Multi-function radio frequency (MFRF) module and gun-launched munition with active and semi-active terminal guidance and fuzing sensors

Patent metadata

Field	Value
Publication number	US-9683814-B2
Application number	US-201514659111-A
Country	US
Kind code	B2
Filing date	Mar 16, 2015
Priority date	Mar 16, 2015
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

Abstract

A multi-function radio frequency (MFRF) module integrates command guidance, active and semi-active terminal guidance (and possibly passive) and fuzing sensors for gun-launched munitions into a single assembly. The MFRF module can be incorporated into a variety of different gun-launched munitions to execute missions currently performed by guided missiles. The MFRF module is programmable during munition activation to select the guidance mode, active or semi-active, and a primary fuze mode, proximity or height of burst.

First claim

I claim:

1. A multi-function radio frequency (MFRF) guided munition, comprising:
a munition;
a plurality of airfoils about the munition to stabilize flight;
an explosive warhead on the munition;
at least four forward-facing antennas conformal with the surface of the munition or the airfoils;
at least one rear-facing antenna;
a MFRF module comprising,
a frequency synthesizer configured to generate an intermediate frequency (IF) signal;
a transmitter configured to upconvert an input waveform from the IF to an RF frequency and to transmit the RF waveform from one or more of the forward-facing antennas;
a multi-channel analog receiver, each channel coupled to a respective antenna to receive an RF signal and to downconvert the RF signal to an IF signal, amplify the signal and filter noise;
an analog-to-digital converter configured to digitize the IF signals from the multiple receiver channels; and
an RF signal processor configured to implement a command-guided mode to process the digital IF signal from the rear-facing antenna and output command guidance information until target acquisition, configurable to implement any one of an active guidance mode in which the transmitter is activated and a semi-active guidance mode to process the digital IF signals from the at least four forward-facing antennas and upon acquisition of the target to derive direction finding information towards the target until terminal, and configurable to implement either of a proximity and height of burst fuze modes by activating the transmitter at terminal and processing the digital IF signal from at least one of the forward-facing antennas to derive range-to-target or Doppler information;

a guidance processor configured to process the direction finding information and output a guidance command; and
a control system responsive to the guidance command to maneuver the munition towards the target; and
a fuze processor configured to initiate detonation of the warhead.

2. The MFRF guided munition of claim 1 , wherein the RF signal processor is configured for selection and storage of the guidance and fuze modes at munition activation just prior to launch.

3. The MFRF guided munition of claim 1 , wherein if one of the proximity or height of burst fuze modes are selected, the RF signal processor outputs the Doppler information or range-to-target, respectively, wherein said fuze processor is configured to process the Doppler information or range-to-target to initiate detonation.

4. The MFRF guided munition of claim 1 , wherein the RF signal processor is configured in either the active or semi-active guidance modes to implement sum/delta processing on the at least four digital IF signals to derive the direction finding information.

5. The MFRF guided munition of claim 1 , wherein the RF signal processor is configurable to implement a passive guidance mode in which the target is actively emitting RF energy, wherein the channels of the multi-channel analog receiver coupled to the at least four forward-facing antennas are configured to receive the actively emitted RF energy to support the passive guidance mode.

6. The MFRF guided munition of claim 1 , wherein at least the frequency synthesizer, the transmitter, the multi-channel analog receiver and the analog-to-digital converter are implemented on a single board within the module.

7. The MFRF guided munition of claim 6 , wherein a receiver channel, the synthesizer and the analog-to-digital converter are implemented on an aft-facing side of the board and four receiver channels are implemented around the transmitter on a forward-facing side of the board.

8. The MFRF guided munition of claim 1 , wherein the munition has a diameter of less than 5 inches.

9. A multi-function radio frequency (MFRF) guided munition, comprising:
a sub-caliber munition having a diameter of less than 5 inches;
a plurality of airfoils deployed about the munition and configured to stabilize flight;
an explosive warhead on the munition;
four forward-facing antennas conformal with the surface of the sub-caliber munition or the airfoils;
a rear-facing antenna;
a MFRF module comprising,
a frequency synthesizer configured to generate an intermediate frequency (IF) signal;
a transmitter configured to upconvert an input waveform from the IF to an RF frequency and to transmit the RF waveform from one or more of the forward-facing antennas; and
a multi-channel analog receiver, each channel coupled to a respective antenna to receive an RF signal and to downconvert the RF signal to an IF signal, amplify the signal and filter noise;
an analog-to-digital converter configured to digitize the IF signals from the multiple receiver channels;
an RF signal processor configured to implement a command-guided mode to process the digital IF signal from the rear-facing antenna and output command guidance information until target acquisition, configurable to implement any one of an active guidance mode in which the transmitter is activated and a semi-active guidance mode to process the digital IF signals from the four forward-facing antennas and upon acquisition of the target to derive direction finding information towards the target until terminal, and configurable to implement either of a proximity and height of burst fuze modes by activating the transmitter at terminal and processing the digital IF signal from at least one of the forward-facing antennas to derive range-to-target or Doppler information, said RF signal processor configured for selection and storage of the guidance fuze modes at munition activation just prior to launch;

a guidance processor configured to process the direction finding information and output a guidance command; and
a control system responsive to the guidance command to maneuver the munition towards the target; and
a fuze processor configured to receive one of the Doppler information or range-to-target as a primary fuze mode to initiate detonation of the warhead.

10. The MFRF guided munition of claim 9 , wherein the RF signal processor is configured in either the active or semi-active guidance modes to implement sum/delta processing on the at least four digital IF signals to derive the direction finding information.

11. The MFRF guided munition of claim 9 , wherein the RF signal processor is configurable to implement a passive guidance mode in which the target is actively emitting RF energy, wherein the channels of the multi-channel analog receiver coupled to the at least four forward-facing antennas are configured to receive the actively emitted RF energy to support the passive guidance mode.

12. The MFRF guided munition of claim 9 , wherein at least the frequency synthesizer, the transmitter, the multi-channel analog receiver and the analog-to-digital converter are implemented on a single board within the module.

13. The MFRF guided munition of claim 12 , wherein a receiver channel, the synthesizer and the analog-to-digital converter are implemented on an aft-facing side of the board and four receiver channels are implemented around the transmitter on a forward-facing side of the board.

14. A multi-function RF (MFRF) module for providing guidance and fuzing sensors to a gun-launched munition, said MFRF module comprising:
a frequency synthesizer configured to generate an intermediate frequency (IF) signal;
a transmitter configured to upconvert an input waveform from the IF to an RF frequency and to transmit the RF waveform from one or more of the forward-facing antennas; and
a multi-channel analog receiver, each channel configured to receive an RF signal from an antenna and to downconvert the RF signal to an IF signal, a

Assignees

• Raytheon Co

Inventors

• Dryer Richard L

Classifications

• F41G7/30

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

• F41G7/226

  Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles · CPC title

• F42B15/01

  Arrangements thereon for guidance or control ({steering arrangements F42B10/60}; aircraft flight control B64C; guidance systems other than those installed aboard F41G7/00, F41G9/00; locating by use of radio or other waves G01S; flight control in general G05D1/00; computer aspects G06]) · CPC title

• F42C13/04

  operated by radio waves · CPC title

• F41H11/02

  Anti-aircraft or anti-guided missile {or anti-torpedo} defence installations or systems (cartridges or missiles for producing smoke or for dispensing radar chaff or infrared material F42B5/15, F42B12/48, F42B12/70; {informative reference: details of radar or sonar systems G01S7/00; jamming or electronic countermeasures G01S7/38, G01S7/495, H04K3/00}) · CPC title