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公开(公告)号:US20250126011A1
公开(公告)日:2025-04-17
申请号:US19000388
申请日:2024-12-23
Applicant: Space Exploration Technologies Corp.
Inventor: Martin S. McCormick , Feipeng Wang
Abstract: A wireless communications system includes a pre-distortion actuator configured to receive a carrier-modulated signal and convert the carrier-modulated signal into an output signal, the pre-distortion actuator comprising a behavioral model that models a transmit chain of the system including at least one antenna and predict an input-output relationship of the transmit chain of the system between an input to the transmit chain to an output of the transmit chain. The system includes a phased antenna array configured to transmit the output signal. The phased antenna array includes a plurality of antenna elements. The pre-distortion actuator is configured to generate the output signal by applying a correction to the carrier-modulated input signal that cancels out nonlinearities The behavioral model is updated based on feedback from a receiver from a previous output signal transmitted to the receiver.
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公开(公告)号:US20250125905A1
公开(公告)日:2025-04-17
申请号:US19000441
申请日:2024-12-23
Applicant: Space Exploration Technologies Corp.
Inventor: Jeffrey A. Gardner , Yashodhan Dandekar , Ramakrishna Akella , Khasim Shaheed Shaik Mahammad
Abstract: Systems, methods, and techniques are provided for a radio link control (RLC) sublayer. An example satellite or user terminal can include a divisional of layer 2 of the OSI protocol layer structure. An example method includes providing a RLC sublayer on top of a MAC sublayer and adaptively switching, via the RLC sublayer and based on external data, between an unacknowledged mode and an acknowledged mode for the electronic communications. If the RLC sublayer is operating in the unacknowledged mode, the RLC sublayer provides one or more of (1) fragmentation and reassembly of service data units; (2) a use of RLC headers; and/or (3) no delivery guarantees. If the RLC sublayer is operating in the acknowledged mode, the RLC sublayer provides reliability in a sequence delivery service and one or more of (1) fragmentation and reassembly of service data units; and/or (2) the use of RLC headers.
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公开(公告)号:USD1061486S1
公开(公告)日:2025-02-11
申请号:US29851272
申请日:2022-08-26
Applicant: Space Exploration Technologies Corp.
Designer: Jackson Shaffner , Anthony Sims , Michael J. Conte , Victor Q. Dang , David Milroy , Duncan Edwin Adams
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公开(公告)号:US20250019395A1
公开(公告)日:2025-01-16
申请号:US18900240
申请日:2024-09-27
Applicant: Space Exploration Technologies Corp.
Inventor: Eric Pepin , Kim W. Schulze , Amir Agah , Dean A. De Carli , Philippe Riondet
IPC: C07K1/36
Abstract: Systems, methods, and computer-readable media are provided for hybrid beamforming. An example method can include determining a plurality of digital beamforming weights associated with a plurality of digital beamforming paths between digital beamformers and groups of analog beamforming circuits in a phased array antenna, each digital beamforming path being coupled to a group of analog beamforming circuits and each analog beamforming circuit being coupled to a respective set of antenna elements of the phased array antenna, and determining analog beamforming weights associated with the groups of analog beamforming circuits. The analog beamforming weights are estimated to put analog beamforming paths associated with the groups of analog beamforming circuits in a desired phase and gain relationship with each other. The method can include varying, based at least partly on the analog beamforming weights, a signal phase shift across the analog beamforming paths associated with the groups of analog beamforming circuits.
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公开(公告)号:US12166282B2
公开(公告)日:2024-12-10
申请号:US18216415
申请日:2023-06-29
Applicant: Space Exploration Technologies Corp.
Inventor: Javier Rodriguez De Luis , Nil Apaydin , Ersin Yetisir , Alireza Mahanfar , Siamak Ebadi
Abstract: An apparatus includes a plurality of conductive structures having first sides and second sides opposite the first sides, wherein the second sides of the plurality of conductive structures are configured to be physically coupleable with a printed circuit board (PCB) of a receiver, a transmitter, or a transceiver. The first sides of the plurality of conductive structures are configured to be spaced from the PCB by a first distance when the plurality of conductive structures is physically coupled with the PCB. The apparatus includes an antenna having a first side and a second side opposite the first side. The second side of the antenna is disposed closer to the plurality of conductive structures than the first side of the antenna when the plurality of conductive structures is physically coupled with the PCB.
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公开(公告)号:US12088398B1
公开(公告)日:2024-09-10
申请号:US17186627
申请日:2021-02-26
Applicant: Space Exploration Technologies Corp.
Inventor: Martin S. McCormick , Torbjorn Larsson , Alazar Tamrat , Jeffrey C. Strait , Chen Chen , Philip J. Treigherman , Stephan O. Roche , Ronald Gottula
CPC classification number: H04B7/18513 , H04B7/18517 , H04L5/001 , H04L25/0202 , H04L27/0014 , H04L27/2636 , H04L2027/0026
Abstract: A modem is configurable on a satellite, user terminal or gateway generates a radio frequency (RF) signal using an orthogonal frequency division multiplexing (OFDM) protocol including a radio frame including one or more bursts. A burst of the one or more bursts includes a first portion including burst detection data, a second portion including channel characteristic estimation data, a third portion including payload data, and fourth and fifth portions including pilot data. The first portion in a time domain is included in the burst prior to the second, third, fourth, and fifth portions. The first portion can include a pseudo-random noise sequence inserted in the time domain. The same physical modem can be configured to transmit signals on an uplink or downlink between a user terminal and a satellite or on the uplink or downlink between the satellite and the gateway.
