Methods and apparatus for using ground based processing resources to support orbiting satellites

• US 6,553,208 B1
• Filed: 09/15/2000
• Issued: 04/22/2003
• Est. Priority Date: 09/15/2000
• Status: Active Grant

• Current Assignee: CDC Propriete Intellectuelle
• Original Assignee: Motorola, Inc. (Motorola Solutions, Inc.)
• Inventors: Redden, James Powers, Worger, William Robert, Schaefer, Bradley Robert
• Primary Examiner(s): Trost, William
• Assistant Examiner(s): Ferguson, Keith
• Application Number:
  US09/663,520
• Time in Patent Office: 949 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.2, 455/427, 455/428, 455/430, 370/389, 370/498, 370/532, 342/357.17, 709/201, 709/202
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays

Abstract

A plurality of orbiting satellites (102-112), each comprised of an onboard computer (142). Each of the orbiting satellites and a plurality of ground-based computers (114-124) are utilized to perform delay-insensitive functions associated with the orbiting satellites. An ubiquitous data link (128-138) is maintained between each satellite and one or more of the ground-based computers. The integrated system is configured to allow a satellite to generate a remote procedure call (RPC), transmit the RPC to a ground-based computer, whereupon the ground-based computer processes the RPC and transmits a response back to the satellite. Delay-sensitive tasks and functions are performed by the computer onboard the satellite; delay-insensitive tasks are advantageously performed by the ground-based computer assets.

Claims

1. A satellite communications system, comprising:

a plurality of earth-orbiting satellites, each having an onboard computer, wherein each said onboard computer includes a first processor, a first memory, and a first data transceiver;

a plurality of ground-based computers, each having a second processor, a second memory, and second data transceiver;

wherein each said first data transceiver is configured to communicate with at least one said second data transceiver to thereby form a high data rate, low latency data link;

wherein each said first processor is configured to automatically generate a remote procedure call (RPC), and each said first data transceiver is configured to automatically transmit an RPC to one said second data transceiver, whereupon one said second processor processes said RPC and generates a response to said RPC; and

wherein one said second transceiver is configured to upload said response to one of said onboard computer.

2. The satellite communications system of claim 1, wherein each said first processor and each said second processor are configured to execute respective software applications which share a common architecture.

3. The satellite communications system of claim 1, wherein each said first processor is configured to periodically generate RPCs at substantially regular intervals.

4. The satellite communications system of claim 1, wherein a particular one of said plurality of ground-based computers is dedicated to processing RPCs for a unique one of said satellites.

5. The satellite communications systems of claim 1, further comprising a multiplexor, and wherein RPCs generated by each of said plurality of satellites are routed by said multiplexor to one of said plurality of ground-based computers in accordance with a then current processing capacity of said plurality of ground-based computers.