Method and system for determining position from signals from satellites

• US 4,870,422 A
• Filed: 08/11/1986
• Issued: 09/26/1989
• Est. Priority Date: 03/01/1982
• Status: Expired due to Term

• Current Assignee: Western Atlas International Incorporated (Northrop Grumman Corporation)
• Original Assignee: Western Atlas International Incorporated (Northrop Grumman Corporation)
• Inventors: Counselman, III, Charles C.
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Sotomayor, John B.
• Application Number:
  US06/895,148
• Time in Patent Office: 1,142 Days
• Field of Search: 342/357, 342/352, 342/450, 342/451, 375/1, 370/104, 370/121
• US Class Current: 342/357.26
• CPC Class Codes: G01C 15/00 Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00
• CPC Class Codes: G01S 19/35 Constructional details or hardware or software details of the signal processing chain
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method

Abstract

A method and a system are disclosed for measuring the baseline vector b between a pair of survey marks on the ground by radio interferometry using radio signals broadcast from the earth orbiting satellites of the NAVSTAR Global Positioning System (GPS), the radio signals broadcast by the satellites being double-sideband modulated with their carriers suppressed. An antenna is positioned at each survey mark. The signals received by one antenna during a predetermined time span are separated into upper and lower sideband components. These separate components are filtered, converted to digital form, and then multiplied together. Their product is analyzed digitally by means of correlation with quadrature outputs of a local oscillator to determine the power, and the phase relative to that local oscillator, of the carrier wave that is implicit in the double-sideband signal being received from each satellite. Differences in Doppler shift are utilized to distinguish the carriers of different satellites. The signals received at the same time by the other antenna are processed in the same manner. Thus, the powers and carrier phases of the signals from a plurality of satellites are measured simultaneously and numerical data representing the measurement results are obtained at each survey mark. The measurements are performed in real time at each mark without reference to signals that are received at any other place and without knowledge of any of the coded signals that modulate the GPS carriers. The data from the measurements performed simultaneously but independently at the two survey marks, once per second for a predetermined time span, are then processed together to determine the baseline vector that extends from one mark to the other. Two methods of processing are disclosed. In either method, an "ambiguity function", is computed which is a function of the measurement data and of a trial value b of the baseline vector. The vector space of b is systematically searched to find the unique value of b that maximizes the computed function. This value of b is taken to be the desired determination of b. By using signals from a plurality of five satellites and a time span of about 5000 seconds, a baseline vector determination can be obtained by the method of the present invention with an accuracy of about 5 millimeters in each coordinate for a baseline length of about 100 meters.

Claims

1. The method of deriving position related data, related to signals modulated by mutually orthogonal codes, from overlapping spread spectrum signals transmitted concurrently with the same frequencies by each of a plurality of satellites, the data being derived independently of externally derived knowledge of the information content of the related modulating codes, comprising:

receiving from the satellites a first composite of the overlapping spread spectrum signals with an upward looking, omnidirectional antenna positioned at a first mark;

reconstructing the first composite of spread spectrum signals to form a second composite simultaneously including a plurality of reconstructed components related to the code modulated signals implicit in the signals received from the satellites; and

applying predictions of the frequency histories of the signals from the satellites to the second composite to derive said position related data therefrom.

2. The method of claim 1 wherein the data derived are related to the signals transmitted by a selected satellite.

3. The method of claim 1 wherein the data derived are related to signals transmitted by a plurality of the satellites.

4. The method of claim 1, further comprising:

deriving at a second mark data related to signals concurrently transmitted by the plurality of satellites; and

processing the data from both marks to determine relative position.

5. The method of claim 1 wherein the reconstructed components have discrete frequencies and phases related to the frequencies and phases of the code modulated signals.

6. The method of claim 1 wherein the reconstruction step further comprises:

applying a phase and frequency doubling non-linearity to the composite of spread spectrum signals to form the composite of reconstructed components.

7. The method of claim 1 wherein the reconstruction step further comprises:

separating the received signals into first and second components representing substantially different spectral portions thereof; and

correlating the spectral portions to generate the composite of reconstructed components.

8. The method of claim 7 wherein the spectral component separation step separates the received signals into upper and lower sidebands of a center frequency carrier implicit therein.

9. The method of claim 7 wherein the correlating step further comprises:

generating a first binary signal representing the time varying sign of the first spectral component;

generating a second binary signal representing the time varying sign of the second spectral component; and

correlating the first and second binary signals to form the composite of reconstructed components.

