Super short baseline navigation using phase-delay processing of spread-spectrum-coded reply signals

• US 5,659,520 A
• Filed: 04/24/1995
• Issued: 08/19/1997
• Est. Priority Date: 04/24/1995
• Status: Expired due to Fees

• Current Assignee: Channel Technologies Group, LLC
• Original Assignee: Sonatech, Inc. (Channel Technologies Group, LLC)
• Inventors: Douglas, Bretton Lee, Loggins, Chester DeWitt Jr., Cyr, Reginald John, Norris, Donald Owen Jr., Wapner, Michael Paul, Watson, Marvin Lee
• Primary Examiner(s): Lobo, Ian J.
• Application Number:
  US08/426,957
• Time in Patent Office: 848 Days
• Field of Search: 367/6, 367/99, 367/118, 367/123, 367/124, 367/125, 367/127, 367/129, 342/146
• US Class Current: 367/125
• CPC Class Codes: G01S 15/74 Systems using reradiation of acoustic waves, e.g. IFF, i.e. identification of friend or foe
• CPC Class Codes: G01S 15/874 Combination of several spaced transponders or reflectors of known location for determining the position of a receiver G01S15/872 takes precedence
• CPC Class Codes: G01S 3/8083 determining direction of source
• CPC Class Codes: G01S 3/86 with means for eliminating undesired waves, e.g. disturbing noises
• CPC Class Codes: G01S 5/24 Position of single direction-finder fixed by determining direction of a plurality of spaced sources of known location

Abstract

A short baseline navigation system employs the real-time estimation of the positions of multiple cooperative targets. Each target replies with a unique stepped frequency sequence signal that covers the usable frequency band. A processor operates on reply signals received by elements on the tracking platform and develops a coarse time-difference-of-arrival estimate using an algorithm derived herein. The processor also estimates the Doppler shift of received signals, and determines a time-window (or gating) that eliminates the portions of the received signals corrupted by multipath interference. The relative phase differences between the received signals are then used in conjunction with the coarse time-difference-of-arrival estimates for a precise direction-of-arrival estimation.

Claims

1. A navigation system employing real-time estimation of the positions of multiple cooperative targets, comprising:

transmitter means for transmitting an interrogation signal for detection by a plurality of transponders or responders each of which, responsive to detection of the interrogation signal, transmits a reply signal having at least one continuous wave frequency component;

first receiver means comprising a plurality of receiving elements spaced apart a distance in the range of 0.5 to 10 wavelengths of the lowest frequency component of the reply signals, said first receiver means comprising direction-of-arrival measurement means including means for measuring the phase difference of the received reply signal between each pair of receiving elements and producing direction-of-arrival estimates, whereby said first receiver means includes spectral and spatial means to resolve ambiguities;

second receiver means for the measurement of round-trip travel times providing distance-to-target estimates for each target; and

computer means for collecting the outputs to said first and second receiver means for determining the position of each target relative to said receiving elements.

2. The navigation system as claimed in claim 1, wherein said direction-of-arrival measurement means produces a fine time-difference-of-arrival estimate which is ambiguous only by an integral number of time periods of the reply signal frequency component being received, and said first receiver means further comprises:

means for producing a coarse time-difference-of-arrival estimate using time-of-arrival estimates as between pairs of receiving elements;

means for comparing said coarse and fine time-difference-of-arrival estimates and determining the number of said time periods in the difference therebetween; and

means for correcting said fine time-difference-of-arrival ambiguity by said number of said time periods in said difference.

3. The navigation system as claimed in claim 2, wherein the reply signal from each transponder or responder includes a series of spaced bursts of continuous wave frequencies, each burst in said series being of a frequency different than all other bursts in the series, and wherein said means for producing a coarse time-difference-of-arrival estimate comprises means for cross-correlating the series of spaced bursts in each reply signal.

4. The navigation system as claimed in claim 3, wherein said first receiver means includes a plurality of narrowband filters for processing separately each said burst of continuous wave frequency.

5. The navigation system as claimed in claim 3, wherein the bursts of continuous wave frequencies in the series of bursts from each transponder or responder are transmitted in a sequential order different from the bursts in the other transponders or responders, and wherein said first receiver means comprises burst sequence detection means for uniquely identifying the series of bursts of continuous wave frequencies from each transponder or responder.

6. The navigation system as claimed in claim 5, wherein the first burst of continuous wave frequency transmitted by each transponder or responder, responsive to receiving an interrogation signal, is common with that of all other transponders or responders and defines a lead burst for each series of bursts.

7. The navigation system as claimed in claim 1, wherein said first receiver means comprises three said receiving elements spaced apart a distance in the range of 0.5 to 10 wavelengths of the lowest frequency components of the reply signals and arranged in an equilateral triangle configuration.

8. The navigation system as claimed in claim 1, wherein:

each transponder or responder transmits a reply signal comprised of a series of gated continuous wave pulses of different frequencies;

said first receiver means includes means for cross-correlating the received series of pulses for each pair of receiving elements, to form a coarse time-difference-of-arrival estimate; and

said direction-of-arrival measurement means produces a fine time-difference-of-arrival estimate which is ambiguous only by an integral number of time periods of the continuous wave pulse being received;

said fine time-difference-of-arrival estimate and said coarse time-difference-of-arrival estimate are processed to produce precise target time-difference-of-arrival information.

9. The navigation system as claimed in claim 6, wherein said first receiver means comprises a common-frequency burst detector for identifying the lead burst in each said series which is at a frequency common with the lead burst frequency of all other transponders or responders.

10. The navigation system as claimed in claim 9, wherein said common-frequency burst detector comprises:

a narrowband receiver channel tuned to the frequency of the lead bursts;

a wideband receiver channel tuned to the frequency of the lead bursts;

an envelope detector in each of said channels; and

a comparator for comparing the outputs of said envelope detectors, said comparator providing an output only when the magnitude of the output of said narrowband channel exceeds a predetermined fraction of that of said wideband channel, thereby indicating the presence of a lead burst.

11. The navigation system as claimed in claim 10, wherein said predetermined fraction is in the range of 0.6/1 to 1/1.

12. The navigation system as claimed in claim 3, wherein said first receiver means comprises frequency estimator means for determining the frequency of each burst in the series of received bursts, said frequency estimator means comprises:

a time-window for selecting a time window of data from a frequency burst in said series of bursts;

a converter for converting the selected time window of data to frequency domain data using a fast Fourier transform;

means for squaring the magnitude of the frequency domain data to obtain an estimate of the frequency spectrum of the selected burst;

a peak detector for fitting a parabola function to three values in the frequency spectrum, the maximum value and two neighboring values; and

means for identifying the peak in the parabola as the maximum of the frequency spectrum and corresponding to the estimated frequency for the selected burst.

13. The navigation system as claimed in claim 1, wherein said first receiver means comprises direct/indirect path detection means for distinguishing direct path signals directly from a transponder or responder and indirect path signals which are received from a transponder or responder from along a path which is not direct from the transponder or responder, said direct/indirect path detection means comprising:

means for detecting an abrupt phase difference between reply signals received by two different receiving elements; and

a threshold detector for providing an output upon detection of said abrupt phase difference between reply signals received by said two different receiving elements, indicating the arrival of the indirect path signal.