Transmission apparatus for orbiting satellite

• US 5,465,096 A
• Filed: 12/30/1994
• Issued: 11/07/1995
• Est. Priority Date: 03/01/1993
• Status: Expired due to Term

• Current Assignee: NEC Corporation
• Original Assignee: NEC Corporation
• Inventors: Nawata, Hizuru
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/367,687
• Time in Patent Office: 312 Days
• Field of Search: 342/375, 342/354, 342/357, 455/12.1, 455/13.1, 455/13.2, 455/13.3
• US Class Current: 342/354
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

A transmission apparatus for an orbiting satellite which can establish stabilized frame synchronization even if the distance between the round-trip satellite and a communications terminal varies and which can minimize the displacement between a frame signal received on the ground and another frame signal generated in a communications terminal. The transmission apparatus comprises M (M is an integral number equal to or greater than 2) composers for forming frame signals, M transmitters for outputting M spot beams having different radiation directions, and M delay circuits interposed between the composers and the transmitters. The delay times of the delay circuits are set so that they are long where the radiation angles of the corresponding spot beams are small, but they are shorter where the radiation angles are larger.

Claims

1. A transmission apparatus for an orbiting satellite which travels around the earth along a low or intermediate orbit, comprising:

M input terminals, M being an integral number equal to or grater than 2;

a frame generator for generating a frame synchronizing signal at a fixed interval;

M composers for forming frame signals from respective transmission data received at said M input terminals in response to the frame synchronizing signal from said frame generator;

M transmitters for receiving outputs of said M composers and outputting M spot beams having different radiation directions from one another;

M frame signal delay circuits individually interposed between said M composers and said M transmitters; and

delay time setting means for setting, for each of said M frame signal delay circuits, a delay time which varies inversely proportionally to the distance from the orbiting satellite to the center of a cell resulting from a corresponding spot beam transmitted to the earth.

2. A transmission apparatus for an orbiting satellite as claimed in claim 1, wherein said delay time setting means includes distance measurement means for measuring the distance from said orbiting satellite to the ground, and conversion means for converting measurement data from said distance measurement means into a delay time which increases in inverse proportion to the distance, the delay time being adjusted in accordance with a variation of the distance.

3. The transmission apparatus for an orbiting satellite as claimed in claim 1, wherein said frame signal delay circuit comprises:

a delay circuit receiving the frame signal output of said composer and outputting a signal having a delay time; and

said delay time setting means determines the delay time of the output signal of said delay circuit.

4. The transmission apparatus for an orbiting satellite as claimed in claim 3, wherein said delay circuit comprises:

a shift register receiving the frame signal output of said composer, and producing outputs having delay times which differ from each other in a stepwise fashion; and

a multiplexer selecting one of the outputs of said shift register as the output of said delay circuit.

5. The transmission apparatus for an orbiting satellite as claimed in claim 3, wherein said delay circuit comprises:

a random access memory receiving the frame signal output of said composer, and producing the output of said delay circuit;

a write counter designating a write address for said random access memory;

a read counter designating a read address of said random access memory; and

a controller which controls the write operation of said write counter and the read operation of said read counter, said controller receives a clock signal for use by said counters, a high speed clock signal for simultaneous writing and reading of said random access memory, and a delay time from said delay time setting means.

6. The transmission apparatus for an orbiting satellite as claimed in claim 1, further comprising:

a distance measurement section which measures the distance from the orbiting satellite to the earth;

said frame signal delay circuit includes;

a conversion section which converts the distance measurement determined by the distance measurement section into a delay time; and

a delay circuit receiving the frame signal output of said composer, and based on the delay time of said conversion section, outputs a frame signal having a delay time.

7. The transmission apparatus for an orbiting satellite as claimed in claim 6, wherein said delay circuit comprises:

a shift register receiving the frame signal output of said composer, and producing outputs having delay times which differ from each other in a stepwise fashion; and

a multiplexer selecting an output of said shift register based on the delay time determined by said conversion section.

