RF link control of satellite clocks

• US 5,506,781 A
• Filed: 06/03/1994
• Issued: 04/09/1996
• Est. Priority Date: 06/03/1994
• Status: Expired due to Term

• Current Assignee: Exelis Incorporated (L3Harris Technologies, Inc.)
• Original Assignee: ITT Corporation (ITT, Inc.)
• Inventors: Doyle, Lawrence J., Epstein, Marvin A., Cummiskey, Peter
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): FREJD, RUSSELL WARREN
• Application Number:
  US08/253,722
• Time in Patent Office: 676 Days
• Field of Search: 364/459, 364/449, 364/454, 364/569, 343/112 R, 343/6 R, 342/433, 342/353, 342/357, 342/358, 342/352, 342/356, 342/463, 375/1, 455/10
• US Class Current: 701/226
• CPC Class Codes: H04B 7/2125 Synchronisation

Abstract

A system and method for maintaining a precise time standard among a system of orbiting satellites is disclosed. In an illustrative embodiment, atomic clock data is circulated among the satellites via RF crosslinks. Each satellite uses the received data as input to a Kalman process which acts to minimize the mean squared error among the satellite clocks to form a set of "ensemble clocks". The resulting ensemble clock values are then transmitted to an earth station where an offset between the ensemble clocks and Universal Time is computed. The offset is transmitted from the earth station to the satellites where it is used by the satellites to lock their on-board clocks to Universal Time, thereby creating a corrected system time. The corrected system time is transmitted, via RF crosslinks, to satellites not having operational on-board clocks. The satellites without atomic clocks employ phase locked loops to anchor their clocks to the corrected system time as it is received over the crosslinks.

Claims

1. A method for maintaining a time standard among a plurality of orbiting satellites, each of said satellites including at least one timing reference, comprising the steps of:

crosslinking said satellites with communication crosslinks in order that said satellites can communicate with each other;

transmitting timing reference data across said communication crosslinks to communicate said data among said satellites, said satellites processing said timing reference data in a predetermined manner to produce a set of ensemble timing references at said satellites, whereby the deviation among said ensemble timing references is less than the deviation among said timing references;

transmitting said ensemble timing references from said satellites to a location where a time standard is maintained;

deriving an offset between said transmitted ensemble timing references and said time standard;

transmitting said offset from said location to said satellites, wherein only a predetermined number of said satellites receive said offset from said location;

transmitting said offset, received by said predetermined number of said satellites said satellites, across said communication cross links to said satellites which did not receive said offset from said location; and

using said offset to lock said ensemble timing references to said time standard, thereby creating a corrected system time.

2. The method according to claim 1, wherein said predetermined manner comprises the steps of:

running a Kalman process at each of said satellites to generate a plurality of local phase offsets, one at each of said satellites; and

adding each of said local phase offsets to its respective timing reference to derive an ensemble timing reference for each of said satellites.

3. The method according to claim 1, wherein said transmission from each of said satellites to said location is achieved by way of radio frequency transmission using L band frequencies.

4. The method according to claim 1, wherein said transmission from said location to said satellites is achieved by way of radio frequency transmission using S band frequencies.

5. The method according to claim 1, wherein the step of using said offset to lock said ensemble timing references to said time standard, comprises the steps of:

filtering said offset to obtain a steering signal; and

using said steering signal and said ensemble timing references as input to a Kalman process that functions to anchor said ensemble timing references to said time standard.

6. A method for maintaining a time standard among a plurality of orbiting satellites, said plurality of orbiting satellites comprising a first set of satellites, wherein each satellite includes at least one timing reference, and a second set of satellites, wherein each satellite includes a timing means, comprising the steps of:

crosslinking said first set of satellites, said second set of satellites, and said first and second set of satellites, with communication crosslinks in order that said satellites can communicate with each other;

transmitting timing reference data across said communication crosslinks to communicate said data among said first set of satellites and processing said timing reference data in a predetermined manner to produce a set of ensemble timing references for said first set of satellites, whereby the deviation among said ensemble timing references is less than the deviation among said timing references of said first set of satellites;

transmitting said ensemble timing references from said first set of satellites to a location where a time standard is maintained;

deriving an offset between said transmitted ensemble timing references and said time standard;

transmitting said offset from said location to said first set of satellites, wherein only a predetermined number of said first set of satellites receive said offset from said location;

transmitting said offset, received by said predetermined number of said first set of satellites, across said communication crosslinks to said first set of satellites which did not receive said offset from said location;

using said offset to lock said ensemble timing references of said first set of satellites to said time standard, thereby creating a corrected system time;

providing a phase locked loop in each satellite of said second set of satellites;

transmitting said corrected system time across said communication crosslinks from said first set of satellites to each satellite of said second set of satellites; and

using said corrected system time in combination with said phase locked loops to lock said timing means of said second set of satellites to said corrected system time.

