Techniques for determining orbital data

• US 4,912,475 A
• Filed: 03/29/1989
• Issued: 03/27/1990
• Est. Priority Date: 03/20/1987
• Status: Expired due to Fees

• Current Assignee: Massachusetts Institute of Technology
• Original Assignee: Massachusetts Institute of Technology
• Inventors: Counselman, III, Charles C.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): Issing, Gregory C.
• Application Number:
  US07/330,976
• Time in Patent Office: 363 Days
• Field of Search: 342/352, 342/356, 342/357, 342/358, 342/424, 364/459
• US Class Current: 342/352
• CPC Class Codes: G01S 19/02 Details of the space or ground control segments
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method
• CPC Class Codes: G01S 3/48 the waves arriving at the antennas being continuous or intermittent and the phase difference of signals derived therefrom being measured

Abstract

Techniques are disclosed for determining orbital data of space borne vehicles including earth satellites such as those of the NAVSTAR Global Positioning System. Each of a set of such satellites transmits signals which include carrier waves which may be suppressed, or only implicity present. The signals are received from the observable satellites concurrently by means of an antenna at each of at least three ground stations forming a network of baselines. The stations are arrayed such that the ratio of the maximum to the minimum baseline length is much greater than one. From the signals received at a station pair forming each baseline a time series of doubly-differenced phase measurement data is formed which is biased by an integer number of cycles of phase. The data series for different satellite and station pairs are processed together to determine the orbits of the satellites and the doubly-differenced phase biases. Unique determination of the integer values of at least some of the biases is facilitated by the above noted spatial arrangement of the stations such that the ratio of the maximum to the minimum baseline length is much greater than one. This integer bias determination enhances the accuracy of the related orbit determination.

Unique determination of the integer values of at least some of the doubly-differenced carrier phase biases may also be facilitated by the use of a plurality of carrier frequencies with the ratio of the maximum to the minimum frequency being much greater than one.

Claims

1. A method of determining orbital data from doubly differenced phase observations of satellites derived from stations defining a network of baselines, comprising:

(a) arranging the stations to provide a wide ranging progression of baseline lengths, from short to long;

(b) applying observations from a long baseline to enhance observations from a substantially shorter baseline by resolving ambiguity in said short baseline observations;

(c) applying the enhanced observations from the short baseline to enhance observations from a longer baseline by resolving ambiguity in said longer baseline observations; and

(d) applying the enhanced observations to enhance the orbital data determination.

2. The method of claim 1, wherein:

a plurality of said satellites transmit code-modulated, spread-spectrum, suppressed-carrier signals simultaneously on the same frequencies; and

the phase observations are related to a plurality of carrier waves implicit in the signals received at each station and are derived from these signals independently of externally derived knowledge of the information content of the codes modulating these carriers.

3. The method of claim 2, further comprising:

using an upward looking omnidirectional antenna at a station to collect a first composite signal simultaneously including overlapping spread-spectrum signals received from a plurality of satellites;

reconstructing the first composite signal to form a second composite signal simultaneously including a discrete reconstructed carrier component from each of the plurality of satellites;

using Doppler differences to separate reconstructed carrier components corresponding to the same implicit frequency transmitted by different satellites; and

measuring the phases of the separated reconstructed carrier components of a plurality of satellites simultaneously.

4. The method of claim 2, further comprising:

deriving phase observations related to a plurality of implicit carriers having a first frequency and a substantially different second frequency in the transmissions of each satellite, said first and second frequencies being the same for different satellites; and

using phase observations related to the second frequency to enhance observations related to the first frequency by resolving ambiguity in the latter observations.

5. The method of claim 1, further comprising:

arranging the stations to provide a wide ranging progression of baseline projections on two orthogonal axes.

6. The method of claim 1, further comprising:

arranging the stations to provide a geometric progression of baselines.

7. The method of claim 5 or 6, further comprising:

arranging the stations to provide redundant baselines.

8. The method of claim 1, further comprising:

applying modulation delay observations of the satellites to enhance the orbital data determination.

9. The method of claim 8, further comprising:

applying modulation delay observations of the satellites to enhance ambiguity resolution.

10. An improved method of determining orbital data from doubly differenced phase observations of satellites derived from stations defining a network of baselines, wherein the improvement comprises:

(a) arranging the stations to provide a wide ranging progression of baseline lengths, from short to long;

(b) applying observations from a long baseline to enhance observations from a substantially shorter baseline by resolving ambiguity in said short baseline observations;

(c) applying the enhanced observations from the short baseline to enhance observations from a longer baseline by resolving ambiguity in said longer baseline observations; and

(d) applying the enhanced observations from the longer baseline to enhance the orbital data determination.

11. The method of claim 10, wherein:

a plurality of said satellites transmit code-modulated, spread-spectrum, suppressed-carrier signals simultaneously on the same frequencies; and

the phase observations are related to a plurality of carrier waves implicit in the signals received at each station and are derived from these signals independently of externally derived knowledge of the information content of the codes modulating these carriers.

12. The method of claim 11, further comprising:

using an upward looking omnidirectional antenna at a station to collect a first composite signal simultaneously including overlapping spread-spectrum signals received from a plurality of satellites;

reconstructing the first composite signal to form a second composite signal simultaneously including a discrete reconstructed carrier component from each of the plurality of satellites;

using Doppler differences to separate reconstructed carrier components corresponding to the same implicit frequency transmitted by different satellites; and

measuring the phases of the separated reconstructed carrier components of a plurality of satellites simultaneously.

13. The method of claim 11, additionally comprising:

deriving phase observations related to a plurality of implicit carriers having a first frequency and a substantially different second frequency in the transmissions of each satellite, said first and second frequencies being the same for different satellites; and

using phase observations related to the second frequency to enhance observations related to the first frequency by resolving ambiguity in the latter observations.

14. The method of claim 10, further comprising:

arranging the stations to provide a wide ranging progression of baseline projections on two orthogonal axes.

15. The method of claim 10, further comprising:

arranging the stations to provide a geometric progression of baselines.

16. The method of claim 14 or 15, further comprising:

arranging the stations to provide redundant baselines.

17. The method of claim 10, further comprising:

applying modulation delay observations of the satellites to enhance the orbital data determination.

18. The method of claim 17, further comprising:

applying modulation delay observations of the satellites to enhance ambiguity resolution.