Accurate range-to-go for command detonation

Patent metadata

Field	Value
Publication number	US-11243058-B2
Application number	US-201816123202-A
Country	US
Kind code	B2
Filing date	Sep 6, 2018
Priority date	Sep 6, 2018
Publication date	Feb 8, 2022
Grant date	Feb 8, 2022

Abstract

The system and method for accurately determining range-to-go for the command detonation of a projectile. Using dual laser and/or radio frequency detectors on the tail and on the nose of a spinning projectile to determine the range-to-go, time-to-go, or lateral offset from the projectile to the target.

First claim

What is claimed:

1. A method for guiding a projectile, comprising:
providing a projectile comprising a tail portion and a nose portion;
detecting a first laser or radio frequency signal via a tail detector mounted on the tail portion of the projectile;
determining a first time at which the first laser or radio frequency signal is detected via the tail detector mounted on the tail portion of the projectile;
detecting a second laser or radio frequency signal via a forward detector mounted on the nose portion of the projectile, the second laser or radio frequency signal being the first laser or radio frequency signal that has reflected off a target;
determining a second time at which the second laser or radio frequency signal is detected via the forward detector mounted on the nose portion of the projectile;
comparing the first time to the second time to determine a time delay;
determining an azimuth and an elevation of the projectile based on the detection of the first laser or radio frequency signal via the tail detector mounted on the tail portion of the projectile; and
determining one or more of the following using the time delay between detection by the tail detector and detection by the forward detector: a lateral offset between the projectile and the target; a time-to-go for the projectile to reach the target; and a range-to-go for the projectile to reach the target.

2. The method for guiding a projectile according to claim 1 , wherein one or both of the tail detector on the tail of the projectile and the forward detector on the nose of the projectile is an electro-optical PIN diode.

3. The method for guiding a projectile according to claim 1 , wherein one or both of the tail detector on the tail of the projectile and the forward detector on the nose of the projectile is a radio frequency antenna.

4. The method for guiding a projectile according to claim 1 , wherein the forward detector on the nose of the projectile is a radio frequency antenna and the tail detector on the tail of the projectile is an electro-optical PIN diode.

5. The method for guiding a projectile according to claim 1 , wherein a range finding clock is started when the first signal is detected (T zero ) by the detector on the tail of the projectile and the range finding clock is stopped when the second signal is detected by the front detector on the nose of the projectile (T reflected ), thereby creating a time differential that represents a round trip time between the projectile and the target which can be converted to a range-to-go.

6. The method for guiding a projectile according to claim 1 , wherein a range finding clock is started when the first signal is detected (T zero ) by the tail detector on the tail of the projectile and the range finding clock is stopped when the second signal is detected by the forward detector on the nose of the projectile (T reflected ), thereby creating a time differential that represents a round trip time between the projectile and the target which can be used as a time-to-go, or limit trip switch.

7. The method for guiding a projectile according to claim 6 , wherein when the time-to-go is about 0.0015 seconds, sending a signal to the projectile to cause the projectile to detonate.

8. The method for guiding a projectile according to claim 6 , wherein the time-to-go determination is dependent on the projectile speed and the detonation time-to-go is programmed at the time of launch.

9. The method for guiding a projectile according to claim 6 , wherein the time-to-go value is negative.

10. The method for guiding a projectile according to claim 1 , wherein the first signal further comprises a first pulse repetition interval and the second signal further comprises a second pulse repetition interval.

11. The method for guiding a projectile according to claim 1 , wherein the lateral offset between the projectile's trajectory and the target's actual position is determined by measuring a time expansion between the first pulse repetition interval and the second pulse repetition interval and convolving the projectile's velocity with the time-to-go thereby improving an accuracy of a detonation.

12. A guided projectile, comprising;
a tail detector located on a tail portion of the guided projectile for detecting a laser or radio frequency signal;
a forward detector located on a forward portion of the guided projectile for detecting a reflected laser or radio frequency signal from a target;
a computer readable storage device having instructions, which when executed by a processor, cause the processor to execute:
determining a first time at which the laser or radio frequency signal is detected via the tail detector;
determining a second time at which the reflected laser or radio frequency signal is detected via the forward detector;
comparing the first time to the second time to determine a time delay;
determining an azimuth and an elevation of the guided projectile based on the detected laser or radio frequency signal; and
determining one or more of the following using the time delay between detection by the tail detector and detection by the forward detector: a lateral offset between the projectile and the target; a time-to-go for the projectile to reach the target; and a range-to-go for the projectile to reach the target.

13. The guided projectile of claim 12 , wherein at least one of the tail detector and the forward detector is an electro-optical PIN diode.

14. The guided projectile of claim 12 , wherein at least one of the tail detector and the forward detector is a radio frequency antenna.

15. The guided projectile of claim 12 , wherein the tail detector is a radio frequency antenna and the forward detector is an electro-optical PIN diode.

16. The guided projectile of claim 12 , wherein a range finding clock is started when the signal is detected (T zero ) by the tail detector and the range finding clock is stopped when the reflected laser or radio frequency signal is detected by the forward detector (T reflected ), thereby creating a time differential that represents a round trip time between the projectile and the target which can be converted to a range-to-go.

17. The guided projectile of claim 12 , wherein a range finding clock is started when the signal is detected (T zero ) by the tail detector and the range finding clock is stopped when the reflected laser or radio frequency signal is detected by the forward detector (T reflected ), thereby creating a time differential that represents a round trip time between the projectile and the target which can be used as a time-to-go, or limit trip switch.

18. The guided projectile of claim 12 , wherein when the time-to-go is about 0.0015 seconds, sending a signal to the projectile to cause the projectile to detonate.

19. The guided projectile of claim 12 , wherein the azimuth and the elevation of the guided projectile is based on the detected laser or radio frequency signal by the tail detector.

20. A computer program product including one or more machine-readable mediums encoded with instructions that when executed by one or more processors cause a process to be carried out for projectile guidance with a projectile having a tail detector and a forward detector, the process comprising:
determining a first time at which a laser or radio frequency signal is detected via the tail detector;
determining a second time at which a reflected laser or radio frequency signal is detected via the forward detector;
comparing the first time to the second time to determine a ti

Assignees

• Bae Sys Inf & Elect Sys Integ

Inventors

• Choiniere Michael J
• Winker Bruce

Classifications

• F42C13/023 Primary

  using active distance measurement · CPC title

• F42C13/04

  operated by radio waves · CPC title

• F41G7/222

  for spin-stabilized missiles · CPC title

• F41G7/2293

  using electromagnetic waves other than radio waves · CPC title

• F41G7/2286

  using radio waves · CPC title