[go: up one dir, main page]

GB2356034A - Missile decoy system - Google Patents

Missile decoy system Download PDF

Info

Publication number
GB2356034A
GB2356034A GB8713360A GB8713360A GB2356034A GB 2356034 A GB2356034 A GB 2356034A GB 8713360 A GB8713360 A GB 8713360A GB 8713360 A GB8713360 A GB 8713360A GB 2356034 A GB2356034 A GB 2356034A
Authority
GB
United Kingdom
Prior art keywords
target
screen
decoy system
missile
image
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB8713360A
Other versions
GB2356034B (en
GB8713360D0 (en
GB2356034A8 (en
Inventor
Clive Ian Coleman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems Electronics Ltd
Original Assignee
GEC Marconi Ltd
Marconi Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by GEC Marconi Ltd, Marconi Co Ltd filed Critical GEC Marconi Ltd
Publication of GB8713360D0 publication Critical patent/GB8713360D0/en
Publication of GB2356034A publication Critical patent/GB2356034A/en
Application granted granted Critical
Publication of GB2356034B publication Critical patent/GB2356034B/en
Publication of GB2356034A8 publication Critical patent/GB2356034A8/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00Defence installations; Defence devices
    • F41H11/02Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H3/00Camouflage, i.e. means or methods for concealment or disguise
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H9/00Equipment for attack or defence by spreading flame, gas or smoke or leurres; Chemical warfare equipment
    • F41H9/06Apparatus for generating artificial fog or smoke screens

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Optical Radar Systems And Details Thereof (AREA)

Abstract

A system for decoying missiles which use thermal imaging sensors to home in on their targets. An infrared image of a ship 4 or other threatened body is projected onto a smoke screen and moved across the screen so as to lead the missile away from the target. The means for projecting the image may comprise an infra-red laser and servo-controlled mirrors housed in a buoy 1. The buoy may be launched from the ship in response to detection of an approaching missile and may incorporate a radar decoy.

Description

2356034 Nissile Decoy System This invention relates to decoy systems for
missiles incorporating imaging sensors. Infrared missile seekers which use imaging sensors rather than single "hot-spotm detectors present a serious threat to potential targets such as warships. Conventional infrared decoys such as flares and modulated heat sources are totally ineffective against these advanced seekers. Imaging sensors may operate in the visible band too. An object of this invention is to present an image of a ship or other platform under threat, to act as a missile decoy.
According to one aspect of the invention a decoy system for decaying missiles incorporating imaging sensors comprises means to generate an image representing a target to be protected and means to project said image onto a projection screen remote from the target. The means to generate the image may comprise a source of radiation, such as a laser, arranged to illuminate a representation of the target, the representation being transparent to that radiation. Preferably the position of the image on the screen can be controlled so as to move the i1nage away from the target and thereby deflect the missile. This may be achieved by one or more servo-controlled -2mirrors, for example.
For use particularly with anti-ship missiles, the means to generate and project the image may be housed in a buoy. The buoy may be radio controlled, or pre-programed to follow a course in the water. The buoy is preferably rocket launched from the target ship in response to detection of an approaching missile. The buoy may additionally incorporate a radar decoy.
The decoy system preferably includes means to generate a smoke screen to constitute the projection screen. The smoke screen may incorporate material to enhance its reflectivity.
According to another aspect of the invention, in a method of decoying a missile having imaging sensors, an image representing the target is projected onto a screen remote from the target and moved away from the target, thereby to deflect the missile. The method may be for decaying an infrared seeking anti-ship missile and may comprise the steps of launching from a target ship, on detection of an approaching missile, a projector mounted on a buoy, and generating a smoke screen, the projector being arranged to project an infrared image of the target ship onto the smoke screen.
One embodiment of the invention will now be described with reference to the accompanying drawings of which:- Figure 1 shows a plan view of the missile decoy system employed to protect a ship; Figure 2(a) shows an image projector of the system; Figure 2(b) shows a transparency carrying an image of the target to be protected; and Figure 3 shows a buoy on which the projector is mounted.
Referring to Figure 1, an infrared-seeking missile (not shown) approaches its target, a ship 4, along a trajectory 5. A smoke screen hangs between the ship and the oncoming missile and a thermal (i.e. infrared) simulated image 2 of the target 4 is projected from a buoy 1 onto the smoke screen.
The smoke screen is generated in response to a missile approach warning provided by a system not shown but mounted on the target ship or other 'friendly' platform. This warning system may give a crude bearing of the missile direction, perhaps within 45% The smoke screen shields the ship 4 by obscuring the infrared target, but in itself is unlikely to deflect the missile off course since the missile might already be travelling in the right direction before any smoke is generated and, on losing target lock, will simply continue on that course; alternatively,.the missile may have a further homing mode (e.g. radar guided) which would be less susceptible to obscuration by the smoke screen and would take over if infrared homing were denied.
A decoy image is provided by a projector 15, launched on a buoy 1 from the ship 4. An infrared image representing the target is projected onto the smoke screen at an initial position 2, and then by controlling the buoy, moved away from the ship. The missile's infrared seeker picks up the thermal signal from the image, recognises it as a ship and tracks it as it moves away along the smoke screen. The image is moved off to a final position 3 such that the incoming missile is deflected well away from the target ship, or any others in the area.
The thermal image projector is shown in Figure 2a. The projector 15 consists of an infrared laser 8, beam formi,ng optics 9 for illuminating a transparency 10 and beam projecting optics 11 to project the image beam towards some means (not shown) for controlling its direction. The laser 8 might be, for example, a C02 laser emitting at about 10 micrometres. Suitable material for the optics 9 and 11 would be germanium or zinc sulphide or other infrared transparent material. The "transparency" is shown in Figure 2(b), consisting simply of a likeness of the ship 4 cut out of a metal sheet; it need not have very high reoslution, but the sheet should be a reasonably good conductor for thermal reasons.
The projector 15 is mounted in a powered and radio controlled buoy 1, as shown in Figure 3. The beam is projected by way of two servo controlled mirrors 16. The projector is radio-controlled to rotate and thereby move the image on the smoke screen away from the target ship, by radio control means 17. Alternatively the servo controlled mirrors may be controlled to move the target image on the smoke screen. The mirror control also acts to stabilise the image position, as the buoy bobs in the water. The image position control means may be pre-programed to rotate as required.
The buoy should be capable of being rapidly deployed; it is therefore rocket-launched in response to a signal from a missile approach warning. The whole decoy system can be simply automated to co-ordinate the missile approach signal, smoke screen generation, buoy deployment, projector control and image 'walk-off', taking into account wind strength and direction, the ship's course and other ship location information. As an alternative to radio control, the buoy could be loaded with a 'prelaunch' message controlling its off-target travel.
Possible refinements of the system include augmenting the reflectivity of the projection screen by the use of appropriate aerosols or reflective chaff, and providing some laser power, via a frequency doubler, at about 5 micrometres, so that 3-5 micrometres or dual infrared band seekers are also defeated. Alternatively a thermal infrared source could be used to provide illumination in the 3-5 micrometres band. A radar transmitter could be incorporated in the buoy, to provide a radar decoy in addition to and independent of the infrared decoy.
As an alternative to controlling the projector or the mirrors to move the projected target image, the buoy can be steered through the water by radio control, or by a pre-programmed motor.
High winds could affect the launch of the buoy but, as in any fire control system, wind speed and direction are taken into account. However it will be appreciated that high positional accuracy -5is not necessary for this system.
The system is equally useful on land, where infrared seeking missiles may be directed against buildings and vehicles. Again, the mirror system or projector is controlled to move the simulated target on a smoke screen, or the projection apparatus may be housed in a remote controlled vehicle which can be steered away over the land, moving the image as it travels.

