Maximum likelihood estimation of G/T of satellite earth terminals using extraterrestrial radio sources

• US 4,684,955 A
• Filed: 11/20/1984
• Issued: 08/04/1987
• Est. Priority Date: 11/20/1984
• Status: Expired due to Term

• Current Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Inventors: Adams, William C. Jr., Patisaul, Charles R.
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Issing, Gregory C.
• Application Number:
  US06/673,412
• Time in Patent Office: 987 Days
• Field of Search: 343/351, 343/352, 343/5 NQ, 364/455, 364/515, 364/516, 364/517, 455/12, 455/25
• US Class Current: 342/351
• CPC Class Codes: G01R 29/10 Radiation diagrams of antennas
• CPC Class Codes: G01R 29/26 Measuring noise figure; Measuring signal-to-noise ratio
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system

Abstract

To measure the figure of merit (G/T) and beam radial pointing error of a satellite earth station multiple Y-factor measurement are taken using a "drift cut" procedure and then these measurements are processed using a maximum likelihood estimate (MLE) algorithm. For carrying out the "drift cut" measurement process, the earth terminal'"'"'s antenna is positioned such that the antenna beam intersects the path of the apparent star motion with a predetermined declination offset and ahead of the current star position. As the star position approaches the stationary antenna beam position, power measurements uniformly spaced in time are recorded. These power measurement "samples" are then divided by the "cold sky" power measurement to obtain corresponding Y-factor measurements. To eliminate the problem of antenna pointing error and star ephemeris error, multiple drift cuts are carried out, each offset in declination by a different amount from the estimate star declination, to produce a matrix of Y-factor values. This matrix of drift cut Y-factors is then processed using a maximum likelihood estimate algorithm, to provide MLE measures of that earth terminal'"'"'s figure of merit and beam radial pointing error.

Claims

1. For use in a communication system, a method of generating an indication from which the figure of merit of receiver equipment employed by said system may be derived comprising the steps of:

(a) directing a signal gathering element of said receiver equipment along the track of a remote signal source and measuring the level of signals received at successive instances in time so a to produce therefrom a matrix of signal level measurements as encompassed by the signal gathering aperture of said signal gathering element;

(b) processing said matrix of signal level measurements produced in step (a) to obtain a matrix of prescribed parameter values arrayed within the beam aperture of said signal gathering elements;

(c) determining the maximum likelihood estimate of the position of the peak prescribed parameter value with said matrix; and

(d) determining the maximum likelihood estimate of the magnitude of the peak prescribed parameter value of said matrix of prescribed parameter values based upon the maximum likelihood estimate of the position of the peak prescribed parameter value determined in step (c).

2. A method according to claim 1, wherein said prescribed parameter corresponds to Y-factor.

3. A method according to claim 1, wherein said signal gathering element comprises a radio wave receiving antenna, said remote signal source comprises an astronomical radio wave source and step (a) comprises directing said antenna at successive positions along the apparent travel track of said astronomical radio wave source such that the beam aperture of said antenna is directed at respectively different declinations relative to said track and, at each of said positions, measuring the level of signals received for successive locations of said astronomical radio wave source along said track within the beam aperture of said antenna, to thereby produce from the measured levels of signals said matrix of signal level measurements.

4. A method according to claim 3, wherein at respective positions for which successive signal level measurements are carried out for successive locations of said astronomical radio source along said track, the effective spacing between adjacent ones of said successive locations is the same.

5. A method according to claim 4, wherein the instances in time, at which said signal level measurements are carried out for the respective different declinations of said antenna, are such that the successive locations of said astronomical radio source along said track as viewed by said beam aperture are readily aligned with one another to form a matrix of effective star track locations within the beam aperture of said antenna.

6. A method according to claim 3, further comprising the step of (e) adjusting said matrix of signal level measurements to compensate for errors in the successive positions at which the beam of said antenna is directed.

7. A method according to claim 3, wherein step (b) includes processing said matrix of signal level measurements in accordance with the size of the beam aperture of said antenna.

8. A method according to claim 3, wherein said prescribed parameter corresponds to Y-factor.

9. A method according to claim 8, further including the step of:

(e) providing a maximum likelihood estimate of antenna boresight pointing error in accordance with the difference between the maximum likelihood estimate of the position of the peak Y-factor value determined in step (c) and its predicted position.

