Redundant satellite system

• US 6,487,476 B1
• Filed: 09/24/1998
• Issued: 11/26/2002
• Est. Priority Date: 09/24/1998
• Status: Expired due to Fees

• Current Assignee: ESBH, Inc.
• Original Assignee: ESBH, Inc.
• Inventors: Draim, John E.
• Primary Examiner(s): Zanelli, Michael J.
• Assistant Examiner(s): Gibson, Eric M
• Application Number:
  US09/160,478
• Time in Patent Office: 1,524 Days
• Field of Search: 701/13, 701/226, 244/158.R, 455/13.1
• US Class Current: 701/13
• CPC Class Codes: H04B 7/18534 for enhancing link reliablility, e.g. satellites diversity

Abstract

A diversity satellite system using a trailer satellite concept. The main satellite is placed into orbit and the trailer satellite, typically a much smaller satellite, is in orbit with the main satellite. The main satellite and trailer satellite are communicating with one another by crosslinks. In this way, two alternative geometric configurations are possible: a first geometric configuration direct from the ground station to the first satellite, and a second geometric configuration to the main satellite from the ground station via the trailer satellite. This enables avoiding interference.

Claims

1. A redundant satellite system communicating with an earth based ground station, comprising:

a main satellite in a predetermined low earth or medium earth orbit, orbiting the earth, and having a communication element which communicates with the ground station on the earth;

a trailer satellite, having a smaller overall size than said main satellite, and in a similar orbit to said main satellite but spaced therefrom to be one of preceding said main satellite or following said main satellite in a way such that a first geometric path between the ground station and said main satellite is different than a second geometric path between the ground station and said trailer satellite,

said trailer satellite and said main satellite each including auxiliary communication parts such that said trailer satellite communicates directly with said main communication satellite over a crosslink path different than either said first geometric path or said second geometric path; and

a controller element, determining when communications between the ground station and the main satellite is likely to include interference, and in response to determining said interference, changing a path of communications between said ground station and said main satellite, from said first geometric path, to said second geometric path and said crosslink path, thereby forming an alternative path.

2. A system as in claim 1 wherein said main satellite and said trailer satellite are in substantially the same orbit, with a space therebetween.

3. A system as in claim 2 wherein said space is between 100-300 kilometers.

4. A system as in claim 1 wherein said interference includes interference with another satellite in a main beam of an antenna on the ground site on the same frequency as the main satellite.

5. A system as in claim 1 wherein said controller element is in the ground station.

6. A system as in claim 5 wherein said controller element includes information indicating a path of the main satellite and a path of other satellites which are likely to interfere with the main satellite.

7. A system as in claim 6 further comprising a processor in the controller, analyzing the paths and determining when interference is likely to exist, and changing the paths when said interference is likely to exist.

8. A system as in claim 1 wherein said auxiliary communication parts is one of an RF or laser.

9. A system as in claim 1 wherein said main satellite and said trailer satellite are each in elliptical orbits.

10. A system as in claim 1 wherein said trailer satellite weighs less then 40 kilograms.

13. A method as in claim 9 wherein said main satellite and said trailer satellite are each in elliptical orbits.

14. A method as in claim 9 wherein said trailer satellite weighs less then 40 kilograms.

11. A method of operating a diversity system, comprising:

establishing two satellites into respective predetermined orbits lower than geostationary, including a main satellite in a predetermined orbit having a communication element which communicates with a ground station on the earth, and a second communication element for crosslink communications, and a trailer satellite, spaced from said main communication satellite, said trailer satellite also having a communication element which communicates with a ground station on the earth, and a crosslink element which communicates with said crosslink element on said main satellite;

determining when communications between said ground station and said main satellite is likely to include interference;

normally communicating with said main satellite;

in response to determining said interference, changing a path of communications from said ground station to said main satellite, to said ground station to said trailer satellite via said crosslink to said main satellite thereby forming an alternative path from said ground station to said main satellite via said trailer satellite.

12. A method as in claim 11 wherein said main satellite and said trailer satellite are in substantially the same orbit but spaced from one another so that said trailer satellite either proceeds or trails main satellite.

15. A system comprising:

a ground station on the earth;

a main satellite in predetermined low earth or medium earth elliptical orbit, orbiting the earth, and having a communication element which communicates with the ground station on the earth;

a trailer satellite, having a smaller overall size than said main satellite, and weighing less than 40 kilograms, and in a similar orbit to said main satellite but spaced therefrom to be one of preceding said main satellite or following said main satellite in a way such that a first geometric path between the ground station and said main satellite is different than a second geometric path between the ground station and said trailer satellite,

said trailer satellite and said main satellite each including auxiliary communication parts such that said trailer satellite communicates directly with said main communication satellite over a crosslink path different than either said first geometric path or said second geometric path; and

a controller element, having a processor determining when communications between the ground station and the main satellite is likely to include interference, and, in response to determining said interference, changing a path of communications between said ground station and said main satellite, from said first geometric path, to said second geometric path and said crosslink path, thereby forming an alternative path.