초록 ▼

Systems and methods for determining and disambiguating the location of the shooter of supersonic projectiles based on shockwave-only signals are described. Using several spaced sensors, an initial portion of the shockwave-only signals is sensed to determine Time-Differences-Of-Arrival (TDOA) for the

Systems and methods for determining and disambiguating the location of the shooter of supersonic projectiles based on shockwave-only signals are described. Using several spaced sensors, an initial portion of the shockwave-only signals is sensed to determine Time-Differences-Of-Arrival (TDOA) for the sensor pairs. The resulting TDOAs are used to determine the gradient of curvature of the shockwave wavefront on the sensors. The gradient of curvature is then used to determine the disambiguated projectile trajectory.

대표청구항 ▼

What is claimed is: 1. A method for disambiguating from shockwave-only signals a trajectory of a projectile producing a shockwave wavefront, comprising: measuring at least an initial portion of the shockwave-only signals with a plurality of spaced acoustic sensors forming an antenna; determining fr

What is claimed is: 1. A method for disambiguating from shockwave-only signals a trajectory of a projectile producing a shockwave wavefront, comprising: measuring at least an initial portion of the shockwave-only signals with a plurality of spaced acoustic sensors forming an antenna; determining from the measured portion of the shockwave-only signals Time-Difference-Of-Arrival (TDOA) values for sensor pairs with an accuracy sufficient to determine a gradient of curvature of the shockwave wavefront across the antenna; determining the gradient of curvature of the shockwave wavefront; and determining from the determined gradient of curvature the disambiguated projectile trajectory. 2. The method of claim 1, wherein the accuracy sufficient to determine the gradient of curvature depends on a size of the antenna. 3. The method of claim 1, wherein the accuracy sufficient to determine the gradient of curvature depends on a spatial distribution of sensor locations. 4. The method of claim 1, wherein measuring the initial portion of the shockwave-only signals includes measuring acoustic energy of a received signal and excluding the received signal from being a shockwave-only signal if the acoustic energy of the received has less than a predetermined threshold value over a predetermined frequency band. 5. The method of claim 4, wherein the predetermined frequency band comprises frequencies between approximately 700 Hz and 10 kHz. 6. The method of claim 1, wherein measuring the initial portion of the shockwave-only signals includes measuring a time interval where a received signal has a positive value and excluding the received signal from being a shockwave-only signal if the time interval is less than a minimum time or greater than a maximum time. 7. The method of claim 6, wherein the minimum time is approximately 70 μs and the maximum time is approximately 300 μs. 8. The method of claim 1, wherein determining the Time-Differences-Of-Arrival (TDOA) values for sensor pairs comprises designating a sensor of the plurality of sensors that first encounters the shockwave wavefront as a reference sensor; setting a first latch of a timing circuit when an amplitude of the initial portion of the shockwave-only signal at the reference sensor crosses a threshold value, said first latch activating counters for each of the other sensors; and stopping the counters in each of the other sensors when the respective other sensors encounter the shockwave wavefront; wherein a count between start and stop of the counters represents the TDOA between the other sensors and the reference sensor. 9. The method of claim 1, wherein determining the Time-Differences-Of-Arrival (TDOA) values for sensor pairs comprises measuring at least the initial portion of the shockwave-only signals at the acoustic sensors with a first clock rate; correlating the measured portions between the acoustic sensors with a second clock rate greater than the first clock rate; and determining a Time-Difference-Of-Arrival (TDOA) from a time shift producing a maximum value of the correlation. 10. The method of claim 9, and further computing from the correlated portions a residual for each sensor and selecting the smallest residual as producing optimum TDOA values. 11. A method for disambiguating a trajectory of a supersonic projectile from shockwave-only signals with an antenna having a plurality of acoustic sensors, comprising: detecting shockwave-only signals at the plurality of acoustic sensors; determining from a correlation between the shockwave-only signals detected at the plurality of sensors Time-Difference-Of-Arrival (TDOA) values for sensor pairs; for an expected closest distance between a projectile trajectory and the antenna, determining if a precision of the Time-Difference-Of-Arrival (TDOA) values is adequate for determining a gradient of curvature of a shockwave wavefront across the antenna; determining the gradient of curvature of the shockwave wavefront; and determining the disambiguated projectile trajectory from the gradient of curvature. 12. The method of claim 11, wherein the correlation is performed with a timing resolution which is greater than a timing resolution used to measure the portion of the shockwave-only signals. 13. The method of claim 11, wherein detecting shockwave-only signals comprises measuring at least an initial portion of a received shockwave-only signals, measuring acoustic energy of the received signal, and excluding the received signal from being a shockwave-only signal if the acoustic energy of the received has less than a predetermined threshold value over a predetermined frequency band. 14. The method of claim 11, wherein detecting shockwave-only signals comprises measuring at least an initial portion of a received shockwave-only signals, measuring a time interval where a received signal has a positive value, and excluding the received signal from being a shockwave-only signal if the time interval is less than a minimum time or greater than a maximum time. 15. The method of claim 11, wherein detecting shockwave-only signals comprises eliminating detected signal not originating from a shockwave. 16. The method of claim 15, wherein a detected signal is deemed to be a shockwave-only signal if it satisfies all of the following criteria: (a) the detected signal has a minimum and a maximum peak signal amplitude, with at least the minimum peak signal amplitude exceeding a predetermined threshold value; (b) the detected signal has a sharp transient from zero to the maximum peak signal amplitude, without being preceded by another signal with a value that is not significantly smaller than the peak signal value; (c) a time between the minimum and maximum peak signal amplitudes of the detected signal is greater than a predetermined time interval; (d) a magnitude of the minimum peak signal amplitude is substantially identical to the maximum peak signal amplitude; (e) the detected signal has a sharp transient from the minimum peak signal amplitude to zero; and (f) a time between the maximum peak signal amplitude and a zero-crossing between the maximum peak signal amplitude and the minimum peak signal amplitude, and between the zero-crossing and the minimum peak signal amplitude are substantially identical. 17. A system for disambiguating a trajectory of a supersonic projectile from shockwave-only signals, comprising: an antenna having a plurality of acoustic sensors; and a processor configured to receive signals at the acoustic sensors and determine if the received signals are shockwave-only signals; perform a correlation between the shockwave-only signals; determine from the correlation Time-Difference-Of-Arrival (TDOA) values for sensor pairs; determine for an expected closest distance between a projectile trajectory and the antenna, if a precision of the Time-Difference-Of-Arrival (TDOA) values is adequate for determining a gradient of curvature of a shockwave wavefront across the antenna; determine the gradient of curvature of the shockwave wavefront; and determine the disambiguated projectile trajectory from the gradient of curvature. 18. The system of claim 17, wherein the antenna is mounted on a vehicle. 19. The system of claim 17, wherein the antenna comprises a frame and elastomeric couplings attached to the frame, with the elastomeric couplings holding the acoustic sensors. 20. The system of claim 19, wherein the acoustic sensors having a mechanical resonance frequency of less than approximately 1 Hz.