Claims (15)

-6CLAINS A decoy system for decoying missiles incorporating imaging sensors, comprising means adapted to generate an image representing a target to be protected, and means adapted to project said image onto a projection screen remote from said target. 2. A decoy system according to Claim 1, comprising means adapted to control the position of the image on said screen, allowing the image to be moved away from said target thereby to deflect the missile. 3. A decoy system according to Claim 1 or 2 wherein said means adapted to generate an image comprises a source of radiation arranged to illuminate a representation of the target, said representation being transparent to said radiation. 4. A decoy system according to Claim 3 wherein said radiation source is an infra-red laser. 5. A decoy system according to Claim 2. 3 or 4 wherein said means adapted to control the position of the image comprises an. arrangement of servocontrolled mirrors. 6. A decoy system according to any preceding claim and adapted to be movable by remote control. 7. A decoy system according to any preceding claim including means adapted to generate a smoke screen to constitute said projecton screen. 8. A decoy system according to Claim 7 wherein said smoke screen incorporates material to enhance its reflectivity. -7 9. A decoy system according to any preceding claim mounted in a buoy and adapted for use against anti-ship missiles. 10. A decoy system according to any preceding claim incorporating a radar decoy. 11. A method of decoying a missile having imaging sensors wherein an image representing a target is projected onto a projection screen remote from said target and moved away from said target, thereby to deflect the missile. 12. A method according to Claim 11 comprising the step of generating a smoke screen to form said projection screen. 13. A method according to Claim 11 or 12 for decoying an infrared seeking anti-ship missile comprising the steps of launching from a target ship, on detection of an approaching missile, a projector mounted on a buoy and projecting an infrared image of said target ship onto said projection screen. 14. A decoy system substantially as hereinbefore described with reference to the accompanying drawings.
1 15. A method of decoying a missile having an imaging sensor, substantially as hereinbefore described with reference to the accompanying drawings.
f Amendments to the claims have been filed as follows A decoy system for decaying missiles incorporating imaging sensors, the system comprising means for deploying a particulate screen in space and means for projecting an image of a target to be protected on to said screen remote from said target.
2. A decoy system according to Claim 1, comprising means adapted to control the position of the image on said screen, allowing the image to be moved away from said target thereby to deflect the missile.
3. A decoy system according to Claim 1 or 2, wherein said means for projecting an image comprises a source of radiation arranged to illuminate a representation of the target, said representation being transparent to said radiation.
4. A decoy system according to Claim 3 wherein said radiation source is an infra-red laser.
5. A decoy system according to Claim 2, wherein said means adapted to control the position of the image comprises an arrangement of servocontrolled mirrors.
6. A decoy system according to any preceding claim and adapted to be movable by remote control.
7. A decoy system according to any preceding claim, wherein said means for deploying a particulate screen in space comprises means for disposing a smoke screen in space.
8. A decoy system according to Claim 7 wherein said smoke screen incorporates material to enhance its reflectivity.
11 -. ----4. -
9. A decoy system according to any preceding claim mounted in a buoy and adapted for use against anti-ship missiles.
10. A decoy system according to any preceding claim incorporating a radar decoy.
11. A method of decoying a missile having imaging sensors wherein a particulate screen is disposed in space and an image representing a target is projected onto the screen remote from said target and moved away from said target, thereby to deflect the missile.
12. A method according to Claim 11 comprising the step of generating a smoke screen to form said screen.
13. A method according to Claim 11 or 12 for decoying an infrared seeking anti-ship missile, comprising the steps of launching from a target ship, on detection of an approaching missile, a projector mounted on a buoy and projecting an infrared image of said target ship onto said screen.
14. A decoy system substantially as hereinbefore described with reference to the accompanying drawings.
15. A method of decoying a missile having an imaging sensor, substantially as hereinbefore described with reference to the accompanying drawings.
GB8713360A 1986-06-18 1987-06-18 Missile decoy system Expired - Fee Related GB2356034B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB8614818.6A GB8614818D0 (en) 1986-06-18 1986-06-18 Missile decoy system

