Method and apparatus for providing additional resources in a satellite communication system

• US 5,978,653 A
• Filed: 05/02/1997
• Issued: 11/02/1999
• Est. Priority Date: 05/02/1997
• Status: Expired due to Term

• Current Assignee: CDC Propriete Intellectuelle
• Original Assignee: Motorola, Inc. (Motorola Solutions, Inc.)
• Inventors: Taylor, Ronald Fredrick, Blanchard, Scott David, Jeffers, Patrick David
• Primary Examiner(s): VO, NGUYEN THANH
• Application Number:
  US08/850,543
• Time in Patent Office: 914 Days
• Field of Search: 455/9, 455/12.1, 455/13.1, 455/13.2, 455/16, 455/427, 455/428, 455/450, 455/452, 455/509, 455/430
• US Class Current: 455/13.1
• 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 7/195 Non-synchronous stations

Abstract

Additional resources and services are provided in a satellite communication system (100) through the use of seam satellites (52). One or more seam satellites (52) are coupled to communication satellites (12) in an existing constellation using previously unused crosslinks. The seam satellites (52) are located between orbital planes (31 and 36) in which the communication satellites (12) are moving in opposite directions with respect to each other. Seam satellites (52) can provide new services such as earth sensing and observation. Seam satellites (52) can also provide attachment points for other new space-based users. Some of the communication units (26) can communicate with the seam satellites (52) via communication satellites (12). This allows these communication units (26) to use the new services provided by the seam satellite (52). Seam satellites (52) can be controlled by separate control centers or can be controlled by the control center for the communication satellites (12).

Claims

1. A method for providing additional resources in a satellite communication system wherein said satellite communication system comprises a plurality of communication satellites located in orbital planes and a seam exists between a first orbital plane and an other orbital plane, said seam existing when said first orbital plane and said other orbital plane are adjacent and first communication satellites traveling in said first orbital plane are moving in a direction opposite to other communication satellites traveling in said other orbital plane and crosslinks do not exist between said first orbital plane and said other orbital plane, said method comprising the steps of:

positioning at least one seam satellite between said first orbital plane and said other orbital plane;

crosslinking said at least one seam satellite to an edge satellite, said edge satellite is one of said other communication satellites or one of said first communication satellites, said crosslinking accomplished by a crosslink communication channel between said at least one seam satellite and said edge satellite;

adding said at least one seam satellite to a node access list, said node access list denoting accessibility to said at least one seam satellite in said satellite communication system;

using said at least one seam satellite to provide said additional resources; and

updating said node access list according to dynamic conditions in said satellite communication system, wherein said updating step comprises the steps of;

comparing in-use crosslink channels against a crosslink capacity;

setting a seam satellite access status to deny a new seam satellite from accessing said satellite communication system, when said in-use crosslink channels exceeds said crosslink capacity; and

resetting said seam satellite access status to allow said new seam satellite to access said satellite communication system, when said in-use crosslink channels does not exceed said crosslink capacity.

2. The method as claimed in claim 1, wherein said positioning step comprises the steps of:

calculating orbital parameters for said at least one seam satellite using equations which were used to calculate orbital parameters for said plurality of communication satellites; and

establishing a spacing distance based on a collision avoidance plan which is generated from said orbital parameters.

3. The method as claimed in claim 1, wherein said positioning step comprises the step of:

positioning said at least one seam satellite in an orbital plane that is substantially close to said seam.

4. The method as claimed in claim 1, wherein said crosslinking step comprises the steps of:

sending an access request from said at least one seam satellite to said edge satellite;

receiving said access request by said edge satellite;

sending an access denied message from said edge satellite to said at least one seam satellite when said edge satellite determines that said access request cannot be serviced and setting seam satellite access status to deny said at least one seam satellite from accessing said satellite communication system; and

said at least one seam satellite cooperating with said edge satellite to establish a crosslink between said at least one seam satellite and said edge satellite when said edge satellite determines that said access request can be serviced and setting said seam satellite access status to allow said at least one seam satellite to access said satellite communication system.

