Lightweight Space-Fed Active Phased Array Antenna System

• US 20090009391A1
• Filed: 06/09/2006
• Published: 01/08/2009
• Est. Priority Date: 06/09/2005
• Status: Active Grant

• Current Assignee: Maxar Technologies ULC (Galileo Parent, Inc.)
• Original Assignee: Macdonald Dettwiler and Associates Limited
• Inventors: James, Kenneth V., Fox, Peter A.
• Granted Patent: US 7,889,129 B2
• Time in Patent Office: Days
• US Class Current: 342/372
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 21/0018 Space- fed arrays
• CPC Class Codes: H01Q 3/46 Active lenses or reflecting arrays

Abstract

A system for a satellite includes a core system and multiple nodes for generating an active phased array. Each node includes a transceiver for wirelessly receiving a transmit signal from the core system, for wirelessly transmitting the transmit signals to a target, for wirelessly receiving the receive signals from the target, and for wirelessly transmitting the receive signal back to the core system. The system also includes a subsystem for inhibiting signal interference between the transmit and receive signals. Each of the nodes may also include local power generation circuitry.

Claims

1. A space-based antenna system for a satellite, the system comprising:

a central system of the space-based antenna system, wherein the central system includes;

a stable local oscillator configured to generate a reference frequency signal,

circuitry configured to generate transmit signals based at least in part on the reference frequency signal,

at least one system transceiver for transmitting the reference frequency signal and the transmit signal, and to receive a receive signal; and

,

multiple active antenna nodes forming a portion of an active phased array antenna system, wherein each active antenna node includes;

at least one node transceiver configured to receive the reference frequency signal and the transmit signal from the system transceiver, and to transmit the receive signal to the system transceiver,

frequency translating circuitry coupled to receive the reference frequency signal, and to provide signal translation between the transmit and receive signals to inhibit interference between the transmit and receive signals,

a power generation portion, and

control circuitry coupled with the node transceiver and the power generation portion, wherein the control circuitry is configured to process or control the transmit and receive signals, and configured to at least facilitate control of beam formation and beam steering of the space-based antenna system using, at least in part, the reference frequency signal and, one or both of the transmit and receive signal.

2. The system of claim 1 wherein the control circuitry employs timing signals local with respect to the node, and wherein the space-based antenna system employs phase control using a distributed reference frequency.

3. The system of claim 1, further comprising at least one antenna wing that retains at least some of the active antenna nodes, and an antenna distortion compensation system that includes:

multiple optical targets positioned on the antenna wing;

at least one image sensor for locating at least some of the multiple targets on the antenna wing and outputting an image signal; and

a geometry compensation subsystem for processing the output image signal and generating a distortion compensation signal.

4. The system of claim 1, further comprising at least one antenna wing that retains at least some of the active antenna nodes, wherein the antenna wing includes a radiating panel portion on one side and solar cells on a reverse side, and provides both structural support and acts as an antenna.

5. The system of claim 1, further comprising stable local oscillator phase control circuitry coupled to the stable local oscillator for implementing a swept receive mode of the space-based antenna system, wherein the phase control circuitry is configured to adjust a received signal sweep phase to point the beam in elevation to receive signals at a near range edge at a start of the sweep, and at a far range edge at an end of the sweep.

6. A system for a satellite, the system comprising:

a core system comprising;

control means for generating transmit signals;

transceiver means for wirelessly transmitting the transmit signal, and for wirelessly receiving a receive signal;

multiple node means for generating an active phased array, wherein each node means comprises;

node transceiver means for wirelessly receiving the transmit signal, for wirelessly transmitting the transmit signals to a target, for wirelessly receiving the receive signals from the target, and for wirelessly transmitting the receive signal to the core system,

means for inhibiting signal interference between the transmit and receive signals; and

node control means, coupled with the transceiver means and the means for inhibiting signal interference, for controlling or processing the transmit and receive signals.

