Systems for surveillance using airborne platforms as receiving platforms for bistatic radars

• US 10,277,306 B2
• Filed: 10/17/2017
• Issued: 04/30/2019
• Est. Priority Date: 02/27/2013
• Status: Active Grant

• Current Assignee: Spatial Digital Systems Inc
• Original Assignee: Spatial Digital Systems Inc
• Inventors: Chang, Donald C. D.
• Primary Examiner(s): Huynh, Dung B
• Application Number:
  US15/786,542
• Publication Number:
  US 20180102832A1
• Time in Patent Office: 560 Days
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: H04B 1/0483 Transmitters with multiple parallel paths
• CPC Class Codes: H04B 7/0617 for beam forming
• CPC Class Codes: H04B 7/18504 Aircraft used as relay or high altitude atmospheric platform
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service
• CPC Class Codes: H04W 4/38 for collecting sensor information
• CPC Class Codes: H04W 4/90 Services for handling of emergency or hazardous situations, e.g. earthquake and tsunami warning systems [ETWS]
• CPC Class Codes: H04W 84/06 Airborne or Satellite Networks space-based or airborne stations H04B7/185
• CPC Class Codes: H04W 84/12 WLAN [Wireless Local Area Networks]
• CPC Class Codes: H04W 84/18 Self-organising networks, e.g. ad-hoc networks or sensor networks

Abstract

A system includes a ground hub and a mobile airborne platform hovering over or close to a coverage area on or near the earth surface. The mobile airborne platform comprises a bistatic radar receiver including an antenna system to capture first radiofrequency signals originated from a first satellite and second radiofrequency signals originated from a second satellite, via direct paths and via reflected paths from the coverage area. The mobile airborne platform transmits the captured first and second radiofrequency signals to a ground hub via a feeder link. The ground hub includes a remote beam forming network to remotely form receiving beams for the antenna system of the bistatic radar receiver to capture the first and second radiofrequency signals, and a remote radar processing center to transform the captured first and second radiofrequency signals into a first and a second two-dimensional radiofrequency image, respectively.

Claims

1. A system comprising:

a first mobile airborne platform hovering over or close to a coverage area on earth surface or near the earth surface, the first mobile airborne platform comprising a bistatic radar receiver including a first antenna system to capture first radiofrequency signals originated from a first satellite, the captured first radiofrequency signals including first radiation signals captured via a first direct path from the first satellite and first reflected radiation signals captured via first reflected paths from the coverage area, and second radiofrequency signals originated from a second satellite, the captured second radiofrequency signals including second radiation signals captured via a second direct path from the second satellite and second reflected radiation signals captured via second reflected paths from the coverage area, the first mobile airborne platform transmitting the captured first and second radiofrequency signals to a ground hub via a feeder link; and

the ground hub comprising;

a remote beam forming network to remotely form receiving beams for the first antenna system of the bistatic radar receiver to capture the first and second radiofrequency signals; and

a remote radar processing center to transform the captured first radiofrequency signals into a first two-dimensional radiofrequency image, and to transform the captured second radiofrequency signals into a second two-dimensional radiofrequency image.

2. The system of claim 1, wherein the remote radar processing center transforms the first and second two-dimensional radiofrequency images into a three-dimensional radiofrequency image such that a first projection of the three-dimensional radiofrequency image in a first direction is nearly identical to the first two-dimensional radiofrequency image and a second projection of the three-dimensional radiofrequency image in a second direction is nearly identical to the second two-dimensional radiofrequency image.

3. The system of claim 1, wherein the first and second satellite transmit radiations over the coverage area in a C, Ku, Ka or another satellite communication band.

4. The system of claim 1, wherein the feeder link is in a Ku or Ka band and wherein the first mobile airborne platform comprises a retrodirective antenna system for transmitting and receiving in the Ku or Ka band.

5. The system of claim 1, wherein the ground hub further comprises:

a remote beam forming network to transform source signals into beam signals;

a wavefront multiplexer coupled to the remote beam forming network, the wavefront multiplexer performing a wavefront multiplexing transformation on input signals that include the beam signals and known diagnostic signals and generating wavefront multiplexed signals;

a bank of adaptive filters coupled to the wavefront multiplexer to equalize the wavefront multiplexed signals; and

an optimization unit coupled to the bank of adaptive filters to modify weightings of the adaptive filters based on differences between the known diagnostic signals and recovered diagnostic signals received from the first airborne platform via the feeder-link.

6. The system of claim 5, wherein the first mobile airborne platform comprises:

a second antenna system to receive a signal from the ground hub via the feeder-link;

a receive frontend system coupled to the second antenna system to condition the signal;

a frequency demultiplexing system coupled to the receive frontend system to frequency down convert and demultiplex the conditioned signal and generate baseband signals; and

a wavefront demultiplexer coupled to the frequency demultiplexing system to perform a wavefront demultiplexing transformation on the baseband signals and generate wavefront demultiplexed signals including recovered beam signals and recovered forward-link diagnostic signals.

7. The system of claim 1, wherein the ground hub further comprises:

a hub antenna system for receiving a signal from the first mobile airborne platform;

a receive frontend system coupled to the hub antenna system to condition the signal;

a frequency demultiplexing system coupled to the receive frontend system to frequency down convert and demultiplex the conditioned signal and generate baseband signals;

a bank of adaptive filters coupled to the frequency demultiplexing system to equalize the baseband signals;

a wavefront demultiplexer coupled to the bank of adaptive filters to perform a wavefront demultiplexing transformation on the baseband signals and generate wavefront demultiplexed signals including recovered element signals and recovered return-link diagnostic signals;

a receive digital beam forming network coupled to the wavefront demultiplexer to convert the recovered element signals to beam signals; and

a return-link optimization unit coupled to the wavefront demultiplexer and the bank of adaptive filters to modify weightings of the adaptive filters based on at least differences between the recovered return-link diagnostic signals and known diagnostic signals.

