US-12627050-B2 - System and method for a digitally beamformed phased array feed

US12627050B2US 12627050 B2US12627050 B2US 12627050B2US-12627050-B2

Abstract

Systems and methods are provided for a digital beamformed phased array feed. The system may include a radome configured to allow electromagnetic waves to propagate; a multi-band software defined antenna array tile; a power and clock management subsystem configured to manage power and time of operation; a thermal management subsystem configured to dissipate heat generated by the multi-band software defined antenna array tile; and an enclosure assembly. The multi-band software defined antenna array tile may include a plurality of coupled dipole array antenna elements; a plurality of frequency converters; and a plurality of digital beamformers.

Inventors

Michael Thomas Pace
David Gregory Baur
Theodore Lyman Schuler-Sandy
William Kennedy
Jeffrey Gerard Micono
William Louis Walker
Garrett James Newell

Assignees

BLUEHALO, LLC

Dates

Publication Date: 20260512
Application Date: 20240828

Claims (16)

1 . A method comprising: (a) receiving, from a digital software system interface via a system controller by memory of a multi-band software defined antenna array tile, for a respective coupled dipole antenna array element of a plurality of respective coupled dipole antenna array elements of the multi-band software defined antenna array tile: i. a respective mission center radio frequency; ii. a respective mission intermediate frequency; wherein each coupled dipole array antenna element of the plurality of respective coupled dipole antenna array elements includes a respective principal polarization component oriented in a first direction and a respective orthogonal polarization component oriented in a second direction; (b) receiving, from the digital software system interface via the system controller by the memory of the multi-band software defined antenna array tile, for a respective principal polarization component and a respective orthogonal polarization component of the respective coupled dipole antenna array element of the plurality of respective coupled dipole antenna array elements: i. a respective channel selection; ii. a respective weighting factor as part of an array of weighting factors; iii. a respective oscillating signal frequency; (c) storing, by the memory operatively connected to the system controller: i. the respective mission center radio frequency for the respective coupled dipole antenna array element; ii. the respective mission intermediate frequency for the respective coupled dipole antenna array element; iii. the respective channel selection for the respective principal polarization component and the respective orthogonal polarization component of the respective coupled dipole antenna array element; iv. each respective weighting factor of the array of weighting factors for the respective principal polarization component and the respective orthogonal polarization component of the respective coupled dipole antenna array element of the plurality of respective coupled dipole antenna array elements; and v. the respective oscillating signal frequency for the respective principal polarization component and the respective orthogonal polarization component of the respective coupled dipole antenna array element; (d) transporting, from the memory to a respective principal polarization frequency converter and a respective orthogonal polarization frequency converter: i. the respective mission center radio frequency for the respective coupled dipole antenna array element; ii. the respective mission intermediate frequency for the respective coupled dipole antenna array element; wherein the respective principal polarization frequency converter and the respective orthogonal polarization frequency converter are a part of a respective pair of frequency converters of a plurality of pairs of frequency converters of the multi-band software defined antenna array tile, wherein each pair of frequency converters of the plurality of pairs of frequency converters is operatively connected to a respective coupled dipole antenna array element, and wherein each pair of frequency converters of the plurality of pairs of frequency converters comprises the respective principal polarization frequency converter corresponding to a respective principal polarization component and the respective orthogonal polarization frequency converter corresponding to a respective orthogonal polarization component; (e) transporting, from the memory to a respective digital beamformer of a plurality of digital beamformers: i. the respective channel selection for the respective principal polarization component and the respective orthogonal polarization component of the respective coupled dipole antenna array element; ii. each respective weighting factor of the array of weighting factors for the respective principal polarization component and the respective orthogonal polarization component of the respective coupled dipole antenna array element of the plurality of respective coupled dipole antenna array elements; iii. the respective oscillating signal frequency for the respective principal polarization component and the respective orthogonal polarization component of the respective coupled dipole antenna array element, wherein each digital beamformer is operatively connected to one of the respective principal polarization frequency converter and the respective orthogonal polarization frequency converter; (f) receiving, by a first digital beamformer of the plurality of digital beamformers of the multi-band software defined antenna array tile, a first partial beam of a first beam of a plurality of beams from a digital software system interface via a data transport bus; (g) applying, by the first digital beamformer, a first weighting factor to first transmit digital data associated with the first partial beam of the first beam of the plurality of beams; (h) transmitting, by the first digital beamformer, the first transmit digital data to a first