Method and apparatus for approximating propagation delay for use in transmission compensation to orbiting satellites

• US 5,644,572 A
• Filed: 10/03/1995
• Issued: 07/01/1997
• Est. Priority Date: 10/03/1995
• Status: Expired due to Term

• Current Assignee: Google Technology Holdings LLC (Alphabet Inc.)
• Original Assignee: Motorola, Inc. (Motorola Solutions, Inc.)
• Inventors: Cutler, Victor Hawes, Olds, Keith Andrew, Tayloe, Daniel Richard
• Primary Examiner(s): Olms, Douglas W.
• Assistant Examiner(s): Patel, Ajit
• Application Number:
  US08/538,762
• Time in Patent Office: 637 Days
• Field of Search: 455/12.1, 455/13.2, 455/67.1, 455/13.1, 455/67.6, 342/355, 342/458, 342/356, 342/357, 342/358, 342/352, 342/354, 370/104.1, 370/103, 370/100.1
• US Class Current: 370/324
• CPC Class Codes: H04B 7/1855 using a telephonic control signal, e.g. propagation delay variation, Doppler frequency variation, power variation, beam identification
• CPC Class Codes: H04B 7/2125 Synchronisation
• CPC Class Codes: H04J 3/0682 by delay compensation, e.g. by compensation of propagation delay or variations thereof, by ranging

Abstract

A subscriber unit (30) operates in a synchronous communication system having dynamic nodes such as satellites (12). Satellites (12) employ a strict transmit and receive time window and all transmissions directed to satellites (12) must fall within the receive window to be recognized. In a dynamic communication system where low earth orbit satellites (12) continuously orbit, propagation timing between a satellite (12) and a subscriber unit (30) vary rapidly over a wide range. Subscriber unit (30) must approximate a transmit timing advance for use in inaugurating a transmission to satellite (12). Subscriber unit (30) utilizes a valid geolocation position when available but when a position is unavailable or stale, relies on configuration characteristics of the constellation for generating an initial approximation of propagation delay.

Claims

1. A method in a synchronous communication system for approximating a transmit time advance offset for use by a subscriber unit in transmitting information to a first satellite having a plurality of beams, one of which is a current beam projected about said subscriber unit, said information arriving at said first satellite during a receive window, and said transmit time advance offset corresponding to a propagation delay in said current beam between said subscriber unit and said first satellite, said method comprising the steps of:

when said subscriber unit does not possess a current geolocation position of said subscriber unit, receiving a first transmission from said first satellite, said first transmission in said current beam comprising a first beam identifier and a first beam center defining a first geographical coordinate of an approximated center of said current beam;

determining if said current beam servicing said subscriber unit is a centrally located beam among said plurality of beams of said first satellite;

when said current beam is centrally located among said plurality of beams defining said first beam center as an approximation of a subscriber unit location;

calculating a distance between said first satellite and said subscriber unit, said distance being derived from said subscriber unit location; and

estimating said transmit time advance offset from said distance between said first satellite and said subscriber unit.

2. A method as recited in claim 1, further comprising the step of prior to said receiving step, evaluating if said subscriber unit possesses said current geolocation position of said subscriber unit, said current geolocation position defining a subscriber unit location.

3. A method as recited in claim 2, wherein said current geolocation position was determined using a passive geolocation method.

4. A method as recited in claim 3, wherein said subscriber unit employs global positioning services as said passive geolocation method.

5. A method as recited in claim 2, further comprising the steps of:

when said current beam is not a centrally located beam of said first satellite, secondly determining if said subscriber unit can detect a second transmission from a second satellite; and

when said subscriber unit detects said second transmission from said second satellite, generating a differential time of arrival between said first transmission from said first satellite and said second transmission from said second satellite, said differential time of arrival defining an approximation of said subscriber unit location.

6. A method as recited in claim 5, further comprising the step of:

when said subscriber unit is unable to detect said second transmission from said second satellite, thirdly determining if said subscriber unit can detect a third transmission from a second beam of said first satellite, said second beam being one of said plurality of beams transmitted by said first satellite; and

when said subscriber unit detects said third transmission, generating a differential power level between said first transmission in said current beam and said third transmission in said second beam, both from said first satellite, said differential power level defining an approximation of said subscriber unit location.