7. The method according to claim 6, wherein said predetermined manner comprises the steps of:

running a Kalman process at each of said first set of satellites to generate a plurality of local phase offsets, one at each satellite of said first set of satellites; and

adding each of said local phase offsets to its respective timing reference to derive an ensemble timing reference for each satellite of said first set of satellites.

8. The method according to claim 6, wherein said transmission from said first set of satellites to said location is achieved by way of radio frequency transmission using L band frequencies.

9. The method according to claim 6, wherein said transmission from said location to said first set of satellites is achieved by way of radio frequency transmissions using S band frequencies.

10. The method according to claim 6, wherein said step of using said offset to lock said ensemble timing references to said time standard, comprises the steps of:

filtering said offset to obtain a steering signal; and

using said steering signal and said ensemble timing references as input to a Kalman process that functions to anchor said ensemble timing references to said time standard.

11. An RF Link Control apparatus for maintaining a time standard among a plurality of orbiting satellites, each of said satellites including at least one timing reference, comprising:

means for computing an ensemble timing reference at each of said satellites, whereby the deviation among said ensemble timing references is less than the deviation among said timing references;

means for transmitting said ensemble timing references from said satellites to a location where a time standard is maintained, said ensemble timing references to be used at said location to derive an offset between said ensemble timing references and said time standard;

means for transmitting said offset from said location to said satellites;

means for generating a steering signal from said offset, said steering signal to be used at said satellites to lock said ensemble timing references to said time standard, thereby creating a corrected system time; and

a plurality of communication crosslinks between said satellites for transferring timing reference data among said satellites.

12. An RF Link Control apparatus according to claim 11, wherein said means for computing an ensemble timing reference at each of said satellites comprises:

a processor associated with each said satellite, said processor operating to implement a Kalman algorithm for computing a phase offset between timing reference data received over said communication crosslinks and a receiving satellite'"'"'s time reference, said phase offset to be added to said receiving satellite'"'"'s timing reference to generate said ensemble timing reference.

13. An RF Link Control apparatus according to claim 11, wherein said means for transmitting said ensemble timing references from said satellites to a location where a time standard is maintained, comprises:

an L band transmitter associated with each of said satellites; and

an L band receiver at said location.

14. An RF Link Control apparatus according to claim 11, wherein said means for transmitting said offset from said location to said satellites comprises:

an S band transmitter at said location; and

an S band receiver associated with each of said satellites.

15. An RF Link Control apparatus according to claim 11, wherein said means for generating a steering signal from said offset comprises:

a steering filter associated with each of said satellites for filtering said offset to create a filtered offset; and

a processor associated with each of said satellites, said processor operating to lock said ensemble timing references to said time standard through implementation of a Kalman algorithm.

16. An RF Link Control apparatus for maintaining a time standard among a plurality of orbiting satellites, said plurality of orbiting satellites comprising a first set of satellites, wherein each satellite includes at least one timing reference, and a second set of satellites, wherein each satellite includes at least one timing means, comprising:

means for computing an ensemble timing reference at each satellite of said first set of satellites, the deviation among said ensemble timing references is less than the deviation among said timing references;

means for transmitting said ensemble timing references from each satellite of said first set of satellites to a location where a time standard is maintained, said ensemble timing references to be used at said location to derive an offset between said ensemble timing references and said time standard;

means for transmitting said offset from said location to said first set of satellites;

means for generating a steering signal from said offset, said steering signal to be used at said first set of satellites to lock said ensemble timing references to said time standard, thereby creating a corrected system time;

a first plurality of communication crosslinks between said satellites of said first set, a second plurality of communication crosslinks between said satellites of second set and a third plurality of communication crosslinks between said first and second sets of said satellites, for transferring timing reference data among said satellites; and

means for locking said timing means of said second set of satellites to said corrected system time.

17. An RF Link Control apparatus according to claim 16, wherein said means for locking said timing means of said second set of satellites to said corrected system time comprises:

a phase locked loop associated with each satellite of said second set of satellites; and

means for transmitting said corrected system time from said first set of satellites to each satellite of said second set of satellites such that the system accuracy is not significantly degraded as compared to a constellation consisting soley of said first set of satellites.

18. An RF Link Control apparatus according to claim 17, wherein said phase locked loop comprises:

a phase meter;

a second order estimator; and

a voltage controlled oscillator.

19. An RF Link Control apparatus according to claim 18, wherein said second order estimator comprises:

a smoothing circuit for removing high frequency noise from a signal input to said second order estimator;

a drift compensation circuit that operates to compensate for frequency drift in said voltage controlled oscillator; and

an estimator circuit for generating a signal for use as input to said voltage controlled oscillator.

20. An RF Link Control apparatus according to claim 19, wherein said voltage controlled oscillator further comprises a phase table in which the output phase of said oscillator may be stored.