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 9,859,973 B2
• Filed: 07/06/2015
• Issued: 01/02/2018
• Est. Priority Date: 12/17/2009
• Status: Active Grant

• Current Assignee: Airbus Defence & Space Sas (Airbus SE)
• Original Assignee: Airbus Defence & Space Sas (Airbus SE)
• Inventors: Tronc, Jrme
• Primary Examiner(s): Jagannathan, Melanie
• Application Number:
  US14/792,547
• Publication Number:
  US 20150381267A1
• Time in Patent Office: 911 Days
• 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

Satellite telecommunications system comprises a transmitting/receiving surface terminal associated with a user substantially on a surface of the Earth, a geostationary satellite configured to receive/transmit signals from/to a predefined coverage area with a line of sight to the geostationary satellite, and a traveling satellite moving above the surface of the Earth. The traveling satellite repeats signals received from the surface terminal towards the geostationary satellite and/or repeat signals received from the geostationary satellite towards the surface terminal. The same frequency band is used to communicate between the surface terminal and the traveling satellite and between the traveling satellite and the geostationary satellite. The tracking/telemetry and command signals of the traveling satellite are relayed by the geostationary satellite.

Claims

1. Satellite telecommunications system, comprising:

at least one transmitting/receiving surface terminal associated with a user substantially on a surface of the Earth;

at least one geostationary satellite configured to receive signals from and to transmit signals to a predefined coverage area with a line of sight to said at least geostationary satellite, and

at least one traveling satellite moving above the surface of the Earth and configured to perform at least one of the following using a same frequency band;

repeat signals received from said at least one transmitting/receiving surface terminal towards said at least one geostationary satellite, or repeat signals received from said at least one geostationary satellite towards said at least one transmitting/receiving surface terminal, the same frequency band is used to communicate between said at least one transmitting/receiving surface terminal and said at least one traveling satellite and between said at least one traveling satellite and said least one geostationary satellite; and

wherein tracking/telemetry and command signals of said at least one traveling satellite are relayed by said at least one geostationary satellite.

2. Satellite telecommunications system according to claim 1, further comprising at least one ground connection station of said at least one geostationary satellite;

and wherein communications between said at least one traveling satellite and a terrestrial operator are performed via said at least one geostationary satellite and said at least one ground connection station.

3. Satellite telecommunications system according to claim 2, wherein all communications between said at least one traveling satellite and the terrestrial operator are performed via geostationary satellites.

4. Satellite telecommunications system according to claim 1, wherein said at least one travelling satellite moves in a low orbit.

5. Satellite telecommunications system according to claim 1, wherein said at least one travelling satellite moves in a polar orbit.

6. Satellite telecommunications system according to claim 1, wherein the frequency band is a L band.

7. Satellite telecommunications system according to claim 1, wherein the frequency band is used for direct communications between said at least one transmitting/receiving surface terminal and said at least one geostationary satellite.

8. Satellite telecommunications system according to claim 7, wherein said at least one geostationary satellite is configured to transmit a signal S5 to a ground connection station, the signal S5 comprises:

a signal S1 received directly from said at least one surface terminal, and a signal S2 received from said at least one travelling satellite, the signal S2 corresponds to the signal S1 received and repeated by said at least one travelling satellite.

9. Satellite telecommunications system according to claim 1, wherein said at least one transmitting/receiving surface terminal utilizes a CDMA type interface and comprises a component to manage arrival of two signals bearing Doppler and delay differences.

10. Satellite telecommunications system according to claim 9, wherein the component to manage arrival of two signals bearing Doppler and delay differences is a Rake type of receiver.