Publications (4)

Publication Number Publication Date
GB8713360D0 GB8713360D0 (en) 2000-08-23
GB2356034A true GB2356034A (en) 2001-05-09
GB2356034B GB2356034B (en) 2001-08-15
GB2356034A8 GB2356034A8 (en) 2005-02-23

Family

ID=10599654

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB8614818.6A Ceased GB8614818D0 (en) 1986-06-18 1986-06-18 Missile decoy system
GB8713360A Expired - Fee Related GB2356034B (en) 1986-06-18 1987-06-18 Missile decoy system

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB8614818.6A Ceased GB8614818D0 (en) 1986-06-18 1986-06-18 Missile decoy system

Country Status (1)

Country Link
GB (2) GB8614818D0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2340858C1 (en) * 2007-04-09 2008-12-10 Военная академия Ракетных войск стратегического назначения имени Петра Великого Obstacle device

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111964532A (en) * 2020-06-02 2020-11-20 天津蓝马博达科技有限公司 People's air defense intelligent smoke screen transmitting system
CN112904379B (en) * 2021-01-28 2022-09-23 中国民航大学 GNSS induced deception jamming data generation method based on track

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2067273A (en) * 1980-01-04 1981-07-22 Gq Defence Equip Ltd Target Training Apparatus

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2067273A (en) * 1980-01-04 1981-07-22 Gq Defence Equip Ltd Target Training Apparatus

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2340858C1 (en) * 2007-04-09 2008-12-10 Военная академия Ракетных войск стратегического назначения имени Петра Великого Obstacle device

Also Published As

Publication number Publication date
GB2356034B (en) 2001-08-15
GB8614818D0 (en) 2000-08-23
GB8713360D0 (en) 2000-08-23
GB2356034A8 (en) 2005-02-23

Similar Documents

Publication Publication Date Title
US5198607A (en) Laser anti-missle defense system
Titterton A review of the development of optical countermeasures
US4143835A (en) Missile system using laser illuminator
US5333814A (en) Towed aerodynamic bodies
US5415156A (en) Method using solar energy
US5703314A (en) Infrared projector countermeasure system
US6626396B2 (en) Method and system for active laser imagery guidance of intercepting missiles
US4281809A (en) Method of precision bombing
CA2243685A1 (en) Target-tracking laser designator
RU2361235C1 (en) Method of detecting and tracking low-flying targets
US3743216A (en) Homing missile system using laser illuminator
RU2500035C2 (en) Method for remote exposure of hazardous object of given type to wave signals and apparatus for realising said method
EP0494092B1 (en) Method and apparatus for removing navigational hazards in water
McManamon et al. A history of laser radar in the United States
RU2141094C1 (en) Method protecting aircraft against rockets equipped with homing heads
GB2356034A (en) Missile decoy system
US12398983B2 (en) Applications of ultra-short pulse laser systems
RU2660518C1 (en) Method of radio-optical shielding of surface ship
Kopp The Sidewinder Story; The Evolution of the AIM-9 Missile
US20070183783A1 (en) Netted communication and weapons system for littoral warfare
Merritt et al. Field test of active tracking of a ballistic missile in the boost phase
Siam et al. Missile detection and destruction robot using detection algorithm
JP2023532299A (en) Incoming threat prevention system and method of use
RU2751260C1 (en) Protection system for moving ground objects from self-guiding and self-aiming high-accuracy ammunition on the march
RU2249172C1 (en) Method to defend military and civil objects against a fire of the weapons using the laser semi-active homing guidance systems (alternatives)

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20050608