10. The method of claim 1 wherein the predicted frequency history step further comprises:

generating a signal whose frequency is proportional to an estimate of the frequency of a satellite signal as received; and

combining the estimate signal with the reconstructed components to separate the component related thereto.

11. The method of claim 10 wherein the predicted frequency history step further comprises:

varying the frequency of the estimate signal to track the frequency of the satellite signals as received.

12. The method of claim 6 wherein the predicted frequency history step further comprises:

generating a predicted signal based on a prediction, made before the first composite is collected, of the Doppler shift of the signals from a selected satellite as received at the first mark; and

correlating the predicted signal with the reconstructed components to separate the reconstructed component whose frequency and phase are related to the frequency and phase of the selected code modulated signal.

13. The method of claim 12 wherein the phase data deriving step, further comprises:

varying the frequency of the predicted signal during the correlation step to maximize the separation of the related component.

14. The method of claim 1 wherein the data deriving step further comprises:

generating a series of signals whose frequencies are related to estimates of the frequencies of selected code modulated signals implicit in the signals received from the satellites; and

combining each of the series of estimate signals with the composite of reconstructed components to separate the components related to each code modulated signal.

15. The method of claim 14 wherein the estimate signal generating step further comprises:

varying the frequencies of the series of estimate signals to track the frequencies of the components.

16. The method of claim 1 further comprising the following step before the reconstructing step:

filtering the first composite signal to reject signals received in a narrow band at the frequency of the implicit code modulated signals.

17. The method of claim 16 wherein the rejected frequency band includes the possible range of Doppler shifted frequencies of the implicit code modulated signals.

18. The system for deriving position related data, related to signals modulated by mutually orthogonal codes, from overlapping spread spectrum signals transmitted concurrently with the same frequencies by each of a plurality of satellites, the data being derived independently of externally derived knowledge of the information content of the related modulating codes, comprising:

an upward looking, omni-directional antenna positioned at a first mark for receiving from the satellites a first composite of the overlapping spread spectrum signals;

means for reconstructing the first composite of spread spectrum signals to form a second composite simultaneously including a plurality of reconstructed components related to the code modulated signals implicit in the signals received from the satellites; and

means for applying predictions of the frequency histories of the signals from the satellites to the second composite to derive said position related data therefrom.

19. The system of claim 18 wherein the data derived are related to the signals transmitted by a selected satellite.

20. The system of claim 18 wherein the data derived are related to signals transmitted by a plurality of the satellites.

21. The system of claim 18, further comprising:

means for deriving data at a second mark related to signals concurrently transmitted by the plurality of satellites; and

data processing means for determining relative position from the data from both marks.

22. The system of claim 18 wherein the reconstructed components have discrete frequencies and phases related to the frequencies and phases of the code modulated signals.

23. The system of claim 18 wherein the reconstruction means further comprises:

means for doubling the phase and frequency of the first composite signal to form the second composite signal.

24. The system of claim 18 wherein the reconstruction means further comprises:

means for separating the spread spectrum signals into first and second components representing substantially different spectral portions thereof; and

a correlator for correlating the spectral portions to generate the composite of reconstructed components.

25. The system of claim 24 wherein the separating means separates the spread spectrum signals into upper and lower sidebands of a center frequency carrier implicit therein.

26. The system of claim 24 wherein the correlating step further comprises:

means for generating a first binary signal representing the time varying sign of the first spectral component;

means for generating a second binary signal representing the time varying sign of the second spectral component; and

a correlator for correlating the first and second binary signals to form the composite of reconstructed components.

27. The system of claim 18 wherein the means for applying the predicted frequency history further comprises:

means for generating a signal whose frequency is proportional to an estimate of the frequency of a satellite signal as received; and

means for combining the estimate signal with the reconstructed components to separate the component related thereto.

28. The system of claim 27 wherein the means for applying the predicted frequency history further comprises:

means for varying the frequency of the estimate signal to track the frequency of the satellite signals as received.

29. The system of claim 23 wherein the means for applying the predicted frequency history further comprises:

means for generating a predicted signal based on a prediction, made before the first composite is collected, of the Doppler shift of the signals from a selected satellite as received at the first mark; and

means for correlating the predicted signal with the reconstructed components to separate the reconstructed component whose frequency and phase are related to the frequency and phase of the selected code modulated signal.

