Apparatus and method for calculating muzzle velocity

• US 6,064,196 A
• Filed: 12/31/1997
• Issued: 05/16/2000
• Est. Priority Date: 12/31/1997
• Status: Expired due to Term

• Current Assignee: AAI Corporation (Textron Inc)
• Original Assignee: AAI Corporation (Textron Inc)
• Inventors: Oberlin, Richard P., Cullison, Doug R.
• Primary Examiner(s): PATIDAR, JAY M
• Application Number:
  US09/001,694
• Time in Patent Office: 867 Days
• Field of Search: 324/207.17, 324/178, 324/179, 324/207.15, 324/207.16, 336/45, 336/129, 73/167, 340/870.31, 346/38, 368/108
• US Class Current: 324/179
• CPC Class Codes: G01P 3/665 for projectile velocity measurements

Abstract

Apparatus for measuring projectile muzzle velocity with an accuracy of ±0.1% is mounted in an easily portable muzzle attachment. It operates in the following manner. A washer shaped permanent magnet is positioned on a projectile body. A position sensor containing two inductive coils is located inside the muzzle. When the projectile is fired, the magnet mounted on the projectile passes through the inductive coils, inducing a voltage in each coil. Each voltage is amplified and then fed into hysteresis and zero crossing comparators corresponding to each inductive coil. The zero crossing comparator detects when the induced voltage crosses zero. The hysteresis comparator will gate out any noise induced zero crossings. The two zero crossings are used to start and stop a digital counter which generates a velocity count signal that corresponds to the velocity of the projectile. Further noise interference rejection is obtained by encasing the muzzle extension in a magnetic metal.

Claims

1. Apparatus for measuring the muzzle velocity of a projectile, comprising:

a washer-shaped magnet having a north pole and a south pole that is positioned on a projectile body so that its outside diameter is located close to that of the projectile'"'"'s outside diameter, and the south pole of said magnet faces the direction in which the projectile will exit the muzzle;

a position sensor having a first and a second inductive coil mounted a known separation apart, wherein a voltage is induced in each coil when said magnet passes through said inductive coil;

a first and a second wide bandwidth preamplifier, each having an input and an output;

first and a second comparator pairs, each comparator in said comparator pairs having a positive input, a negative input connected to and electrically coupled to ground voltage, and an output;

a digital counter having a start input, a stop input, an in input, a reset input and an output; and

a high precision frequency source connected to and electrically coupled to the input of said digital counter to provide a clock signal to said digital counter;

wherein the input of said first wide bandwidth preamplifier is connected to and electrically coupled to said first inductive pickup coil to amplify the voltage induced in said first inductive coil when said magnet passes through it and the input of said second wide bandwidth preamplifier is connected to and electrically coupled to said second inductive coil to amplify the voltage induced in said second coil when said magnet passes through it;

wherein the positive inputs of said first comparator pair are connected to and electrically coupled to the output of said first wide bandwidth preamplifier and the positive inputs of said second comparator pair are connected to and electrically coupled to the output of said second wide bandwidth preamplifier;

wherein the outputs of said first comparator pair are connected to and electrically coupled to the start input of said digital counter to start said counter when the voltage induced in said first inductive coil crosses zero; and

wherein the outputs of said second comparator pair are connected to and electrically coupled to the stop input of said digital counter to stop said counter when the voltage induced in said second coil crosses zero, and thereby generate a velocity count signal, corresponding to the velocity of the projectile, on said output of said digital counter.

2. Apparatus according to claim 1, wherein said first and second comparator pairs each comprise a hysteresis comparator and a zero crossing comparator.

3. Apparatus according to claim 2, further comprising a pair of gates, each of which is connected to and electrically coupled between the outputs of a respective one of said first and second comparator pairs and its respective start or stop input of said counter.

4. Apparatus according to claim 3, wherein the output of each said gate comprises a digital "zero" until both of the outputs of its respective comparator pair are digital "ones".

5. Apparatus according to claim 1, wherein said magnet is less than or equal to about 0.020 inches thick.

6. Apparatus according to claim 1, wherein said first and second comparator pairs each comprise a Schmitt trigger and a zero crossing comparator.

7. Apparatus according to claim 1, wherein each of said inductive coils is a single wire.

8. Apparatus according to claim 1, wherein each of said inductive coils is a thin disk.

9. Apparatus according to claim 1, wherein each of said inductive coils is laminated on one of the ends of a spacer.

10. Apparatus according to claim 1, wherein said pickup coils are separated by a spacer inserted into a muzzle.

11. Apparatus according to claim 10, wherein said spacer is made from a zero temperature coefficient material.

12. Apparatus according to claim 10, wherein the temperature of the spacer is measured and used in a compensation term.

13. Apparatus according to claim 10, wherein the spacer has a positional uncertainty of 0.0001 inch.

14. Apparatus according to claim 1, wherein said muzzle is encased in a magnetic metal so that the muzzle acts as a waveguide and filters out high frequency noise.

15. Apparatus according to claim 14, wherein said magnetic metal is iron.

16. Apparatus according to claim 14, wherein said magnetic metal is steel.

17. Apparatus according to claim 14, wherein said magnetic metal is nickel.

18. Apparatus according to claim 1, wherein a time between two crossing events is calculated by multiplying the velocity count signal from said output of said digital counter by the frequency output of said high precision frequency source.

19. Apparatus according to claim 18, wherein the muzzle velocity is calculated by dividing the known separation apart between the first and second inductive coils by the time between two crossing events.

20. A method of calculating a muzzle velocity comprising the steps of:

generating a start input signal to a digital counter, when a voltage induced in a first coil decreases in magnitude from a positive voltage to a negative voltage crossing the zero voltage point, based on when a second pole of a magnet mounted on a projectile crosses said first inductive coil;

commencing a counting operation of said digital counter based on said start input signal;

generating a stop input signal to a digital counter when a voltage induced in a second coil decreases in magnitude from a positive voltage to a negative voltage crossing the zero voltage point, based on when the second pole of the magnet mounted on the projectile crosses said second inductive coil;

ceasing the counting operation of said digital counter based on said stop input signal;

determining a velocity count by retrieving an output of said digital counter;

retrieving a known frequency of a high precision frequency source;

calculating a time between said start input signal and said stop input signal by multiplying said velocity count by the output frequency of said high precision frequency source; and

dividing a known separation apart distance by the time between said start input signal and said stop input signal.

21. A method of calculating a muzzle velocity comprising the steps of:

generating a start input signal to a digital counter when a voltage induced in a first coil decreases in magnitude from a positive voltage to a negative voltage crossing the zero voltage point, based on when a second pole of a magnet mounted on a projectile crosses said first inductive coil;

commencing a counting operation of said digital counter based on said start input signal;

generating a stop input signal to a digital counter when a voltage induced in a second coil decreases in magnitude from a positive voltage to a negative voltage crossing the zero voltage point, based on when the second pole of the magnet mounted on the projectile crosses said second inductive coil;

ceasing the counting operation of said digital counter based on said stop input signal;

determining a velocity count by retrieving an output of said digital counter; and

calculating the muzzle velocity by dividing a known separation distance apart between said first inductive coil and said second inductive coil by the time between said start input signal and said stop input signal.

22. The method according to claim 21, wherein said calculating step further comprises the steps of:

retrieving a known frequency of a high precision frequency source;

calculating a time between said start input signal and said stop input signal by multiplying said velocity count by the output frequency of said high precision frequency source; and

dividing a known separation apart distance by the time between said start input signal and said stop input signal.