7. In a subscriber unit, a method for approximating a transmit time advance offset for use by said subscriber unit in transmitting information to a first satellite, said first satellite having a receive time window wherein said first satellite recognizing said information transmitted by said subscriber unit and said first satellite projecting a plurality of beams upon the earth, said method comprising the steps of:

when said subscriber unit does not possess a current geolocation position of said subscriber unit, receiving in a current beam projected about said subscriber unit a first transmission comprising a first beam identifier and a first beam center, said current beam being one of said plurality of beams projected by said first satellite and said first beam center defining a first geographical coordinate of an approximated center of said current beam;

when said first beam identifier denotes said current beam as being centrally located among said plurality of beams of said first satellite, defining said first beam center as an approximation of a subscriber unit location;

calculating a distance between said first satellite and said subscriber unit, said distance being derived from said subscriber unit location; and

estimating said transmit time advance offset from said distance between said first satellite and said subscriber unit.

8. In a subscriber unit, a method as recited in claim 7, further comprising the step of:

when said subscriber unit possesses said current geolocation position of said subscriber unit, prior to said receiving step, retrieving said current geolocation position for use as said subscriber unit location.

9. In a subscriber unit, a method as recited in claim 8, wherein said current geolocation position was determined using a passive geolocation method.

10. In a subscriber unit, a method as recited in claim 9, wherein said subscriber unit employs global positioning services as said passive geolocation method.

11. In a subscriber unit, a method as recited in claim 8, further comprising the steps of:

when said current beam is not a centrally located beam of said plurality of beams of said first satellite and said subscriber unit does not possess said current geolocation position, said subscriber unit attempting to receive a second transmission from a second satellite; and

when said subscriber unit receives said second transmission from said second satellite, generating a differential time of arrival between said first transmission from said first satellite and said second transmission from said second satellite, said differential time of arrival defining an approximation of said subscriber unit location.

12. In a subscriber unit, a method as recited in claim 11, further comprising the steps of:

when said subscriber unit is unable to detect said second transmission from said second satellite, determining if said subscriber unit can detect a third transmission from a second beam of said first satellite, said second beam being one of said plurality of beams transmitted by said first satellite; and

when said subscriber unit detects said third transmission, generating a differential power level between said first transmission in said current beam and said third transmission in said second beam, both from said first satellite, said differential power level defining an approximation of said subscriber unit location.

13. A subscriber unit for approximating a transmit time advance offset for use by a subscriber unit in transmitting information to a first satellite having a plurality of beams, one of which is a current beam projected about said subscriber unit, said information arriving at said first satellite during a receive window, and said transmit time advance offset corresponding to a propagation delay in said current beam between said subscriber unit and said first satellite, said subscriber unit comprising:

a transceiver for receiving in said current beam a first transmission comprising a first beam identifier and a first beam center, said current beam being one of a plurality of beams projected by said first satellite and said first beam center defining a first geographical coordinate of an approximated center of said current beam said transceiver further employing said transmit time advance offset for transmitting said information to said first satellite during said receive window;

a processor for calculating an approximation of a subscriber unit location, and for estimating said transmit time advance offset from said approximation of said subscriber unit location; and

a memory for storing data that serves as instructions to said processor.

14. A subscriber unit as recited in claim 13, further comprising:

a passive geolocation position locator for generating a current geolocation position for said subscriber unit; and

said memory further comprising a means for storing said current geolocation position as generated by said passive geolocation position locator.

15. A subscriber unit as recited in claim 14, wherein said passive geolocation position locator is a global positioning services type.

16. A subscriber unit as recited in claim 14, further comprising:

said transceiver further comprising a means for receiving a second transmission from a second satellite; and

said processor further comprising a means for generating a differential time of arrival between said first transmission from said first satellite and said second transmission from said second satellite, said differential time of arrival defining an approximation of said subscriber unit location.

17. A subscriber unit as recited in claim 16, further comprising:

said transceiver further comprising a means for receiving a third transmission from a second beam of said first satellite, said second beam being one of said plurality of beams transmitted by said first satellite; and

said processor further comprising a means for generating a differential power level between said first transmission in said current beam and said third transmission in said second beam, both from said first satellite, said differential power level defining an approximation of said subscriber unit location.