IP Library Granted Patent US 12,489,519
Granted Patent B2
US 12,489,519 · App. 18/012,163 · Granted Dec 2, 2025

Methods for the transmission of data between a resource constrained device and a non-geostationary satellite and associated system

Inventors: Antonin Hirsch (Issy-les-Moulineaux, FR); Geoffroy Brichler (Issy-les-Moulineaux, FR); Florian Collard (Issy-les-Moulineaux, FR)
Assignee: EUTELSAT SA
H04B7/18513H04B7/195
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Quick Facts
Patent No.
US 12,489,519
App. No.
18/012,163
Granted
Dec 2, 2025
Kind
B2
Abstract

A method for the transmission to a non-geostationary satellite of data stored by a ground-based device being carried out by the device, includes entering an awaken mode, performing successive Doppler shift estimations: receiving, by the device during the awaken mode, a signal from the satellite including a frequency parameter and an elevation emission criterion, performing a Doppler shift estimation based on the frequency of the received signal; estimating a Doppler rate of frequency change to obtain a relative position of the device, defining a transmission window during which the position of the device relative to position of the satellite verifies the elevation emission criterion, and if the position of the device relative to the position of the satellite verifies the elevation emission criterion: emitting at the frequency parameter a signal including the data stored by the device.

Claims (32)

1 . A method for the transmission to at least one non-geostationary satellite of at least one piece of data stored by a ground-based device, the method being carried out by the ground-based device and comprising:

entering an awaken mode,

performing successive Doppler shift estimations, a Doppler shift estimation of the Doppler shift estimations comprising:

receiving, by the ground-based device during the awaken mode, at least one signal from the non-geostationary satellite, the signal comprising at least one frequency parameter of the current reception frequency used by the non-geostationary satellite and at least one elevation emission criterion,

performing a Doppler shift estimation based on the frequency of the received signal;

estimating a Doppler rate of frequency change to obtain a position of the ground-based device relative to the position of the non-geostationary satellite, the estimation being carried out by using an estimation method on a plurality of computed Doppler rates of frequency change, the computing of a Doppler rate of frequency change comprising deriving the Doppler shift estimations,

defining a transmission window, the transmission window being a period of time during which the position of the ground-based device relative to position of the non-geostationary satellite verifies the elevation emission criterion,

when, at a transmission time comprised in the transmission window, the position of the ground-based device relative to the position of the non-geostationary satellite verifies the elevation emission criterion:

emitting, at the transmission time and at the current reception frequency, at least one signal comprising at least the piece of data stored by the ground-based device.

2 . The method according to claim 1 , wherein the at least one signal emitted by the ground-based device comprises the position of the ground-based device relative to the position of the non-geostationary satellite.

3 . The method according to claim 1 , wherein the received signal from the non-geostationary satellite further comprises at least one information of the current altitude of the non-geostationary satellite at the time of emission of the signal and wherein the current altitude information is used in the defining of a transmission window to define an adjusted transmission window.

4 . The method according to claim 1 , wherein entering an awaken-mode is carried out during a reduced time window, the reduced time window being computed by computing orbital period of the non-geostationary satellite using previous received signals from the non-geostationary satellite.

5 . The method according to claim 4 , wherein the orbital period of the non-geostationary satellite is computed using a peak-to-peak algorithm.

6 . The method according to claim 2 , wherein the received signal from the non-geostationary satellite further comprises at least one information of the current altitude of the non-geostationary satellite at the time of emission of the signal and wherein the current altitude information is used in the defining of a transmission window to define an adjusted transmission window, and wherein the computing orbital period of the non-geostationary satellite further uses the current altitude information comprised in the received signal.

7 . The method according to claim 1 , wherein the elevation emission criterion is an information of the current beam size of the non-geostationary satellite or an elevation emission threshold.

8 . The method according to claim 1 , wherein the ground-based device is in an occulted environment and the emitting is only carried out if the ground-based device receives another signal from the non-geostationary satellite during a time period before the transmission time.

9 . A method for the transmission to at least one non-geostationary satellite of at least one piece of data stored by a ground-based device, the method being carried out by the non-geostationary satellite and comprising:

emitting at least one signal periodically towards the Earth, the signal comprising at least one frequency parameter of the current reception frequency used by the non-geostationary satellite and at least one elevation emission criterion; and

when the position of the non-geostationary satellite relative to the position of the ground-based device verifies the elevation emission criterion:

receiving at least one signal sent by the ground-based device at the current reception frequency, the signal comprising at least one piece of data stored by at least one ground-based device,

wherein the at least one signal sent by the ground-based device and received by the non-geostationary satellite further comprises the position of the ground-based device relative to the position of the non-geostationary satellite and the non-geostationary satellite computes the absolute position of the ground-based device based on the position of the ground-based device relative to the position of the non-geostationary satellite and on the absolute position of the non-geostationary satellite.

10 . A method for the transmission to at least one non-geostationary satellite of at least one piece of data stored by a ground-based device, the method being carried out by the non-geostationary satellite and comprising:

emitting at least one signal periodically towards the Earth, the signal comprising at least one frequency parameter of the current reception frequency used by the non-geostationary satellite and at least one elevation emission criterion; and

when the position of the non-geostationary satellite relative to the position of the ground-based device verifies the elevation emission criterion:

receiving at least one signal sent by the ground-based device at the current reception frequency, the signal comprising at least one piece of data stored by at least one ground-based device,

wherein the elevation emission criterion is an information of the current beam size of the non-geostationary satellite or an elevation emission threshold.

11 . A communication system for the transmission to at least one non-geostationary satellite of at least one piece of data stored by a ground-based device wherein the non-geostationary satellite is configured to carry out the method according to claim 8 .

12 . The communication system according to claim 11 , wherein the non-geostationary satellite is a low Earth orbit satellite.

13 . The communication system according to claim 11 wherein the ground-based device is a resource-constrained device.

14 . A non-transitory computer program product comprising instructions which, when the instructions are executed by a computer, causes the computer to carry out the method according to claim 1 .

15 . A non-transitory computer readable medium comprising instructions which, when executed by a computer, cause the computer to carry out the method according to claim 1 .

16 . A communication system for the transmission to at least one non-geostationary satellite of at least one piece of data stored by a ground-based device wherein the ground-based device is configured to carry out the method according to claim 1 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 18, 2025
From: HIRSCH, ANTONIN; BRICHLER, GEOFFROY; COLLARD, FLORIAN
To: EUTELSAT SA
Reel/Frame 072303/0551 →
Continuity (1)
Related Publication 20230275651A1 · Aug 31, 2023
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