5. The method as claimed in claim 4, wherein said crosslinking step further comprises the steps of:

when said seam satellite access status is set to deny said at least one seam satellite from accessing said satellite communication system, said at least one seam satellite abstains access to said satellite communication system; and

when said seam satellite access status is reset to allow said at least one seam satellite to access said satellite communication system, said at least one seam satellite initiates access to said satellite communication system.

6. The method as claimed in claim 1, wherein said adding step comprises the steps of:

establishing said at least one seam satellite as a new terminating node in said node access list for said satellite communication system; and

transmitting said node access list on a broadcast channel of said satellite communication system to inform certain system resources about said new terminating node.

7. The method as claimed in claim 1, wherein said using step comprises the steps of:

passing control data between said at least one seam satellite and said edge satellite to control said crosslink communication channel; and

passing mission data between said at least one seam satellite and said edge satellite as required to satisfy mission requirements.

8. The method as claimed in claim 1, wherein said updating step further comprises the steps of:

comparing in-use system crosslink channels against a system crosslink channel capacity;

when said in-use system crosslink channels exceeds said system crosslink channel capacity, said updating step comprises the step of setting said seam satellite access status to deny a new seam satellite from accessing said satellite communication system; and

when said updating step does not set said seam satellite access status to deny, said updating step comprises the step of resetting said seam satellite access status to allow said new seam satellite to access said satellite communication system.

9. A method for operating a seam satellite to provide additional resources in a satellite communication system wherein said satellite communication system comprises a plurality of communication satellites located in orbital planes and a seam exists between a first orbital plane and an other orbital plane, said seam existing when said first orbital plane and said other orbital plane are adjacent and first communication satellites traveling in said first orbital plane are moving in a direction opposite to other communication satellites traveling in said other orbital plane and crosslinks do not exist between said first orbital plane and said other orbital plane, said method comprising the steps of:

positioning said seam satellite between said first orbital plane and said other orbital plane;

crosslinking said seam satellite to an edge satellite, said edge satellite is one of said other communication satellites or one of said first communication satellites, said crosslinking accomplished by a crosslink communication channel between said seam satellite and said edge satellite, wherein said crosslinking step comprises the steps of;

sending an access request from said seam satellite to said edge satellite; and

receiving a message from said edge satellite, said message comprising a seam satellite access status, when said seam satellite access status is set to deny said seam satellite from accessing said communication system, said seam satellite abstains access to said communication system, and when said seam satellite access status is reset to allow said seam satellite to access said communication system, said seam satellite initiates access to said satellite communication system; and

using said seam satellite to provide said additional resources.

10. The method as claimed in claim 9, wherein said positioning step comprises the steps of:

calculating orbital parameters for said seam satellite using equations which were used to calculate said orbital parameters for said plurality of communication satellites; and

establishing a spacing distance based on a collision avoidance plan which is generated from said orbital parameters.

11. The method as claimed in claim 9, wherein said crosslinking step comprises the steps of:

receiving said access request from said seam satellite by said edge satellite;

determining if said seam satellite is a valid user; and

sending said acknowledgment message from said edge satellite, said acknowledgment message comprising said seam satellite access status, wherein

said seam satellite access status is set to deny said seam satellite from accessing said communication system when said seam satellite is not a valid user.

12. The method as claimed in claim 9, wherein said crosslinking step further comprises the steps of:

receiving, by said edge satellite, said access request from said seam satellite;

determining if resources are available; and

sending said acknowledgment message from said edge satellite, said acknowledgment message comprising said seam satellite access status, wherein said seam satellite access status is set to deny said seam satellite from accessing said communication system

when said resources are not available.

13. The method as claimed in claim 9, wherein said using step comprises the steps of:

passing control data between said seam satellite and said edge satellite to control said crosslink communication channel; and

passing mission data between said at seam satellite and said edge satellite as required to satisfy mission requirements.