10. For use in a communication system, a method of generating an indication of the pointing error in the operation of a signal gathering element of receiver equipment employed by said system comprising the steps of:

(a) directing a signal gathering element of said receiver equipment along the track of a remote signal source and measuring the level of signals received at successive instances in time so as to produce therefrom a matrix of signal level measurements as encompassed by the signal gathering aperture of said signal gathering element;

(b) processing said matrix of signal level measurements produced in step (a) to obtain a matrix of prescribed parameter values arrayed within the beam aperture of said signal gathering element;

(c) determining the maximum likelihood estimate of the position of the peak prescribed parameter value within said matrix; and

(d) providing a maximum likelihood estimate of said pointing error in accordance with the difference between the maximum likelihood estimate of the position of the peak prescribed parameter value determined in step (c) and its predicted position.

11. A method according to claim 10, wherein said prescribed parameter corresponds to Y-factor.

12. A method according to claim 11, wherein said signal gathering element comprises a radio wave receiving antenna, said remote signal source comprises an astronomical radio wave source and step (a) comprises directing said antenna at successive positions along the apparent travel track of said astronomical radio wave source such that the beam aperture of said antenna is directed at respectively different declinations relative to said track and, at each of said positions, measuring the level of signals received for successive locations of said astronomical radio wave source along said track within the beam aperture of said antenna, to thereby produce from the measured levels of signals said matrix of signal level measurements.

13. A method according to claim 12, wherein step (b) includes processing said matrix of signal level measurements in accordance with the size of the beam aperture of said antenna.

14. For use with a satellite communication system, a method of generating an indication from which the figure of merit, terminal gain-to-terminal system noise temperature, of a satellite earth station may be derived, comprising the steps of:

(a) directing a radio wave receiving antenna of said earth station at successive positions along the apparent motion track of an astronomical radio wave source such that the beam aperture of said antenna is directed at respectively different declinations relative to said track;

(b) at each of said successive positions, measuring the level of signals received by said antenna for sequential locations of said astronomical radio wave source along said track within the confines of the beam aperture of said antenna;

(c) assembling said measured signal levels into a matrix of signal levels, a first coordinate axis of which effectively corresponds to the direction of said track, and a second coordinate axis of which effectively corresponds to the direction of the declination of the beam relative to said track;

(d) processing such matrix of signal levels assembled in step (c) to obtain a matrix of prescribed parameter values effectively arrayed within the beam aperture of said antenna;

(e) determing the maximum likelihood estimate of the position of the peak prescribed parameter value within said matrix; and

(f) determining the maximum, likelihood estimate of the magnitude of the peak prescribed parameter value of said matrix of prescribed parameter values based upon the maximum likelihood estimate of the position of the peak prescribed parameter value determined in step (e).

15. A method according to claim 14, wherein said prescribed parameter corresponds to Y-factor.

16. A method according to claim 14, wherein adjacent ones of the sequential locations of said astronomical radio wave source along said track are effectively equally spaced apart from one another.

17. A method according to claim 14, wherein the instances in time, at which said signal level measurements are carried out for the respective different declinations of said antenna, are such that the successive locations of said astronomical radio source along said track as viewed by said beam aperture are readily aligned with one another to form a matrix of effective star track locations within the beam aperture of said antenna.

18. A method according to claim 14, wherein adjacent ones of the sequential locations of said astronomical radio wave source along said track are effectively equally spaced apart from one another.

19. A method according to claim 18, wherein the instances in time, at which said signal level measurements are carried out for the respective different declinations of said antenna, are such that the successive locations of said astronomical radio source along said track as viewed by said beam aperture are readily aligned with one another to form a matrix of effective star track locations within the beam aperture of said antenna.

20. A method according to claim 14, further comprising the step of (g) adjusting said matrix of signal levels to compensate for errors in the successive positions at which the beam of said antenna is directed.

21. A method according to claim 20, wherein step (d) includes processing said matrix of signal levels in accordance with the size of the beam aperture of said antenna.

22. A method according to claim 15, further including the step of (g) providing a maximum likelihood estimate of antenna boresight pointing error in accordance with the difference between the maximum likelihood estimate of the position of the peak Y-factor value determined in step (e) and its predicted position.