8. The transmission apparatus for an orbiting satellite as claimed in claim 6, wherein said delay circuit comprises:

a random access memory receiving the frame signal output of said composer, and producing the output of said delay circuit;

a write counter designating a write address for said random access memory;

a read counter designating a read address of said random access memory; and

a controller which controls the write operation of said write counter and the read operation of said read counter, said controller receives a clock signal for use by said counters, a high speed clock signal for simultaneous writing and reading of said random access memory, and a delay time from said conversion section.

9. A transmission apparatus for an orbiting satellite, comprising:

input terminals for receiving transmission data;

a frame generator which generates a frame synchronizing signal at a fixed interval;

composers receiving transmission data from said input terminals and outputting frame signals in response to the frame synchronizing signal for said frame generator;

frame signal delay circuits which receive the frame signal outputs of the composers and interpose a delay time to each such frame signal output;

transmitters processing the delayed frame signal outputs of said frame signal delay circuits and transmitting to earth spot beams having different radiation directions, wherein the spot beams result in communication cells on earth; and

the delay time interposed on each output signal of said frame signal delay circuits varies inversely proportionally to the distance from the orbiting satellite to the center of a communication cell on earth.

10. The transmission apparatus for an orbiting satellite as claimed in claim 9, wherein said frame signal delay circuit comprises:

a delay circuit receiving the frame signal output of said composer and outputting a signal having a delay time; and

a delay time setting means for determining the delay time of the output signal of said delay circuit

11. The transmission apparatus for an orbiting satellite as claimed in claim 9, wherein said delay circuit comprises:

a shift register receiving the frame signal output of said composer, and producing outputs having delay times which differ from each other in a stepwise fashion; and

a multiplexer selecting a fixed one of the outputs of said shift register as the output of said delay circuit.

12. The transmission apparatus for an orbiting satellite as claimed in claim 10, wherein said delay circuit comprises:

a random access memory receiving the frame signal output of said composer, and producing the output of said delay circuit;

a write counter designating a write address for said random access memory;

a read counter designating a read address of said random access memory; and

a controller which controls the write operation of said write counter and the read operation of said read counter, said controller receives a clock signal for use by said counters, a high speed clock signal for simultaneous writing and reading of said random access memory, and a delay time from said delay time setting means.

13. The transmission apparatus for an orbiting satellite as claimed in claim 9, further comprising:

a distance measurement section which measures the distance from the orbiting satellite to the earth;

said frame signal delay circuit includes;

a conversion section which converts the distance measurement determined by the distance measurement section into a delay time; and

a delay circuit receiving the frame signal output of said composer, and based on the delay time of said conversion section, outputs a frame signal having a delay time.

14. The transmission apparatus for an orbiting satellite as claimed in claim 13, wherein said delay circuit comprises:

a shift register receiving the frame signal output of said composer, and producing outputs having delay times which differ from each other in a stepwise fashion; and

a multiplexer selecting an output of said shift register based on the delay time determined by said conversion section.

15. The transmission apparatus for an orbiting satellite as claimed in claim 13, wherein said delay circuit comprises:

a random access memory receiving the frame signal output of said composer, and producing the output of said delay circuit;

a write counter designating a write address for said random access memory;

a read counter designating a read address of said random access memory; and

a controller which controls the write operation of said write counter and the read operation of said read counter, said controller receives a clock signal for use by said counters, a high speed clock signal for simultaneous writing and reading of said random access memory, and a delay time from said delay time setting means.

16. A transmission apparatus for an orbiting satellite, comprising:

input terminals for receiving transmission data;

a frame generator which generates a frame synchronizing signal at a fixed interval;

composers receiving transmission data from said input terminals and outputting frame signals in response to the frame synchronizing signal for said frame generator;

frame signal delay circuits which receive the frame signal outputs of the composers and interposes a delay time to each such frame signal output;

transmitters processing the delayed frame signal outputs of said frame signal delay circuits and transmitting to earth spot beams having different radiation directions, wherein the spot beams result in communication cells on earth; and

the delay time interposed on each output signal of said frame signal delay circuits increases as the radiation angle of the spot beams increases, thus the delay time varies inversely proportionally to the distance from the orbiting satellite to the center of a communication cell on earth.