14. A satellite communication system comprising:

a plurality of communication satellites located in orbital planes wherein a seam exists between a first orbital plane and an other orbital plane, said seam existing when said first orbital plane and said other orbital plane are adjacent and first communication satellites traveling in said first orbital plane are moving in a direction opposite to other communication satellites traveling in said other orbital plane and crosslinks do not exist between said first orbital plane and said other orbital plane;

at least one seam satellite positioned in an orbital plane that is substantially within said seam between said first orbital plane and said other orbital plane, said at least one seam satellite being crosslinked to an edge satellite wherein said edge satellite is one of said other communication satellites or one of said first communication satellites, and said at least one seam satellite providing additional services in said satellite communication system when said at least one seam satellite is crosslinked to said edge satellite;

a plurality of communication units some of which are for requesting said additional services from said at least one seam satellite; and

at least one control center for controlling said plurality of communication satellites and said at least one seam satellite.

15. The satellite communication system as claimed in claim 14, wherein said plurality of communication satellites and said at least one seam satellite are located substantially within a common orbital shell.

16. The satellite communication system as claimed in claim 14, wherein said at least one seam satellite is an Earth Observation Satellite.

17. A seam satellite for use in a satellite communication system, wherein said seam satellite comprises:

an earth-link antenna unit for receiving and transmitting signals by said seam satellite, said signals being command and control signals;

an earth-link transceiver coupled to said earth-link antenna unit, for processing said command and control signals;

a crosslink antenna unit for receiving and transmitting crosslink signals by said seam satellite, said crosslink signals being command signals, control signals, and communication signals that allow said seam satellite to be incorporated into said satellite communication system;

a crosslink transceiver coupled to said crosslink antenna unit, said crosslink transceiver for processing said crosslink signals;

a mission payload antenna unit for receiving and transmitting mission critical signals by said seam satellite;

a mission payload transceiver coupled to said mission payload antenna unit, said mission payload transceiver for processing said mission critical signals;

a controller coupled to said earth-link transceiver, to said crosslink transceiver, and to said mission payload transceiver, said controller processing command data, control data, mission critical data, and communication data, and said controller determining when said seam satellite can be incorporated into said satellite communication system;

a timer means coupled to said controller; and

a memory means coupled to said controller.

18. A communication unit for operating in a satellite communication system wherein said satellite communication system comprises a plurality of communication satellites located in orbital planes wherein a seam exists between a first orbital plane and an other orbital plane, said seam existing when said first orbital plane and said other orbital plane are adjacent and first communication satellites traveling in said first orbital plane are moving in a direction opposite to other communication satellites traveling in said other orbital plane and crosslinks do not exist between said first orbital plane and said other orbital plane, at least one seam satellite wherein said at least one seam satellite is positioned between said first orbital plane and said other orbital plane, said at least one seam satellite being crosslinked to an edge satellite wherein said edge satellite is one of said other communication satellites or one of said first communication satellites, and said at least one seam satellite provides additional services in said satellite communication system, a plurality of communication units some of which for requesting said additional services from said at least one seam satellite, and at least one control center for controlling said plurality of communication satellites and said at least one seam satellite, said communication unit comprising:

a transceiver for receiving data from and transmitting data to said at least one seam satellite via said plurality of communication satellites, wherein received data comprises seam satellite access status and transmitted data comprises an access request; and

a processor for processing said received data, for processing said transmitted data, for prohibiting access to said at least one seam satellite when said seam satellite access status is set to deny said communication unit from accessing said at least one seam satellite in said satellite communication system, and for initiating access to said at least one seam satellite when said seam satellite access status is reset to allow said communication unit to access said at least one seam satellite in said satellite communication system.

19. A communication unit as claimed in claim 18, wherein said communication unit further comprises:

a second transceiver, coupled to said processor, for receiving data from and transmitting data to said at least one seam satellite, wherein data transmitted by said second transceiver comprises a request for access, and data received by said second transceiver comprises said seam satellite access status, wherein

said processor is further for processing said seam satellite access status from said second transceiver,

for prohibiting access to said at least one seam satellite when said seam satellite access status is set to deny said communication unit from accessing said at least one seam satellite in said satellite communication system,

and for initiating access to said at least one seam satellite when said seam satellite access status is reset to allow said communication unit to access said at least one seam satellite in said satellite communication system.

20. A communication unit as claimed in claim 18, wherein said communication unit is further

for transmitting a request for said additional services in response to said at least one seam satellite initiating access to said satellite communication system.