7. The system of claim 6, further comprising:

at each node means, power generation means for generating power, and,

wherein the node control means includes means for facilitating beam formation and beam steering based at least in part on the transmit signal.

8. The system of claim 6, further comprising:

oscillator means, coupled to the control means, for generating a stable reference frequency signal, and

wherein the transceiver means includes means for transmitting the reference frequency signal to the node means.

9. The system of claim 6, further comprising:

wing means for carrying some of the multiple nodes; and

compensation means, coupled to the control means, for determining a distortion of the wing means, and for generating at least one compensation signal based on the determined distortion.

10. A computer-readable medium whose contents cause at least one satellite to perform a method, the method comprising:

receiving a reference frequency signal;

generating transmit signals, based at least in part on the reference frequency signal, to form a transmit beam wirelessly directed at a target;

at each of multiple antenna nodes, wirelessly receiving a receive signal from the target;

at each of multiple antenna nodes, wirelessly transmitting the receive signal to another portion of the satellite; and

at each of multiple antenna nodes, controlling or processing the transmit and receive signals to inhibit signal interference between the transmit and receive signals.

11. The computer-readable medium of claim 10 wherein the computer-readable medium is a memory of a server or a removable memory.

12. The computer-readable medium of claim 10 wherein the computer-readable medium is a logical node in a computer network receiving the contents, or a data transmission medium carrying a generated data signal containing the contents.

13. The computer-readable medium of claim 10 wherein the computer-readable medium is a computer-readable disk.

14. The computer-readable medium of claim 10 wherein the method further comprises, at each of multiple antenna nodes, locally generating power.

15. The computer-readable medium of claim 10 wherein the method further comprises, at each of multiple antenna nodes, facilitating beam formation and beam steering based at least in part on the reference frequency signal.

16. In an active lens radar system having at least one wing, an apparatus comprising:

multiple nodes carried by the wing, wherein each node comprises;

a transmit portion configured to wirelessly receive a space fed signal from the radar system and to generate a transmit signal to be wirelessly directed to a target as part of a transmit beam;

a receive portion configured to wirelessly receive an echo signal from the target and to generate a receive signal to be wirelessly transmitted to the radar system;

a signal isolation portion, coupled to at least one of the transmit and receive portions, and configured to inhibit signal interference between the transmit signal and the receive signal; and

a controller coupled among the transmit, receive and signal isolation portions.

17. The apparatus of claim 16, further comprising local power generation for providing power to the controller and to the transmit, receive and signal isolation portions.

18. The apparatus of claim 16, further comprising a wired connection between the controller and a central control system of the radar system.

19. The apparatus of claim 16, further comprising:

a frequency adjuster for adjusting a received reference signal and to produce a frequency adjusted signal,

a modulator for producing a modulated signal based on the frequency adjusted signal,

transmit and receive paths, each having a mixer for mixing in the modulated signal, and

a signal selector for selectively providing the modulated signal to the transmit and receive paths.

20. The apparatus of claim 16 wherein a rear portion of the wing carries the multiple nodes, and wherein a front portion of the wing is configured to transmit at least a portion of the transmit beam and receive at least a portion of the echo signal.

21. The apparatus of claim 16 wherein the signal isolation portion is configured to inhibit signal interference between the transmit signal and the receive signal via frequency translation, electromagnetic shielding, use of different signal polarizations, use of digital signal processing techniques, use of differently coded spread spectrum channels, or use of time domain multiplexing.

22. In an active lens radar system having at least one wing, an apparatus comprising:

multiple nodes carried by the wing, wherein each node comprises;

a signal processing portion configured to at least assist in directing a transmit signal to a target as part of a transmit beam, and to receive an echo signal from the target;

a controller coupled to the signal processing portion; and

,

local power generation circuitry configured to locally provide power to the controller and to the signal processing portion, without use of power distribution wiring from the radar system to the multiple nodes.

23. The apparatus of claim 22 wherein the local power generation circuitry includes a solar cell array, a rechargeable battery, and a battery charge regulator coupled between the solar cell array and the battery.