8. The communications system of claim 7, wherein the first mobile airborne platform further comprises:

low-noise amplifiers coupled to the first antenna system to amplify the captured first and second radiofrequency signals;

frequency converter units coupled to the low-noise amplifiers to frequency-convert the amplified captured signals and generate element signals;

a wavefront multiplexer coupled to the frequency converter units, the wavefront multiplexer performing a wavefront multiplexing transformation on input signals that include the element signals, the known diagnostic signals, and recovered forward-link diagnostic signals that are previously obtained from a forward-link calibration, and generating wavefront multiplexed signals;

a frequency multiplexing system coupled to the wavefront multiplexer to transform the wavefront multiplexed signals into at least one frequency multiplexed signal;

a transmit backend system coupled to the frequency multiplexing system to frequency up-convert and amplify the at least one frequency multiplexed signal and generate at least one amplified signal; and

a second antenna system coupled to the transmit backend system to radiate the at least one amplified signal toward the ground hub.

9. The system of claim 1, wherein the first and second satellites transmit respectively the first and second radiation signals at a first frequency slot and a second frequency slot, respectively.

10. The system of claim 1, wherein the first and second satellites transmit respectively the first and second radiation signals at a common frequency slot in a Ka or Ku band.

11. The system of claim 1, wherein one of the first and second satellites is a Ka or Ku high throughput satellite (HTS) in a geostationary orbit (GSO), or a Ka or Ku direct broadcasting satellite in a geostationary orbit (GSO), or a commercial satellite in a non-geostationary orbit (NGSO).

12. The system of claim 1, wherein the first mobile airborne platform is an unmanned aerial vehicle (UAV).

13. The system of claim 1, further comprising:

at least a second mobile airborne platform hovering over or close to the coverage area, the at least second mobile airborne platform comprising a second bistatic radar receiver including a third antenna system to capture third radiofrequency signals originated from the first satellite, the captured third radiofrequency signals including third radiation signals captured via a third direct path from the first satellite and third reflected radiation signals captured via third reflected paths from the coverage area, and fourth radiofrequency signals originated from the second satellite, the captured fourth radiofrequency signals including fourth radiation signals captured via a fourth direct path from the second satellite and fourth reflected radiation signals captured via fourth reflected paths from the coverage area, the at least second mobile airborne platform transmitting the captured third and fourth radiofrequency signals to the ground hub via a respective feeder link.

14. The system of claim 1, wherein the first mobile airborne platform comprises at least one of optical sensors, infrared sensors, microwave sensors.

15. A system comprising:

a set of mobile airborne platforms hovering over or close to a coverage area on earth surface or near the earth surface, each of the mobile airborne platforms comprising a bistatic radar receiver including a first antenna system to capture first radiofrequency signals originated from a first satellite, the captured first radiofrequency signals including first radiation signals captured via a first direct path from the first satellite and first reflected radiation signals captured via first reflected paths from the coverage area, and second radiofrequency signals originated from a second satellite, the captured second radiofrequency signals including second radiation signals captured via a second direct path from the second satellite and second reflected radiation signals captured via second reflected paths from the coverage area, each of the mobile airborne platforms transmitting the respective captured first and second radiofrequency signals to a ground hub via a respective feeder link; and

the ground hub comprising;

a remote beam forming network to remotely form receiving beams for each of the first antenna systems to capture the respective first and second radiofrequency signals; and

a remote radar processing center to transform the captured respective first radiofrequency signals into respective first two-dimensional radiofrequency images, and to transform the captured respective second radiofrequency signals into respective second two-dimensional radiofrequency images.

16. The system of claim 15, wherein the remote radar processing center transforms the respective first and second two-dimensional radiofrequency images into three-dimensional radiofrequency images such that a first projection of one of the three-dimensional radiofrequency images in a first direction is nearly identical to one of the first two-dimensional radiofrequency images and a second projection of the one of the three-dimensional radiofrequency images in a second direction is nearly identical to one of the second two-dimensional radiofrequency images.

17. The system of claim 15, wherein the first and second satellite transmit radiations over the coverage area in a C, Ku, Ka or another satellite communication band.

18. The system of claim 15, wherein the respective feeder links are in a Ku or Ka band and wherein each of the mobile airborne platforms comprises a retrodirective antenna system for transmitting and receiving in the Ku or Ka band.

19. The system of claim 15, wherein the ground hub further comprises:

a remote beam forming network to transform source signals into beam signals;

a wavefront multiplexer coupled to the remote beam forming network, the wavefront multiplexer performing a wavefront multiplexing transformation on input signals that include the beam signals and known diagnostic signals and generating wavefront multiplexed signals;

a bank of adaptive filters coupled to the wavefront multiplexer to equalize the wavefront multiplexed signals; and

an optimization unit coupled to the bank of adaptive filters to modify weightings of the adaptive filters based on differences between the known diagnostic signals and recovered diagnostic signals received from one of the airborne platforms via a respective feeder-link.

20. The system of claim 19, wherein each of the mobile airborne platforms comprises:

a second antenna system to receive a signal from the ground hub via the respective feeder-link;

a receive frontend system coupled to the second antenna system to condition the signal;

a frequency demultiplexing system coupled to the receive frontend system to frequency down convert and demultiplex the conditioned signal and generate baseband signals; and

a wavefront demultiplexer coupled to the frequency demultiplexing system to perform a wavefront demultiplexing transformation on the baseband signals and generate wavefront demultiplexed signals including recovered beam signals and recovered forward-link diagnostic signals.