Hybrid space system based on a constellation of low-orbit satellites working as space repeaters for improving the transmission and reception of geostationary signals

• US 9,077,428 B2
• Filed: 12/16/2010
• Issued: 07/07/2015
• Est. Priority Date: 12/17/2009
• Status: Active Grant

• Current Assignee: Airbus Defence and Space GmbH
• Original Assignee: Airbus Defence and Space GmbH
• Inventors: Tronc, Jrme
• Primary Examiner(s): Fan, Chieh M
• Assistant Examiner(s): Cadeau, Wednel
• Application Number:
  US13/516,495
• Publication Number:
  US 20120300815A1
• Time in Patent Office: 1,664 Days
• Field of Search: None
• US Class Current: 1/1
• CPC Class Codes: H04B 1/7115 Constructive combining of multi-path signals, i.e. RAKE receivers
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/18521 Systems of inter linked satellites, i.e. inter satellite service for optical links between satellites H04B10/118
• CPC Class Codes: H04B 7/1855 using a telephonic control signal, e.g. propagation delay variation, Doppler frequency variation, power variation, beam identification
• CPC Class Codes: H04W 40/22 using selective relaying for reaching a BTS [Base Transceiver Station] or an access point

Abstract

The remote communications system, intended for low-throughput data transfer between at least two users located substantially on the surface of a celestial body, includes:

• • a plurality of transmitting/receiving surface terminals, each associated to a user,
  • one or more geostationary element installed on board satellites placed in geostationary orbit around the celestial body, these geostationary elements being able to transmit data from and to a predefined coverage area on the surface of the celestial body with a line of sight to the geostationary satellite,
  • and one or more signal repetition element for the signals transmitted and/or received from the geostationary elements to the surface terminals these traveling repetition elements being on board satellites moving in a traveling orbit; the same frequency band is used for communications between the surface terminals and the traveling elements and for communications between the traveling elements and the geostationary elements.

Claims

1. Telecommunications system, intended for low-throughput data transfer between at least two users located substantially on the surface of a celestial body, comprising:

at least two transmitting/receiving surface terminals, each associated with a different user,

one or more stationary means GEO above the surface of the celestial body, these stationary means being able to transmit data from and to a predefined coverage area with a line of sight to the stationary means, and

one or more signal repeater to repeat signals transmitted and/or received from the stationary means GEO and the surface terminals, said repeater traveling above the surface of the celestial body and comprising means of performing an amplification without frequency translation of the signal received from the stationary means GEO;

a same frequency band being used for communications between the surface terminals and the repeater and for communications between the repeater and the stationary means; and

wherein at least one user terminal utilizes a CDMA type interface to manage arrival of two signals bearing Doppler and delay differences.

2. Telecommunications system according to claim 1, further comprising at least one ground connection station (GES) for the GEO stationary means;

and wherein communications between the repeater and a terrestrial operator are performed via the GEO stationary means and GES connection stations of the GEO stationary means.

3. Telecommunications system according to claim 1, wherein at least one stationary means GEO is installed on board a satellite placed in geostationary orbit around the celestial body.

4. Telecommunications system according to claim 1, wherein at least one repeater is installed on board a satellite moving in low orbit traveling around the celestial body.

5. Telecommunications system according to claim 1, wherein at least one repeater is installed on board a satellite moving in a polar orbit around the celestial body.

6. Telecommunications system according to claim 1, wherein the frequency band is the L band.

7. Telecommunications system according to claim 1, wherein the frequency band is also used for direct communications between the user terminals REC and at least one stationary means GEO.

8. Telecommunications system according to claim 1, wherein said at least one user terminal managing the arrival of two signals comprising Doppler and delay differences comprises a Rake type of receiver.

9. Telecommunications system according to claim 1, wherein at least one repeater is a transparent analog repeater;

and wherein an air interface comprises means of limiting interference at a user terminal REC between the signals from a GEO stationary means and the signals relayed by the transparent analog repeater.

10. Telecommunications system according to claim 1, wherein at least one repeater relays the signal, in a transparent or regenerative way, in an adjacent channel, before its retransmission;

and wherein the communications system comprises a coordination entity for coordinating the frequency plans between the GEO stationary means and the repeater.

11. Telecommunications system according to claim 2, wherein at least one stationary means GEO is installed on board a satellite placed in geostationary orbit around the celestial body.

12. Telecommunications system according to claim 2, wherein at least one repeater is installed on board a satellite moving in low orbit traveling around the celestial body.

13. Telecommunications system according to claim 3, wherein at least one repeater is installed on board a satellite moving in low orbit traveling around the celestial body.

14. Telecommunications method, intended for low-throughput data transfer between two users located substantially on the surface of a celestial body;

the first user being equipped with a user terminal, with a line of sight to at least one repeater, and the repeater having a line of sight to at least one stationary means above the surface of the celestial body, the stationary means configured to transmit data from and to a predefined coverage area, the method comprises the steps of;

transmitting a first uplink signal, representative of data to be transmitted, to the repeater by the first user'"'"'s terminal;

receiving and amplifying the first uplink signal transmitted by the user terminal on the ground; and

transmitting the amplified first uplink signal in the form of a second uplink signal to the stationary means without frequency translation in the same frequency band as the first uplink signal by the repeater, the stationary means ensuring a final transmission of data to a user terminal of the second user and

utilizing a CDMA type interface by at least one user terminal to manage arrival of two signals bearing Doppler and delay differences.

15. Telecommunications method, intended for low-throughput data transfer between two users located substantially on the surface of a celestial body;

the second user being equipped with a second user terminal, with a line of sight to at least one repeater and the repeater having a line of sight to at least one stationary means, the method comprises the steps of;

retransmitting a signal, representative of data to be transmitted, received from a first user via a GES connection station, to the repeater in the form of a first downlink signal by the stationary means;

receiving and amplifying the first downlink signal transmitted by the stationary means;

transmitting the amplified first downlink signal to the second user'"'"'s terminal on the ground without frequency translation in the same frequency band as the first downlink signal in the form of a second downlink signal by the repeater; and

utilizing CDMA type interface by at least one user terminal to manage arrival of two signals bearing Doppler and delay differences.