30. The system of claim 29 wherein the means for applying the predicted frequency history further comprises:

means for varying the frequency of the predicted signal during the correlation step to maximize the separation of the related component.

31. The system of claim 18 wherein the means for applying the predicted frequency history further comprises:

means for generating a series of signals whose frequencies are related to estimates of the frequencies of selected code modulated signals implicit in the signals received from the satellites; and

means for combining each of the series of estimate signals with the composite of reconstructed components to separate the components related to each code modulated signal.

32. The system of claim 31 wherein the estimate generating means further comprises:

means for varying the frequencies of the series of estimate signals to track the frequencies of the components.

33. The system of claim 18 further comprising;

means for filtering the first composite signal to reject signals received in a narrow band at the frequency of the implicit code modulated signals.

34. The system of claim 33 wherein the rejected frequency band includes the possible range of Doppler shifted frequencies of the implicit code modulated signals.

35. A GPS receiver for determining a baseline vector between two marks, comprising:

an antenna at a first mark for receiving overlapping, carrier suppressed L band signals concurrently transmitted at the same nominal frequencies by each of a plurality of NAVSTAR satellites;

a sideband separator for separating the received signals into upper and lower sidebands of the suppressed L band carriers;

a correlator for cross-correlating the separated sidebands to form a composite of reconstructed suppressed carriers;

a plurality of satellite tracking channels responsive to the composite of suppressed carriers for determining the phases of reconstructed suppressed carriers related to selected satellites;

means for determining the phases of reconstructed carriers from signals concurrently received from the selected satellites at a second mark; and

means for computing the baseline vector between the marks from the reconstructed carrier phases so determined.

36. The GPS receiver claimed in claim 35 wherein the satellite tracking channels further comprise:

a numerical oscillator for generating signals whose time varying frequencies represent predictions of the Doppler shifted frequencies of the signals received from a selected satellite;

a correlator for cross-correlating the signals from the numerical oscillator and the composite of reconstructed carriers to select therefrom the reconstructed carrier related to the selected satellite; and

a phase detector for determining the time varying phase of the selected reconstructed carrier.

37. The GPS receiver claimed in claimed in claims 35 or 36 wherein the sideband separator further comprises:

an RF power splitter for splitting the received signals into two identical RF signals;

a quadrature hybrid for generating a pair of local oscillator output signals in phase quadrature at the nominal frequency of the suppressed carriers;

a pair of doubly balanced mixers for down-converting the identical RF signals to baseband in response to the in phase quadrature local oscillator signals; and

a quadrature hybrid for phase shifting the down-converted RF signals and adding and subtracting the phase shifted results to separate the sidebands.

38. The GPS receiver claimed in claim 37 wherein the correlator further comprises:

a pair of one bit clippers for generating first and second binary signals representing the time varying signs of the sidebands.

39. A method of determining a baseline vector between two marks from overlapping, carrier suppressed L band signals concurrently transmitted at the same nominal frequencies by each of a plurality of NAVSTAR satellites and received at the marks, comprising the steps of;

separating the signals received at each mark into upper and lower sidebands of the suppressed L band carriers;

cross-correlating the separated sidebands to form a composite of reconstructed suppressed carriers related to each mark;

determining the phases of reconstructed suppressed carriers at each mark related to a plurality of selected satellites; and

computing the baseline vector between the marks from the reconstructed carrier phases so determined.

40. The method claimed in claim 39 wherein the phase determining step further comprises:

generating signals whose time varying frequencies represent predictions of the Doppler shifted frequencies of the signals received from selected satellites;

cross-correlating the predicted signals with the composite of reconstructed carriers to select therefrom the reconstructed carriers related to selected satellites; and

determining the time varying phases of the reconstructed carriers so selected.

41. The method claimed in claimed in claims 39 or 40 wherein the sideband separating step further comprises:

splitting the received signals into two identical RF signals;

generating a pair of local oscillator output signals in phase quadrature at the nominal frequency of the suppressed carriers;

down-converting the identical RF signals to baseband in response to the in phase quadrature local oscillator signals;

phase shifting the down-converted RF signals; and

adding and subtracting the phase shifted results to separate the sidebands.

42. The method claimed in claim 41 wherein the sideband cross-correlation step further comprises:

clipping the sideband signals to form first and second binary signals representing the time varying signs of the sidebands.