Communication system employing space-based and terrestrial telecommunications equipment

• US 5,793,813 A
• Filed: 06/06/1996
• Issued: 08/11/1998
• Est. Priority Date: 06/06/1996
• Status: Expired due to Term

• Current Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Original Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Inventors: Cleave, Robert R.
• Primary Examiner(s): Chin, Stephen
• Assistant Examiner(s): DEPPE, BETSY LEE
• Application Number:
  US08/659,317
• Time in Patent Office: 796 Days
• Field of Search: 375/259, 375/377, 375/222, 375/219, 342/352, 364/449.7, 455/12.1, 370/316, 370/401, 340/870.01, 340/853.3, 340/825.06
• US Class Current: 375/259
• CPC Class Codes: G01S 19/14 specially adapted for specific applications
• CPC Class Codes: G01S 2205/002 for traffic control, mobile tracking, guidance, surveillance or anti-collision
• CPC Class Codes: G01S 5/0081 Transmission between base stations
• CPC Class Codes: H04B 7/18567 Arrangements for providing additional services to the basic mobile satellite telephony service

Abstract

A communications system employing a telestation that uses a computer to provide command and data handling, a GPS receiver to provide position, time, and attitude information, and a transceiver to provide two-way wireless digital communications. The computer is coupled to an instrument, measuring device, or payload, and is controlled to relay data generated thereby to a user. Commands and data are uplinked and downlinked to the telestation by way of a satellite network, such as a Globalstar network. The telestation provides a user with real-time command and control of globally distributed instruments. This capability may be used terrestrially for gathering information (e.g., science, environmental, etc.) in remote or inhospitable locations, or where logistical support is inadequate. An in-orbit version may be used for spacecraft or satellite instruments 15, allowing investigators instant access to the instruments during all phases of a mission.

Claims

1. Communication apparatus comprising:

a telestation comprising;

a transceiver;

a computer coupled to transceiver, which computer provides for command and data handling;

a GPS receiver coupled to the computer, which receiver provides position, attitude and time data to the computer; and

a power supply coupled to the transceiver, the computer, and the GPS receiver to provide power thereto;

data-gathering apparatus coupled to the computer, which apparatus provides a means for gathering data indicative of predetermined events;

a user terminal comprising voice and data transceivers, which user terminal generates instrument commands;

a communication gateway having a gateway transceiver;

a communication link coupled between the user terminal and the communication gateway; and

a satellite-based communications system having a plurality of satellite transceivers for communicating between the transceiver in the user terminal and the transceiver in the telestation;

and wherein instrument commands generated at the user terminal are communicated via the communication link to the communication gateway, which uplinks the commands to the satellite-based communications system, which relays the uplinked commands to the transceiver in the telestation, and wherein the computer interprets the commands to configure and control the data-gathering apparatus;

and wherein data gathered by the data-gathering apparatus is processed by the computer and is transmitted by the transceiver in the telestation by way of the satellite-based communications system to the gateway, which transmits the data to the user terminal by way of the communication link.

2. The communication apparatus of claim 1 wherein the computer is coupled to a data recorder that provides for command and data handling.

3. The communication apparatus of claim 1 wherein the power supply comprises a solar panel.

4. The communication apparatus of claim 1 wherein the power supply comprises a battery.

5. The communication apparatus of claim 1 further comprising:

a data interface coupled to the computer for interfacing to devices that are external to the communication apparatus.

6. The communication apparatus of claim 1 wherein the communication gateway comprises a public service telephone network.

7. The communication apparatus of claim 1 wherein the communication gateway comprises an Internet link.

8. The communication apparatus of claim 1 wherein the satellite-based communications system comprises a Globalstar satellite-based communications system.

9. The communication apparatus of claim 1 further comprising:

a local oscillator;

and wherein the transceiver in the telestation comprises;

an RF antenna;

an RF converter coupled to the RF antenna;

a signal processor coupled between the RF converter and the computer which signal processor outputs commands uplinked by the user to the computer and outputs data by way of the computer that is downlinked to the user;

a first frequency synthesizer having an input coupled to the local oscillator and having outputs coupled to the RF converter and signal processor;

and wherein the GPS receiver comprises;

a GPS antenna;

an RF downconverter coupled to the GPS antenna;

a signal/navigation processor coupled between the RF downconverter and the computer which signal/navigation processor outputs position velocity and time data to the computer;

a second frequency synthesizer having an input coupled to the local oscillator and having outputs coupled to the RF downconverter and the signal/navigation processor.

10. Communication apparatus comprising:

a telestation comprising;

a transceiver;

a computer coupled to transceiver, which computer provides for command and data handling;

a GPS receiver coupled to the computer, which receiver provides position, attitude and time data to the computer; and

a power supply coupled to the transceiver, the computer, and the GPS receiver to provide power thereto;

a user terminal comprising voice and data transceivers, which user terminal generates instrument commands;

a communication gateway having a gateway transceiver;

a communication link coupled between the user terminal and the communication gateway; and

a satellite-based communications system having a plurality of satellite transceivers for communicating between the transceiver in the user terminal and the transceiver in the telestation;

and wherein commands generated at the user terminal are communicated via the communication link to the communication gateway, which uplinks the commands to the satellite-based communications system, which relays the uplinked commands to the transceiver in the telestation, and wherein the computer interprets the commands to configure and control the telestation.

11. The communication apparatus of claim 10 wherein the computer is coupled to a payload, and wherein the computer couples commands to the payload.

12. The communication apparatus of claim 10 wherein the power supply comprises a solar panel.

13. The communication apparatus of claim 10 wherein the power supply comprises a battery.

14. The communication apparatus of claim 10 further comprising:

a data interface coupled to the computer for interfacing to devices that are external to the communication apparatus.

15. The communication apparatus of claim 10 wherein the communication gateway comprises a public service telephone network.

16. The communication apparatus of claim 10 wherein the communication gateway comprises an Internet link.

17. The communication apparatus of claim 10 wherein the satellite-based communications system comprises a Globalstar satellite-based communications system.

18. The communication apparatus of claim 10 further comprising:

a local oscillator;

and wherein the transceiver in the telestation comprises;

an RF antenna;

an RF converter coupled to the RF antenna;

a signal processor coupled between the RF converter and the computer, which signal processor outputs commands uplinked by the user to the computer and outputs data by way of the computer that is downlinked to the user;

a first frequency synthesizer having an input coupled to the local oscillator and having outputs coupled to the RF converter and signal processor;

and wherein the GPS receiver comprises;

a GPS antenna;

an RF downconverter coupled to the GPS antenna;

a signal/navigation processor coupled between the RF downconverter and the computer which signal/navigation processor outputs position velocity and time data to the computer;

a second frequency synthesizer having an input coupled to the local oscillator and having outputs coupled to the RF downconverter and the signal/navigation processor.