digital to analog converter; (i) converting, using the first digital to analog converter, the first transmit digital data from a digital signal to an analog signal having a first intermediate frequency, wherein the first intermediate frequency is associated with the respective mission intermediate frequency; (j) receiving, by a first principal polarization frequency converter of a first pair of frequency converters of the plurality of pairs of frequency converters of the multi-band software defined antenna array tile, respective first modulated signals associated with the first intermediate frequency from the first digital beamformer of the plurality of digital beamformers, (k) converting, by the first principal polarization frequency converter of the first pair of frequency converters, the respective first modulated signals associated with the first intermediate frequency into respective second modulated signals associated with a respective radio frequency, wherein the respective radio frequency is associated with the respective mission center radio frequency; (l) transmitting, from the first principal polarization frequency converter of the first pair of frequency converters, the respective second modulated signals associated with the respective radio frequency to a first coupled dipole array antenna element of the plurality of respective coupled dipole antenna array elements; and (m) transmitting, by the first coupled dipole array antenna element, the respective second modulated signals associated with the respective radio frequency.
2 . The method of claim 1 , wherein the plurality of respective coupled dipole antenna array elements are tightly coupled relative to a wavelength of operation.
3 . The method of claim 1 , wherein the plurality of respective coupled dipole antenna array elements are spaced at less than half a wavelength.
4 . The method of claim 1 , wherein the plurality of pairs of frequency converters further comprise thermoelectric coolers configured to actively manage thermally a system noise temperature and increase a system gain over temperature.
5 . The method of claim 4 , wherein the plurality of pairs of frequency converters further comprise a plurality of spatially distributed high power amplifiers so as to increase an effective isotropic radiated power.
6 . The method of claim 1 , wherein the first intermediate frequency is between 50 MHz and 1250 MHz.
7 . The method of claim 6 , wherein the respective radio frequency is between 900 MHz and 6000 MHz.
8 . The method of claim 6 , wherein the respective radio frequency is between 2000 MHz and 12000 MHz.
9 . The method of claim 6 , wherein the respective radio frequency is between 10000 MHZ and 50000 MHz.
10 . The method of claim 1 , wherein the method further comprises selecting, by the first digital beamformer, a first channel of a first plurality of channels using a first multiplexer.
11 . The method of claim 1 , wherein the digital software system interface generates the array of weighting factors by using the formula: w m , n = ( A m , n tap * A m , n cal ) ︷ A m , n * e - j * ( θ m , n steer + θ m , n tap + θ m , n cal ) ︷ θ m , n wherein w m,n is the respective weighting factor associated with each position in an antenna array comprised of the plurality of respective coupled dipole antenna array elements expressed as a horizontal position m and a vertical position n, A m,n is an amplitude weighting factor associated with each position in the antenna array expressed as a horizontal position m and a vertical position n, A tap is a tapered amplitude weighting factor associated with each position in the antenna array expressed as a horizontal position m and a vertical position n, A cal is a calibration weighting factor associated with each position in the antenna array expressed as a horizontal position m and a vertical position n, θ m,n is a phase factor associated with each position in the antenna array expressed as a horizontal position m and a vertical position n, θ steer is a steering phase factor associated with each position in the antenna array expressed as a horizontal position m and a vertical position n, θ top is a taper phase factor associated with each position in the antenna array expressed as a horizontal position m and a vertical position n, and θ cal is a calibration phase factor associated with each position in the antenna array expressed as a horizontal position m and a vertical position n.
12 . The method of claim 11 , wherein the digital software system interface generates the respective weighting factor by using the formula: w ⁡ ( t ) = ( cosh ⁡ ( πα * 1 - 4 ⁢ t 2 ) cosh ⁡ ( πα ) ) P wherein w(t) is the respective weighting factor at a location t, where t is defined by an array associated with a location of the respective principal polarization component and the respective orthogonal polarization component of the respective coupled dipole antenna array element, α is a respective tuning parameter, and P is a respective power parameter.
13 . The method of claim 12 , wherein the digital software system interface receives specific mission parameters for the plurality of respective coupled dipole antenna array elements as an input, and wherein the digital software system interface uses the specific mission parameters to generate the array of weighting factors.
14 . The method of claim 13 , wherein the respective weighting factor is selected from the array of weighting factors.
15 . The method of claim 11 , wherein a plurality of oscillating signal frequencies may be received for a plurality of principal polarization components and a plurality of orthogonal polarization components of the plurality of respective coupled dipole antenna array elements.
16 . The method of claim 12 , wherein the digital software system interface receives specific mission parameters for respective coupled dipole antenna array elements as an input, and wherein the digital software system interface uses the specific mission parameters to generate the respective oscillating signal frequency.

