Methods and apparatus for determining the trajectory of a supersonic projectile

• US 5,241,518 A
• Filed: 02/18/1992
• Issued: 08/31/1993
• Est. Priority Date: 02/18/1992
• Status: Expired due to Term

• Current Assignee: First Fidelity Bank National Association As Agent
• Original Assignee: AAI Corporation (Textron Inc)
• Inventors: Conner, Nelson O., McNelis, Niall B.
• Primary Examiner(s): Pihulic, Daniel T.
• Application Number:
  US07/836,601
• Time in Patent Office: 560 Days
• Field of Search: 367/906, 367/127, 367/124, 367/118, 367/129, 434/16, 434/17, 434/18, 434/19, 273/372
• US Class Current: 367/127
• CPC Class Codes: G01S 3/80 using ultrasonic, sonic or infrasonic waves
• CPC Class Codes: G01S 5/18 using ultrasonic, sonic, or infrasonic waves
• CPC Class Codes: Y10S 367/906 Airborne shock-wave detection

Abstract

Apparatus and method for determining the trajectory of a supersonic projectile of unknown velocity and direction having at least three spaced-apart sensors capable of encountering a shock wave generated by a supersonic projectile passing in the vicinity of the sensors and capable of generating signals in response to the shock wave, which signals are related to an azimuth and elevation angle of a unit sighting vector from each sensor to an origin of the shock wave. Means are provided for calculating from the signals the azimuth and elevation angle of the unit sighting vector from each sensor to the origin of the shock wave. Means are provided for calculating from the unit sighting vector of each of the three sensors, the azimuth and elevation angle of the local trajectory of the projectile.

Claims

1. Apparatus for determining the trajectory of a supersonic projectile of unknown velocity and direction, comprising:

(1) at least three spaced-apart sensors capable of encountering a shock wave generated by a supersonic projectile passing in the vicinity of the sensors and capable of generating signals in response to the shock wave, which signals are related to an azimuth and elevation angle of a unit sighting vector from each sensor to an origin of the shock wave;

(2) means for calculating from the said signals the azimuth and elevation angle of the unit sighting vector from each sensor to the origin of the shock wave; and

(3) means for calculating from the unit sighting vector of each of the three sensors, the azimuth and elevation angle of the local trajectory of the projectile.

2. The apparatus of claim 1 wherein the sensors have transducers which are sensitive to a shock wave propagated by a projectile.

3. The apparatus of claim 2 including means for measuring the time lapses of the shock wave in passing the transducers of a sensor.

4. The apparatus of claim 3 including means for measuring differences in time lapses of the shock wave in passing the transducers.

5. The apparatus of claim 4 wherein the transducers are sensitive to the shock front of the shock wave.

6. The apparatus of claim 1 wherein the sensors are sensitive to the shock wave and to an ambient density line and means are provided for calculation of the length of the projectile from the time lapse of the passing of the shock wave and the ambient density line over a sensor.

7. The apparatus of claim 2 wherein there are three transducers in each sensor.

8. The apparatus of claim 7 wherein the transducers are arranged as an equilateral triangle.

9. The apparatus of claim 1 wherein the at least three sensors are arranged so as to form a triangle.

10. The apparatus of claim 1 wherein there is a plurality of more than three sensors and means are provided for selecting at least three sensors from the plurality of sensors for calculating the azimuth and elevation angle of the local trajectory of the projectile.

11. The apparatus of claim 2 wherein the transducers of a sensor are spaced apart at least 3 cm.

12. The apparatus of claim 11 wherein the sensors are spaced apart at least 200 cm and up to 30 meters.

13. The apparatus of claim 1 wherein the sensors are substantially acoustically isolated from each other.

14. The apparatus of claim 2 wherein the transducers are substantially acoustically isolated from each other.

15. The apparatus of claim 1 wherein the sensors are mounted on a motorized vehicle, a gun, a rifle or a portable base.

16. The apparatus of claim 15 wherein the sensors are mounted on a tank.

17. The apparatus of claim 2 wherein the transducer is a piezoelectric crystal.

18. The apparatus of claim 17 wherein the crystals are mounted on an acoustic damping material.

19. A method for determining the trajectory of a supersonic projectile of unknown velocity and direction, comprising:

(1) providing at least three spaced-apart sensors capable of encountering a shock wave generated by a supersonic projectile passing in the vicinity of the sensors and capable of generating signals in response to the shock wave, which signals are related to an azimuth and elevation angle of a unit sighting vector from each sensor to an origin of the shock wave;

(2) calculating from the said signals the azimuth and elevation angle of a unit sighting vector from each sensor to the origin of the shock wave; and

(3) calculating from the unit sighting vectors of each of the three sensors, the azimuth and elevation angle of the local trajectory of the projectile.

20. The method of claim 19 wherein the sensors have transducers which are sensitive to a shock wave propagated by a projectile.

21. The method of claim 20 including measuring the time lapses of the shock wave in passing the transducers of a sensor.

22. The method of claim 21 including measuring differences in time lapses of the shock wave in passing the transducers.

23. The method of claim 22 wherein the transducers are sensitive to the shock front of the shock wave.

24. The method of claim 19 wherein the sensors are sensitive to the shock wave and to an ambient density line and the length of the projectile is calculated from the time lapse of the passing of the shock wave and the ambient density line over a sensor.

25. The method of claim 20 wherein there are three transducers in each sensor.

26. The method of claim 25 wherein the transducers are arranged as an equilateral triangle.

27. The method of claim 19 wherein the at least three sensors are arranged so as to form a triangle.

28. The method of claim 19 wherein there is a plurality of more than three sensors and at least three sensors from the plurality of sensors are selected for calculating the azimuth and elevation angle of the trajectory of the projectile.

29. The method of claim 20 wherein the transducers of a sensor are spaced apart at least 3 cm.

30. The method of claim 19 wherein the sensors are substantially acoustically isolated from each other.

31. The method of claim 20 wherein the transducers are substantially acoustically isolated from each other.

32. The method of claim 29 wherein the sensors are spaced apart at least 200 cm and up to 30 meters.

33. The method of claim 19 wherein the sensors are mounted on a motorized vehicle, a gun, a rifle or a portable base.

34. The method of claim 33 wherein the sensors are mounted on a tank.

35. The method of claim 20 wherein the transducers are piezoelectric crystals.

36. The method of claim 35 wherein the crystals are mounted on an acoustic damping material.