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公开(公告)号:US12074683B1
公开(公告)日:2024-08-27
申请号:US17186706
申请日:2021-02-26
Applicant: Space Exploration Technologies Corp.
Inventor: Martin S. McCormick , Torbjorn Larsson , Alazar Tamrat , Jeffrey C. Strait , Chen Chen , Philip J. Treigherman , Stephan O. Roche , Ronald Gottula
IPC: H04B7/185 , H04L5/00 , H04W72/0453
CPC classification number: H04B7/18513 , H04L5/0048 , H04W72/0453
Abstract: A modem is configurable on a satellite, user terminal or gateway generates a radio frequency (RF) signal using an orthogonal frequency division multiplexing (OFDM) protocol including a radio frame including one or more bursts. A burst of the one or more bursts includes a first portion including burst detection data, a second portion including channel characteristic estimation data, a third portion including payload data, and fourth and fifth portions including pilot data. The first portion in a time domain is included in the burst prior to the second, third, fourth, and fifth portions. The first portion can include a pseudo-random noise sequence inserted in the time domain. The same physical modem can be configured to transmit signals on an uplink or downlink between a user terminal and a satellite or on the uplink or downlink between the satellite and the gateway.
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公开(公告)号:US20240213652A1
公开(公告)日:2024-06-27
申请号:US18435899
申请日:2024-02-07
Applicant: Space Exploration Technologies Corp.
Inventor: Erik N. Littleton , Duncan Edwin Adams
CPC classification number: H01Q1/125 , F16M11/126 , F16M11/18 , H01Q3/08
Abstract: In one embodiment of the present disclosure, a pan/tilt assembly for an antenna apparatus having a housing enclosing antenna components and a leg extending from the housing includes a first actuator for rotating a first gear, a second actuator for rotating a second gear, a third gear coupled to the leg and engaged by the first and second gears, and a tee having a first portion substantially transverse to a second portion, wherein the first portion has a first end rotatably received within the first gear and a second end rotatably received within the second gear, and wherein the second portion is rotatably received within the third gear.
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公开(公告)号:US11924821B1
公开(公告)日:2024-03-05
申请号:US17339860
申请日:2021-06-04
Applicant: Space Exploration Technologies Corp.
Inventor: Peter J. Worters , Martin S. McCormick , Andrew G. Whitlow
IPC: H04W72/121 , H04B7/185 , H04L5/16 , H04W56/00 , H04W72/1273
CPC classification number: H04W72/121 , H04B7/18513 , H04L5/16 , H04W56/0045 , H04W56/0055 , H04W72/1273
Abstract: Systems, methods, and non-transitory media are provided for timing half-duplex transmissions in a wireless communication system. An example method can include receiving, by a user terminal (UT), a radio frame transmitted by a satellite to a group of UTs; identifying an offset delay defined in the radio frame for scheduling transmissions between the satellite and each UT in the group of UTs, the offset delay providing non-overlapping time intervals for receive, process, and transmit operations at each UT; determining, based on the offset delay and a time when the radio frame was received by the UT, a time for transmitting an uplink radio burst to the satellite, wherein the uplink radio burst transmitted at the time is estimated to arrive at the satellite within a same radio frame interval as uplink radio bursts from other UTs; and transmitting, to the satellite, the uplink radio burst at the time.
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公开(公告)号:US20240040601A1
公开(公告)日:2024-02-01
申请号:US18486035
申请日:2023-10-12
Applicant: Space Exploration Technologies Corp.
Inventor: Jayasuryan V. Iyer , Yashodhan Dandekar , Khasim Shaheed Shaik Mahammad , Ramakrishna Akella , Chen Chen , Phillip E. Barber , Peter J. Worters
IPC: H04W72/54 , H04B17/382 , H04B17/336 , H04L1/00 , H04W72/21
CPC classification number: H04W72/54 , H04B17/382 , H04B17/336 , H04L1/0009 , H04L1/0003 , H04W72/21
Abstract: A method for downlink link adaptation includes receiving, from a satellite and at a user terminal, a first data packet data unit according to a first downlink modulation and coding scheme (MCS), computing error vector magnitude data associated with the first data packet data unit, generating, based on one or more of the error vector magnitude data, user terminal signal-to-noise-ratio feedback based on a constant times a previous user terminal signal-to-noise-ratio and a current user terminal signal-to-noise-ratio, and transmitting an uplink packet data unit having a downlink block error rate and the user terminal signal-to-noise-ratio feedback. A satellite runs a link adaptation algorithm based on the user terminal signal-to-noise-ratio feedback and block error rate to generate a second downlink MCS. The method includes receiving at the user terminal a second data packet data unit according to the second downlink MCS for the satellite-to-user-terminal downlink. Uplink link adaptation is also disclosed.
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