of claim 8, wherein the at least one multiport amplifier includes a plurality of identical or nearly identical variable power high power amplifiers (HPAs) whose inputs are communicatively coupled to the plurality of digital channelizer output ports, wherein output power levels of the variable power HPAs are set and varied approximately in unison.

11. The payload subsystem of claim 1, wherein at least one of the frequency filters has a rolloff characteristic such that there is 15 dB attenuation between adjacent ones of the plurality of transmit antenna feeds.

12. The payload subsystem of claim 1, wherein the frequency filters include surface acoustic wave filters.

13. The payload subsystem of claim 1, wherein the frequency filters are implemented as a band pass filter, a low-pass filter, a high-pass filter, or a serial combination of low-pass and high-pass filters.

14. The payload subsystem of claim 1, wherein the frequency filters have a passband at least as wide as a channel bandwidth allocated for one of the transmit antenna feeds.

15. The payload subsystem of claim 1, wherein the power amplifiers are implemented as either SSPAs or TWTAs.

16. A satellite, comprising:

a payload subsystem including a plurality of transmit antenna feeds, a plurality of frequency filters, and a power amplification arrangement including a plurality of power amplifiers, the power amplification arrangement having at least one multiport amplifier, the multiport amplifier including a plurality of output ports, wherein;

each output port coupled with a respective one of the plurality of transmit antenna feeds;

each antenna feed is coupled with a single respective output port by way of a respective one of the plurality of frequency filters; and

the payload subsystem is configured to operate at a frequency band of Ku band or higher.

17. The satellite of claim 16, wherein the power amplification arrangement is configured to exhibit a ratio of carrier-to-isolation (C/I), between adjacent ones of the plurality of transmit antenna feeds, of at least 30 dB.

18. The satellite of claim 17, wherein the power amplification arrangement exhibits a C/I, between adjacent ones of the plurality of transmit antenna feeds, of at least 30 dB irrespective of whether calibration of gain and phase variations over life and compensation for the gain and phase variations is performed.

19. The satellite of claim 18, wherein calibration of gain and phase variations over life and compensation for the gain and phase variations is avoided.

20. The satellite of claim 17, wherein the transmit antenna feeds correspond to a coverage map comprising a plurality of coverage regions, wherein adjacent coverage regions are diverse in one or both of channel center frequency and antenna polarization.