Satellite communication system having double-layered earth orbit satellite constellation with two different altitudes

• US 5,722,042 A
• Filed: 10/12/1995
• Issued: 02/24/1998
• Est. Priority Date: 02/06/1995
• Status: Expired due to Fees

• Current Assignee: ATR Optical And Radio Communications Research Laboratories
• Original Assignee: ATR Optical And Radio Communications Research Laboratories
• Inventors: Kimura, Kazuhiro, Karasawa, Yoshio
• Primary Examiner(s): MULLEN, THOMAS J
• Application Number:
  US08/541,268
• Time in Patent Office: 866 Days
• Field of Search: 455/12.1, 455/13.1, 370/316, 342/352, 342/353, 342/355
• US Class Current: 455/13.1
• CPC Class Codes: H04B 7/195 Non-synchronous stations

Abstract

A satellite communication system has a double-layered earth orbit satellite constellation with a lower first orbit altitude and a higher second orbit altitude. In the satellite communication system, first and second communication satellites are deployed in respective earth orbits located at the first and second orbit altitudes to each have first and second satellite communication stations, respectively. Small terminals and large terminals are further provided as earth stations on the earth. Each first satellite communication station communicates with the small terminals and communicates with the first satellite communication stations of adjacent first communication satellites within the same earth orbit and the second satellite communication stations, and each second satellite communication station communicates with the large terminals and communicates with the second satellite communication stations of adjacent communication satellites within the same earth orbit, the second satellite communication stations of the second communication satellites of both adjacent earth orbits, and the first satellite communication stations.

Claims

1. A satellite communication system having a double-layered earth orbit satellite constellation with two different altitudes including a predetermined first orbit altitude and a predetermined second orbit altitude higher than the first orbit altitude, comprising:

a plurality of first communication satellites deployed in each of a plurality of earth orbits located at the first orbit altitude, each of said plurality of first communication satellites having a first satellite communication station;

a plurality of second communication satellites deployed in each of a plurality of earth orbits located at the second orbit altitude, each of said plurality of second communication satellites having a second communication satellite station;

a plurality of small terminals provided as earth stations on the earth, each of said plurality of small terminals being used as one of a mobile terminal and a semi-fixed terminal; and

a plurality of large terminals provided as earth stations on the earth, each of said plurality of large terminals being used as a fixed terminal,

wherein each of said first satellite communication stations comprises;

first communication means for communicating with at least one of said plurality of small terminals and for communicating with at least one of said first satellite communication stations of adjacent first communication satellites within the same earth orbit and said plurality of second satellite communication stations; and

first repeater exchange means for relaying and switching a signal of at least two of said communications performed by said first communication means,

wherein each of said second satellite communication stations comprises;

second communication means for communicating with at least one of said plurality of large terminals and for communicating with at least one of said second satellite communication stations of adjacent communication satellites within the same earth orbit, said second satellite communication stations of said second communication satellites of both adjacent earth orbits, and said plurality of first satellite communication stations; and

second repeater exchange means for relaying and switching a signal of at least two of said communications performed by said second communication means,

wherein each of said small terminals comprises third communication means for communicating with at least one of said plurality of first satellite communication stations, and

wherein each of said large terminals comprises fourth communication means for communicating with at least one of said plurality of second satellite communication stations.

2. The satellite communication system as claimed in claim 1, wherein said first orbit altitude is set to an altitude within a range of 700 km to 2000 km, and

wherein said second orbit altitude is set to an altitude within one of a range of 1200 km to 2000 km and a range of 10000 km to 20000 km.

3. The satellite communication system as claimed in claim 2,

wherein (a) communications between one of said first satellite communication stations and another one of said first satellite communication stations,

(b) communications between one of said second satellite communication stations and another one of said second satellite communication stations, and

(c) communications between said first satellite communication stations and said second satellite communication stations are carried out through optical satellite communication lines, and

wherein (d) communications between said first satellite communication stations and said small terminals, and

(e) communications between said second satellite communication stations and said large terminals are carried out through radio satellite communication lines.

4. The satellite communication system as claimed in claim 2,

wherein (a) communications between one of said first satellite communication stations and another one of said first satellite communication stations,

(b) communications between one of said second satellite communication stations and another one of said second satellite communication stations,

(c) communications between said first satellite communication stations and said second satellite communication stations,

(d) communications between said first satellite communication stations and said small terminals, and

(e) communications between said second satellite communication stations and said large terminals are carried out through radio satellite communication lines.

5. The satellite communication system as claimed in claim 1,

wherein (a) communications between one of said first satellite communication stations and another one of said first satellite communication stations,

(b) communications between one of said second satellite communication stations and another one of said second satellite communication stations, and

(c) communications between said first satellite communication stations and said second satellite communication stations are carried out through optical satellite communication lines, and

wherein (d) communications between said first satellite communication stations and said small terminals, and

(e) communications between said second satellite communication stations and said large terminals are carried out through radio satellite communication lines.

6. The satellite communication system as claimed in claim 1,

wherein (a) communications between one of said first satellite communication stations and another one of said first satellite communication stations,

(b) communications between one of said second satellite communication stations and another one of said second satellite communication stations,

(c) communications between said first satellite communication stations and said second satellite communication stations,

(d) communications between said first satellite communication stations and said small terminals, and

(e) communications between said second satellite communication stations and said large terminals are carried out through radio satellite communication lines.