Onboard initial entry processor for facilitating a satellite communication

• US 6,697,344 B1
• Filed: 03/16/1999
• Issued: 02/24/2004
• Est. Priority Date: 03/16/1999
• Status: Expired due to Fees

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Corporation
• Inventors: Wright, David A., Jue, Reginald, Caso, Gregory S., Carrozza, Dominic P., Moretti, Vincent C.
• Primary Examiner(s): Trost, William
• Assistant Examiner(s): ZEWDU, MELESS NMN
• Application Number:
  US09/270,167
• Time in Patent Office: 1,806 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.2, 455/427-431, 455/503, 455/504, 370/321, 370/350, 370/503, 370/324, 370/316, 370/508, 375/371, 375/373, 375/376, 375/343, 375/362-368, 342/357.06
• US Class Current: 370/316
• CPC Class Codes: H04B 7/1858 Arrangements for data transmission on the physical system, i.e. for data bit transmission between network components

Abstract

An initial entry processor (40) for use in a processing satellite (12) in a satellite based communications system (10) is provided having a buffer (62), a detection and timing circuit (64) and an identity circuit (66). The buffer (62) stores an initial entry burst (54) transmitted from at least one terrestrial terminal (14) to the processing satellite (12). The detection and timing circuit (64) detects the initial entry burst (54) and determines a time of arrival of the initial entry burst (54) relative to an initial entry burst slot (52). The identity circuit (66) determines an identity of the terrestrial terminal (14) that transmitted the initial entry burst (54) such that the time of arrival is used by the identified terrestrial terminal (14) during subsequent communications with the processing satellite (12).

Claims

1. An initial entry processor for use in a processing satellite in a satellite based communications system, said initial entry processor comprising:

a buffer operable to store an initial entry burst transmitted from at least one of a plurality of a terrestrial terminals to said processing satellite;

a detection and timing circuit operable to detect said initial entry burst and determine a time of arrival of said initial entry burst relative to an initial entry burst slot, where the detection and timing circuit determines a coarse timing error and a fine timing error of said initial entry burst relative to said initial entry burst slot; and

an identity circuit operable to determine an identity of said terrestrial terminal that transmitted said initial entry burst, wherein said time of arrival is used by said identified terrestrial terminal during subsequent communications with said processing satellite.

2. The initial entry processor as defined in claim 1 wherein said coarse timing error represents an integer number of one half symbols of misalignment of said initial entry burst relative to said initial entry burst slot.

3. The initial entry processor as defined in claim 2 wherein said fine timing error is no more than about one quarter of a symbol.

4. The initial entry processor as defined in claim 1 wherein said detection and timing circuit includes a correlator to correlate said initial entry burst and a modulus to determine a modulus of said correlated data.

5. The initial entry processor as defined in claim 4 further comprising a result buffer operable to store said modulus data and a peak locator operable to determine a maximum modulus from said modulus data.

6. The initial entry processor as defined in claim 5 further comprising a comparitor operable to compare said maximum modulus with at least a threshold value to determine a presence of said initial entry burst.

7. The initial entry processor as defined in claim 6 wherein said detection and timing circuit further includes a fine error function module operable to determine a fine timing error based upon modulus data before and after said maximum modulus.

8. The initial entry processor as defined in claim 7 wherein said identity circuit includes a trig function module operable to form an estimate of a SIN and COS of said correlated data from said correlators.

9. The initial entry processor as defined in claim 8 wherein said identity circuit further includes an inner decoder and an outer decoder operable to decode at least a portion of said initial entry burst to identify said terrestrial terminal that transmitted said initial entry burst.

10. The initial entry processor as defined in claim 1 wherein said initial entry burst includes an L symbol preamble and a D symbol data field, said L symbol preamble used by said detection and timing circuit to detect and determine said time of arrival of said initial entry burst relative to said initial entry burst slot and said D symbol data field used by said identity circuit to identify said terrestrial terminal that transmitted said initial entry burst.

11. An initial entry processor for use in a processing satellite in a satellite based communications system, said initial entry processor comprising:

buffer means for storing an initial entry burst transmitted from one of a plurality of terrestrial terminals to said processing satellite;

detection and timing means for detecting said initial entry burst stored in said buffer means and for determining a time of arrival of said initial entry burst relative to an initial entry burst slot; and

identity means for determining an identity of said terrestrial terminal that transmitted said initial entry burst, wherein said time of arrival is used by said identified terrestrial terminal to re-enter communications with said processing satellite so as to have a reduced timing error between said terrestrial terminal and said processing satellite, wherein said initial entry burst includes an L symbol preamble and a D symbol data field, said L symbol preamble used by said detection and timing means to detect and determine said time of arrival of said initial entry burst and said D symbol data field used by said identity means to identify said terrestrial terminal that transmitted said initial entry burst.

12. The initial entry processor as defined in claim 11 wherein said initial entry burst slot includes said initial entry burst and a window positioned at a leading edge and a lagging edge of said initial entry burst slot.

13. The initial entry processor as defined in claim 11 wherein said detection and timing means determines a coarse timing error and a fine timing error, said coarse timing error represents an integer number of one half symbols of misalignment of said initial entry burst and said fine timing error is no more than one quarter of a symbol.

14. The initial entry processor as defined in claim 13 wherein said detection and timing means includes a correlator to correlate said initial entry burst and a modulus to determine a modulus of said correlated data.

15. The initial entry processor as defined in claim 14 wherein said detection and timing means further includes a result buffer operable to store said modulus data, a peak locator operable to determine a maximum modulus from said modulus data and a fine error function module operable to determine said fine timing error, said maximum modulus used for determining said coarse timing error by said peak locator and said modulus data before and after said maximum modulus used by said fine error function module to determine said fine timing error.

16. A method of performing initial entry of communications between a plurality of terrestrial terminals and a processing satellite, said method comprising the steps of:

transmitting an initial entry burst from one of the plurality of terrestrial terminals during an initial entry burst slot;

receiving the initial entry burst in an initial entry processor in the processing satellite;

detecting the initial entry burst and determining a time of arrival of the initial entry burst relative to the initial entry burst slot with the initial entry processor, including determining a coarse timing error and determining a fine timing error;

identifying the terrestrial terminal that transmitted the initial entry burst with the initial entry processor; and

employing the time of arrival by the identified terrestrial terminal during subsequent communication with the processing satellite.

17. The initial entry method as defined in claim 16 wherein the step of identifying the terrestrial terminal that transmitted the initial entry burst further includes the step of determining an identity field that identifies the terrestrial terminal.