Semi-active RF target detection and proximity detonation based on angle-to-target

Patent metadata

Field	Value
Publication number	US-9709372-B2
Application number	US-201514623886-A
Country	US
Kind code	B2
Filing date	Feb 17, 2015
Priority date	Feb 17, 2015
Publication date	Jul 18, 2017
Grant date	Jul 18, 2017

Abstract

A semi-active RF proximity fuze for warhead detonation is provided where external RADAR is available to illuminate the target. The fuze incorporates multiple receiving antennas with digital phase detection processing to distinguish the angle from which the target returns are received and uses that information to determine the detonation timing for the warhead. Detonation timing can be improved by processing the rate of change of the angle-to-target or processing the range and Doppler information to compensate for target velocity and distance.

First claim

I claim:

1. An apparatus, comprising:
a projectile adapted to pass in proximity to a target, said projectile including a plurality of RF antennae having at least one rear-facing lobe configured to receive pulsed radiation directly from an RF source and at least three forward-facing lobes configured to receive reflections of said pulsed radiation from the target;
an explosive warhead; and
a multi-channel receiver comprising a plurality of processing channels coupled to said plurality of RF antennae that together feed digital samples of received pulsed radiation to a digital signal processor, said digital signal processor comprising sample memory to receive and store digital samples from the at least one rear-facing lobe and each of said forward-facing lobes, at least three match filters to correlate the digital samples of each of said at least three forward-facing lobes to the digital samples from the at least one rear-facing lobe to match the digital samples of the RF source to the samples of reflections of said pulsed radiation from the target, a phase comparator to compare a phase relationship between the matched digital samples from the at least three forward-facing lobes and the at least one rear-facing lobe to generate via triangulation a sequence of angle-to-target estimates and detonation timing logic to process the angle-to-target estimates to issue a detonation command to detonate the explosive warhead.

2. The apparatus of claim 1 , wherein the digital signal processor is configured to process the sequence of angle-to-target estimates to generate an angle-to-target rate and to issue the detonation command when the angle-to-target rate reaches and then decreases from a peak value.

3. The apparatus of claim 1 , wherein the digital signal processor is configured to issue the detonation command when the angle-to-target estimate reaches a certain angle, wherein the digital signal processor is configurable to set the certain angle.

4. The apparatus of claim 3 , wherein the certain angle is fixed and the digital signal processor set apriori based on characteristics of the projectile or the target.

5. The apparatus of claim 4 , wherein the digital signal processor is configured to process the sequence of angle-to-target estimates to generate an angle-to-target rate and to use that rate to predict when the angle-to-target estimate will reach the certain angle.

6. The apparatus of claim 3 , wherein the digital signal processor is configured to process the sequence of digital samples from at least one of the forward-facing lobes and the at least one rear-facing lobe to generate a range-to-target estimate and a relative velocity estimate and to process the range-to-target and relative velocity estimates to set the certain angle.

7. The apparatus of claim 6 , wherein the digital signal processor is configured to process the sequence of angle-to-target estimates to generate an angle-to-target rate and to use that rate to predict when the angle-to-target estimate will reach the certain angle.

8. The apparatus of claim 1 , wherein the projectile comprises a rear-facing antenna and at least three forward-facing antennae.

9. The apparatus of claim 1 , wherein each channel of the multi-channel receiver comprises gain control configured to keep an amplitude of the received RF signal within a linear range of the A/D converter and a filter configured to pass an RF signal frequency at a source frequency of the RF source plus an expected Doppler shift.

10. The projectile of claim 1 , wherein the digital signal processor comprises a plurality of match filters that correlate the digital samples from the at least one rear-facing lobe to the digital samples from each of the at least three forward-facing lobes to extract the phase relationship.

11. A proximity fuze for a projectile, comprising:
a plurality of RF antennae having at least one rear-facing lobe configured to receive pulsed radiation directly from an RF source and at least three forward-facing lobes configured to receive reflections of said pulsed radiation from the target; and
a multi-channel receiver comprising a plurality of processing channels coupled to said plurality of RF antennae that together feed digital samples of received pulsed radiation to a digital signal processor, said digital signal processor comprising sample memory to receive and store digital samples from the at least one rear-facing lobe and each of said forward-facing lobes, at least three match filters to correlate the digital samples of each of said at least three forward-facing lobes to the digital samples from the at least one rear-facing lobe to match the digital samples of the RF source to the samples of reflections of said pulsed radiation from the target, a phase comparator to compare a phase relationship between the matched digital samples from the at least three forward-facing lobes and the at least one rear-facing lobe to generate via triangulation a sequence of angle-to-target estimates and detonation timing logic to process the angle-to-target estimates to issue a detonation command to detonate the explosive warhead.

12. The proximity fuze of claim 11 , wherein the digital signal processor is configured to process the sequence of angle-to-target estimates to generate an angle-to-target rate and to issue the detonation command when the angle-to-target rate reaches and then decreases from a peak value.

13. The proximity fuze of claim 11 , wherein the digital signal processor is configured to issue the detonation command when the angle-to-target estimate reaches a certain angle, wherein the digital signal processor is configurable to set the certain angle.

14. The projectile of claim 13 , wherein the digital signal processor is configured to process the sequence of digital samples from at least one of the forward-facing lobes and the at least one rear-facing lobe to generate a range-to-target estimate and a relative velocity estimate and to process the range-to-target and relative velocity estimates to set the certain angle.

15. The projectile of claim 14 , wherein the digital signal processor is configured to process the sequence of angle-to-target estimates to generate an angle-to-target rate and to use that rate to predict when the angle-to-target estimate will reach the certain angle.

16. A method of proximity detonation of a projectile, comprising:
receiving and conditioning an RF signal at each of at least one rear-facing lobe configured to receive pulsed radiation directly from an RF source and at least three forward-facing lobes configured to receive reflections of said pulsed radiation from a target;
converting the RF signal to a sequence of digital samples;
correlating the digital samples of each of said at least three forward-facing lobes to the digital samples from the at least one rear-facing lobe to match the digital samples of the RF source to the samples of reflections of said pulsed radiation from the target;
comparing a phase relationship between the matched digital samples from the at least three forward-facing lobes and the at least one rear-facing lobe to generate via triangulation a sequence of angle-to-target estimates; and
processing the angle-to-target estimates to issue a detonation command to detonate the explosive warhead.

17. The method of claim 16 , further comprising processing the sequence of angle-to-target estimates to generate an angle-to-target rate and issuing the detonation command when the angle-to-target rate reaches and then decreases from a peak value.

18. The method of claim 16 , wherein the deton

Assignees

• Raytheon Co

Inventors

• Edwards Jeffrey C

Classifications

• F42C13/04 Primary

  operated by radio waves · CPC title

• F42C13/045 Primary

  using transmission of F.M. waves · CPC title

• F41G7/30

  Command link guidance systems {(homing F41G7/2206)} · CPC title

• F42B12/20

  of high-explosive type (F42B12/44 takes precedence) · CPC title