IP Library Patent Application 19068646
Patent Application
App. No. 19/068,646

TILTED EARTH-BASED ANTENNA SYSTEMS AND METHODS OF TILTING FOR COMMUNICATION WITH A SATELLITE SYSTEM

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Quick Facts
Patent No.
US None
App. No.
19/068,646
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.

Claims (14)

1 . A method of communicating with a non-GEO satellite constellation, the method comprising:

positioning a satellite of the non-GEO satellite constellation to travel along a first orbital path at a first, non-zero-degree inclination, wherein the first orbital path has a reduced overlap with the GEO-belt interference zone as compared to a satellite traveling along a second orbital path at a zero-degree inclination;

selecting an orientation for an endpoint terminal configured for communicating with the satellite, wherein the endpoint terminal includes a housing and an electronically steered phased array antenna system disposed within the housing, wherein the electronically steered phased array antenna system defines a field of regard for a single steerable beam for communication with the non-GEO satellite constellation including the satellite, wherein the field of regard is a limited field of regard having a first end and a second end, and wherein the orientation tilts the housing relative to a horizontal plane and directs the field of regard towards the satellite traveling along the first orbital path;

positioning the endpoint terminal to the selected orientation such that the endpoint terminal can communicate with the satellite.

2 . The method of claim 1 , wherein the satellite constellation includes a plurality of satellites in low Earth orbit (LEO).

3 . The method of claim 1 , wherein the endpoint terminal includes a tilting mechanism configured to adjust the positioning of the endpoint terminal.

4 . The method of claim 1 , wherein positioning the endpoint terminal to the selected orientation includes tilting the endpoint terminal from a first position to a second position.

5 . A method of communicating with a non-GEO satellite constellation, the method comprising:

selecting an orientation for an endpoint terminal configured for communicating with a satellite of the non-GEO satellite constellation, wherein the endpoint terminal includes a housing and an electronically steered phased array antenna system disposed within the housing, wherein the electronically steered phased array antenna system defines an aperture and a field of regard for a single steerable beam for communication with the non-GEO satellite constellation including the satellite, wherein the field of regard is a limited field of regard having a first end and a second end, wherein the orientation directs the field of regard towards the satellite, and wherein the orientation tilts the housing relative to a horizontal plane;

positioning the endpoint terminal to the selected orientation such that the endpoint terminal can communicate with the satellite.

6 . The method of claim 5 , further comprising positioning the satellite of the non-GEO satellite constellation to travel along a first orbital path at a first, non-zero-degree inclination, wherein the first orbital path has a reduced overlap with the GEO-belt interference zone as compared to a satellite traveling along a second orbital path at a zero-degree inclination.

7 . The method of claim 5 , wherein the satellite constellation includes a plurality of satellites in low Earth orbit (LEO).

8 . The method of claim 5 , wherein the endpoint terminal includes a tilting mechanism configured to adjust the positioning of the endpoint terminal.

9 . The method of claim 5 , wherein positioning the endpoint terminal to the selected orientation includes tilting the endpoint terminal from a first position to a second position.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 3, 2025
From: MILROY, DAVID; ADAMS, DUNCAN E.; JOHNSON, JESSICA D.; HERMAN, JONATHAN FRANÇOIS CORNELIS
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 070389/0096 →