Dual layer satellite communications system and geostationary satellite therefor

• US 6,023,605 A
• Filed: 09/08/1997
• Issued: 02/08/2000
• Est. Priority Date: 03/19/1997
• Status: Expired due to Fees

• Current Assignee: Fujitsu Limited
• Original Assignee: Fujitsu Limited
• Inventors: Sasaki, Takao, Katoh, Tadayoshi
• Primary Examiner(s): Eisenzopf, Reinhard J.
• Assistant Examiner(s): Kincaid, Lester G.
• Application Number:
  US08/925,287
• Time in Patent Office: 883 Days
• Field of Search: 455/12.1, 455/13.1, 455/427, 455/428, 455/429, 455/430, 455/13.2, 455/13.3, 244/158 R, 370/316, 370/323, 370/325, 342/359, 342/368, 342/352, 342/354
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/1851 Systems using a satellite or space-based relay H04B7/18508, H04B7/18521 take precedence; providing specific services H04B7/18523 - H04B7/18576
• CPC Class Codes: H04B 7/195 Non-synchronous stations

Abstract

The system allows a plurality of earth stations to communicate with one another by relaying transmission signals via satellites circling the earth in high earth and low earth orbits. A geostationary satellite operates in a geostationary orbit, while a plurality of low-earth orbiting satellites circle the earth in low-earth orbits. Those satellites serve as repeaters for the communications between a first earth station and a second earth station. Tracking relay means, disposed in the geostationary satellite, tracks only a limited number of low-earth orbiting satellites within an orbital range that corresponds to a predetermined area on the earth. Accordingly, the tracking relay means relays transmission signals of the second earth station to the low-earth orbiting satellites only when they are within the orbital range.

Claims

1. A dual layer satellite communications system that allows a plurality of earth stations to communicate with one another by relaying transmission signals via satellites circling the earth in high earth and low earth orbits, comprising:

a first earth station located on the earth'"'"'s surface;

a second earth station located on the earth'"'"'s surface;

a geostationary satellite circling the earth in a high-earth geostationary orbit, which always faces a predetermined area on the earth;

a plurality of low-earth orbiting satellites circling the earth in low earth orbits for relaying transmission signals between said geostationary satellite and said first earth station;

tracking relay means, disposed in said geostationary satellite, for relaying transmission signals to/from said low-earth orbiting satellites, while tracking said low-earth orbiting satellites within an orbital range that corresponds to the predetermined area on the earth; and

a network control station located on the earth'"'"'s surface, which acquires relative positions of said first and second earth stations, said geostationary satellite, and said plurality of low-earth orbiting satellites, and sends tracking information to said first and second earth stations, said geostationary satellite, and said plurality of low-earth orbiting satellites

wherein said network control station comprises time estimation means for estimating an entry time when one of the low-earth orbiting satellites enters to the orbital range and an exit time when said one of tie low-earth orbiting satellites exits from the orbital range, and sending the estimated entry time and the estimated exit time to said first and second earth stations, said geostationary satellite, and said plurality of low-earth orbiting satellites.

2. The dual layer satellite communications system according to claim 1, wherein said network control station comprises

restarting means for, when said low-earth satellites have all left the orbital range and an ongoing communication session between said first and second earth stations is thus interrupted, restarting the communication session between said first and second earth stations after waiting for one of said low-earth orbiting satellites to enter to said orbital range.

3. The dual layer satellite communications system according to claim 1, further comprising

area changing means for changing said orbital range when a predetermined condition is satisfied.

4. The dual layer satellite communications system according to claim 3, wherein said predetermined condition is satisfied when a time previously scheduled in Universal Time Coordinate has come.

5. The dual layer satellite communications system according to claim 3, wherein said predetermined condition is satisfied when a frequency of communication requests from the earth stations exceeds a predetermined threshold.

6. The dual layer satellite communications system according to claim 1, wherein said plurality of low-earth orbiting satellites includes low-earth orbiting satellites dedicated to either uplink communications or downlink communications.

7. The dual layer satellite communications system according to claim 1, wherein said network control station comprises

elevation angle updating means for updating a minimum elevation angle that enables said first earth station to communicate with said low-earth orbiting satellites, according to weather conditions.

8. The dual layer satellite communications system according to claim 1, wherein said network control station comprises

elevation angle registration means for previously registering a minimum elevation angle that enables said first earth station to communicate with said low-earth orbiting satellites,

time determination means for determining tracking start time and tracking end time to control mutual tracking of said first earth station and one of said low-earth orbiting satellites facing the first earth station according to the minimum elevation angle that is registered in said elevation angle registration means.

9. A geostationary satellite for dual layer satellite communications system that allows a plurality of earth stations to communicate with one another by relaying transmission signals via satellites circling the earth in high earth and low earth orbits, comprising

tracking relay means for tracking low-earth orbiting satellites, only within an orbital range that is mapped onto a part of the corresponding predetermined area on the earth that the geostationary satellite always faces, to relay transmission signals to/from low-earth orbiting satellites,

wherein the tracking relay means is responsive to tracking information and timing information sent from a network control station located on the earth'"'"'s surface.

10. The geostationary satellite according to claim 9, further comprising

area changing means for changing said orbital range when a predetermined condition is satisfied.

11. The geostationary satellite according to claim 10, wherein said predetermined condition is satisfied when a time previously scheduled in Universal Time Coordinate has come.

12. The geostationary satellite according to claim 10, wherein said predetermined condition is satisfied when a frequency of communication requests from the earth stations exceeds a predetermined threshold.