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1.发明申请公开(公告)号：US20200382206A1
公开(公告)日：2020-12-03
申请号：US16892223
申请日：2020-06-03
Applicant: Space Exploration Technologies Corp.
IPC: H04B7/185
Abstract: In one embodiment of the present disclosure, a satellite communication system includes a satellite constellation including a plurality of satellites in non-geosynchronous orbit (non-GEO), wherein at least some of the plurality of satellites travel in a first orbital path at a first inclination, and an end point terminal having an earth-based geographic location, the end point terminal having an antenna system defining a field of regard for communicating with the satellite constellation, wherein the field of regard is a limited field of regard, wherein the field of regard is tilted from a non-tilted position to a tilted position, and wherein the tilt angle of the tilted position is a function of the latitude of the geographic location.
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Patent Agency Ranking
2.发明公开公开(公告)号：US20240187089A1
公开(公告)日：2024-06-06
申请号：US18437044
申请日：2024-02-08
Applicant: Space Exploration Technologies Corp.
IPC: H04B7/185
CPC classification number: H04B7/18519 , H04B7/18517 , H04B7/18536 , H04B7/18547 , H04B7/18571 , H04B7/18573
Abstract: In one embodiment of the present disclosure, a satellite communication system includes a satellite constellation including a plurality of satellites in non-geosynchronous orbit (non-GEO), wherein at least some of the plurality of satellites travel in a first orbital path at a first inclination, and an end point terminal having an earth-based geographic location, the end point terminal having an antenna system defining a field of regard for communicating with the satellite constellation, wherein the field of regard is a limited field of regard, wherein the field of regard is tilted from a non-tilted position to a tilted position, and wherein the tilt angle of the tilted position is a function of the latitude of the geographic location.
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3.发明授权公开(公告)号：US12244399B2
公开(公告)日：2025-03-04
申请号：US18437044
申请日：2024-02-08
Applicant: Space Exploration Technologies Corp.
IPC: H04B7/185
Abstract: In one embodiment of the present disclosure, a satellite communication system includes a satellite constellation including a plurality of satellites in non-geosynchronous orbit (non-GEO), wherein at least some of the plurality of satellites travel in a first orbital path at a first inclination, and an end point terminal having an earth-based geographic location, the end point terminal having an antenna system defining a field of regard for communicating with the satellite constellation, wherein the field of regard is a limited field of regard, wherein the field of regard is tilted from a non-tilted position to a tilted position, and wherein the tilt angle of the tilted position is a function of the latitude of the geographic location.
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4.发明授权公开(公告)号：US11611392B2
公开(公告)日：2023-03-21
申请号：US16892223
申请日：2020-06-03
Applicant: Space Exploration Technologies Corp.
IPC: H04B7/185
Abstract: In one embodiment of the present disclosure, a satellite communication system includes a satellite constellation including a plurality of satellites in non-geosynchronous orbit (non-GEO), wherein at least some of the plurality of satellites travel in a first orbital path at a first inclination, and an end point terminal having an earth-based geographic location, the end point terminal having an antenna system defining a field of regard for communicating with the satellite constellation, wherein the field of regard is a limited field of regard, wherein the field of regard is tilted from a non-tilted position to a tilted position, and wherein the tilt angle of the tilted position is a function of the latitude of the geographic location.
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5.发明授权公开(公告)号：US11909506B2
公开(公告)日：2024-02-20
申请号：US18123879
申请日：2023-03-20
Applicant: Space Exploration Technologies Corp.
IPC: H04B7/185
CPC classification number: H04B7/18519 , H04B7/18517 , H04B7/18536 , H04B7/18547 , H04B7/18571 , H04B7/18573
Abstract: In one embodiment of the present disclosure, a satellite communication system includes a satellite constellation including a plurality of satellites in non-geosynchronous orbit (non-GEO), wherein at least some of the plurality of satellites travel in a first orbital path at a first inclination, and an end point terminal having an earth-based geographic location, the end point terminal having an antenna system defining a field of regard for communicating with the satellite constellation, wherein the field of regard is a limited field of regard, wherein the field of regard is tilted from a non-tilted position to a tilted position, and wherein the tilt angle of the tilted position is a function of the latitude of the geographic location.
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6.发明公开公开(公告)号：US20230246708A1
公开(公告)日：2023-08-03
申请号：US18123879
申请日：2023-03-20
Applicant: Space Exploration Technologies Corp.
IPC: H04B7/185
CPC classification number: H04B7/18519 , H04B7/18517 , H04B7/18571 , H04B7/18547 , H04B7/18573 , H04B7/18536
Abstract: In one embodiment of the present disclosure, a satellite communication system includes a satellite constellation including a plurality of satellites in non-geosynchronous orbit (non-GEO), wherein at least some of the plurality of satellites travel in a first orbital path at a first inclination, and an end point terminal having an earth-based geographic location, the end point terminal having an antenna system defining a field of regard for communicating with the satellite constellation, wherein the field of regard is a limited field of regard, wherein the field of regard is tilted from a non-tilted position to a tilted position, and wherein the tilt angle of the tilted position is a function of the latitude of the geographic location.
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