Satellite onboard data transmission system

• US 6,252,690 B1
• Filed: 11/07/1995
• Issued: 06/26/2001
• Est. Priority Date: 10/08/1992
• Status: Expired due to Term

• Current Assignee: Alcatel Espace
• Original Assignee: Alcatel Espace
• Inventors: Laine, Robert
• Primary Examiner(s): PASCAL, LESLIE C
• Application Number:
  US08/554,460
• Time in Patent Office: 2,058 Days
• Field of Search: 359/172, 359/152, 359/154, 359/157, 359/163
• US Class Current: 398/121
• CPC Class Codes: H04B 10/801 using optical interconnects, e.g. light coupled isolators, circuit board interconnections
• CPC Class Codes: H04B 7/18532 Arrangements for managing transmission, i.e. for transporting data or a signalling message

Abstract

A system for transmitting data inside a satellite comprises senders and receivers of digital signals containing the data interconnected by non-directional infra-red links.

Claims

1. A satellite, comprising:

a system for transmitting data inside said satellite;

wherein said system comprises, entirely inside said satellite;

senders,

receivers, and

non-directional infra-red links;

wherein said senders and said receivers respectively send and receive digital signals containing said data,

wherein said senders are interconnected with said receivers by said non-directional infra-red links, and

wherein said digital signals are communicated over said non-directional infra-red links.

2. The satellite according to claim 1, wherein:

each of said senders communicates with one of said receivers by at least one of (1) line-of-sight transmission and (2) reflected transmission.

3. The satellite according to claim 2, wherein:

said reflected transmission is reflected by an optical mirror disposed inside said satellite.

4. The satellite according to claim 1, wherein:

said satellite further comprises;

a central unit, and

equipment units;

said central unit and said equipment units are disposed inside said satellite; and

said digital signals comprise at least one of (1) telecontrol signals sent by said central unit to one of said equipment units and (2) telemetry signals sent by one of said equipment units to said central unit.

5. The satellite according to claim 4, wherein:

each one of said telecontrol signals includes an addressing headers;

said addressing header identifies a corresponding one of said equipment units; and

only said corresponding one of said equipment units is responsive to said one of said telecontrol signals.

6. The satellite according to claim 1, wherein:

said senders and said receivers comprise infra-red diodes.

7. A satellite, comprising:

a central unit,

equipment units, and

a system for transmitting data between said central unit and said equipment units;

wherein said system for transmitting data comprises;

senders,

receivers, and

non-directional infra-red links for carrying said data between said senders and said receivers;

wherein each of said equipment units has a respective sender and a respective receiver, defining respective sender/receiver pairs of said equipment units;

wherein said central unit has fewer of said senders and fewer of said receivers than the total number of said sender/receiver pairs; and

wherein each of said senders communicates with one of said receivers by at least one of (1) line-of-sight transmission, (2) transmission reflected by an optical mirror, and (3) transmission by successive reflections from inside walls of said satellite.

8. The satellite as set forth in claim 7, wherein said data comprises at least one of (1) telecontrol signals sent by said central unit to one of said equipment units and (2) telemetry signals sent by one of said equipment units to said central unit.

9. The satellite as set forth in claim 8, wherein:

each one of said telecontrol signals includes an addressing header;

said addressing header identifies a corresponding one of said equipment units; and

only said corresponding one of said equipment units is responsive to said one of said telecontrol signals.

10. A satellite, comprising:

a satellite onboard transmission system for communicating with a ground station,

equipment units,

a central unit for providing an interface between said equipment units and said satellite onboard transmission system, and

a system for transmitting data between said central unit and said equipment units;

wherein said system for transmitting data comprises;

senders,

receivers, and

non-directional infra-red links for carrying said data between said senders and receivers;

wherein each of said equipment units has a respective sender and a respective receiver, defining respective sender/receiver pairs of said equipment units;

wherein said central unit has fewer of said senders and fewer of said receivers than the total number of said sender/receiver pairs; and

wherein each of said equipment units communicates with said central unit free of intervention by others of said equipment units.

11. The satellite as set forth in claim 10, wherein said data comprises at least one of (1) telecontrol signals sent by said central unit to one of said equipment units and (2) telemetry signals sent by one of said equipment units to said central unit.

12. The satellite as set forth in claim 11, wherein:

each one of said telecontrol signals includes an addressing header;

said addressing header identifies a corresponding one of said equipment units; and

only said corresponding one of said equipment units is responsive to said one of said telecontrol signals.

13. A satellite, comprising:

inner walls,

a central unit, and

equipment units;

wherein said central unit communicates data with said equipment units via non-directional infra-red transmission; and

wherein said transmission overcomes an intervening obstacle by successive reflection from said inner walls.

14. The satellite as set forth in claim 13, wherein said data comprises at least one of (1) telecontrol signals sent by said central unit to one of said equipment units and (2) telemetry signals sent by one of said equipment units to said central unit.

15. The satellite as set forth in claim 14, wherein:

each one of said telecontrol signals includes an addressing header;

said addressing header identifies a corresponding one of said equipment units; and

only said corresponding one of said equipment units is responsive to said one of said telecontrol signals.

16. The satellite as set forth in claim 15, wherein:

said transmission overcomes another intervening obstacle by reflection by an optical mirror.