Description

RELATED APPLICATIONS This application is a continuation of U.S. patent application Ser. No. 18/378,045, filed on Oct. 9, 2023, and entitled “SYSTEM AND METHOD FOR A DIGITALLY BEAMFORMED PHASED ARRAY FEED, which is a continuation of U.S. patent application Ser. No. 18/104,630, filed Feb. 1, 2023, and entitled “SYSTEM AND METHOD FOR A DIGITALLY BEAMFORMED PHASED ARRAY FEED, which is a continuation of U.S. patent application Ser. No. 17/690,852, filed on Mar. 9, 2022, and entitled “SYSTEM AND METHOD FOR A DIGITALLY BEAMFORMED PHASED ARRAY FEED”, which is a continuation of U.S. patent application Ser. No. 17/679,817, filed on Feb. 24, 2022, and entitled “SYSTEM AND METHOD FOR A DIGITALLY BEAMFORMED PHASED ARRAY FEED”, which claims the benefit and priority to U.S. Provisional Patent Application No. 63/200,260, filed on Feb. 24, 2021, and entitled “SYSTEM AND METHOD FOR A DIGITALLY BEAMFORMED PHASED ARRAY FEED”, the entire contents of which are incorporated by reference herein. U.S. patent application Ser. No. 17/679,817, filed on Feb. 24, 2022, and entitled “SYSTEM AND METHOD FOR A DIGITALLY BEAMFORMED PHASED ARRAY FEED” also claims the benefit and priority to U.S. Provisional Patent Application No. 63/188,959, filed on May 14, 2021, and entitled “SYSTEM AND METHOD FOR A DIGITALLY BEAMFORMED PHASED ARRAY FEED”, the entire contents of which are incorporated by reference herein. U.S. patent application Ser. No. 17/679,817 also claims the benefit and priority to U.S. Provisional Patent Application No. 63/262,124, filed on Oct. 5, 2021, and entitled “SYSTEM AND METHOD FOR A DIGITALLY BEAMFORMED PHASED ARRAY FEED”, the entire contents of which are incorporated by reference herein. FIELD OF THE INVENTION The present invention generally relates to systems and methods for a digitally beamformed phased array feed. In embodiments, the digitally beamformed phased array feed may be used in conjunction with a parabolic reflector. In embodiments, the present invention generally relates to systems and methods for a large form-factor phased array utilizing a plurality of multi-band software defined antenna array tiles. BACKGROUND Satellite communications are made between communications satellites and parabolic reflector antennas of ground stations on Earth. Most traditional satellite communications require satellites to maintain geostationary orbit 22,236 miles above the equator so that the parabolic reflector antennas can be aimed permanently at that spot and the parabolic surfaces and/or reflectors do not have to move in order to track the flight object. In this existing system, wherever the parabolic reflector antenna is mechanically pointing is where the antenna beam is pointing and therefore the target flight object must be located within the beam in order for the antenna to track or communicate with the object. The current state of satellite communication has a number of problems. For example, existing parabolic reflector antennas are fitted for single band signals and because of traditional beamforming techniques, a parabolic reflector antenna may only communicate with one flight object at a time. The existing state of the art is a static technology, where one antenna is designed specifically for one reflector. Further, the application of existing satellite antennas fixed to moving objects such as ships and fast-moving aircraft remains difficult due to the significant design challenges involved in stabilizing the reflector such that the antenna beam remains fixed on the desired target. It would therefore be beneficial to implement a digital beamforming technique which includes digital sampling and processing of antenna element data to steer the direction of the antenna beam to allow for simultaneous tracking of multiple flight objects with a single antenna array. It would be further beneficial to permit rapid configuration and multi-band operations from a single antenna array. SUMMARY In view of the above, it is the object of the present disclosure to provide a technological solution to address the long felt need and technological challenges faced in conventional satellite communication systems in which traditional antennas are designed for receiving and transmitting single band signals to and from one flight object at time. The present disclosure provides for a system of a digitally beamformed phased array feed that allows for receiving and transmitting signals within multiple bandwidths for multiple flight objects simultaneously. In embodiments, a method for digital beamforming may include: (a) receiving, by a first coupled dipole array antenna element of a plurality coupled dipole array antenna elements of a multi-band software defined antenna array tile, a plurality of respective modulated signals associated with a plurality of respective radio frequencies, wherein each coupled dipole array antenna element of the plurality of coupled dipole array antenna elements includes a respective principal polarization component