WO2006096183A2 - Arme activee par une cible - Google Patents

Arme activee par une cible Download PDF

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Publication number
WO2006096183A2
WO2006096183A2 PCT/US2005/010323 US2005010323W WO2006096183A2 WO 2006096183 A2 WO2006096183 A2 WO 2006096183A2 US 2005010323 W US2005010323 W US 2005010323W WO 2006096183 A2 WO2006096183 A2 WO 2006096183A2
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WO
WIPO (PCT)
Prior art keywords
target
signal
ammunition
firing
firearm
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PCT/US2005/010323
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English (en)
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WO2006096183A3 (fr
Inventor
Oliver J. Edwards
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Individual
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Individual
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Publication of WO2006096183A2 publication Critical patent/WO2006096183A2/fr
Publication of WO2006096183A3 publication Critical patent/WO2006096183A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/06—Aiming or laying means with rangefinder
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
    • F41A19/58—Electric firing mechanisms
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/14—Indirect aiming means
    • F41G3/16—Sighting devices adapted for indirect laying of fire
    • F41G3/165—Sighting devices adapted for indirect laying of fire using a TV-monitor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/03—Cartridges, i.e. cases with charge and missile containing more than one missile
    • F42B5/035—Cartridges, i.e. cases with charge and missile containing more than one missile the cartridge or barrel assembly having a plurality of axially stacked projectiles each having a separate propellant charge

Definitions

  • This invention relates to weapons and more particularly to a novel weapon selectively capable of firing only on targets having a particular radiative characteristic.
  • the primary problem with firearm ineffectiveness in the field is the human involvement. This includes the time to notice and identify an uncertain and moving target, the time to bring the weapon into alignment, the erratic motion of the shooter at the best of times, his increased oscillation and shaking during combat, and the movement of the weapon as the trigger is jerked, and again as the firing pin plunges into the primer.
  • the soldier tends simply to fire as many bullets as he can as fast as he can in the general direction of the enemy, in hopes that some of them will hit something useful.
  • patent 5,392,688 (1995) shows a television camera as a weapon sight for aiming, wherein the user designates the "target” by placing the scope crosshairs on it and partially depressing the trigger. It is unclear why the user would at that point prefer simply to kill the target, this patent invokes an undisclosed "autolock-follow processor” circuit to differentiate and follow a target ignoring the background. Such capability is not generally known. Further, the weapon described simply as “fired electrically” and no useful firearm method is taught.
  • U.S. patent 4,370,914 (1983) teaches a gun-aiming method for calculationally averaging the swings of a rifleman's point of aim by gyroscopic measurement. The rifleman first designates the desired point of aim using his trigger switch.
  • a disadvantage is the use of a visible-light camera which greatly limits use in combat. Further, no method for electrically firing the weapon is taught, the electrical firing is simply invoked without teaching and there is no provision for correcting for the effects of angular velocity either of the target or of the weapon; thus aiming would only be accurate for a stationary weapon and stationary target.
  • U.S. patent 5,544,439 (1996) describes a modification to a prior art weapon with percussive firing, wherein the sear is operated by a solenoid in response to a target signal.
  • the target signal is generated by a single infrared detector at the focal plane of a lens. Since a single detector is used, the weapon provides no compensation for target or weapon motion; interpreting the signal to differentiate human radiation from other radiation patterns; and the use of electromechanical actuation has the disadvantages of firing pin jolt and solenoidal mass acceleration. Both of these are likely to cause a significant movement of the point of aim between electronic "fire" command and the exit of the bullet from the barrel.
  • U.S. patent 5,966,859 (1999) describes the use of infrared radiation from a target imaged on a pyroelectric quad cell through unspecified optical filters, to cause a solenoid to pull the trigger on a gun.
  • Pyroelectric detectors require the use of a mechanical chopper to modulate the incident optical beam on and off, with the inherent disadvantages of mechanical complexity, fragility and loss of half the target signal time and significantly limits the detection range due to electronic noise.
  • No method is taught for interpreting the signal to differentiate human radiation from other or for compensating the point of aim for target motion or weapon motion.
  • the aiming disadvantages of mechanical percussion firing are further increased by impulse motion and delay in action of a solenoid.
  • U.S. patent 6,174,288 (2001) couples the matter of 5,966,859 above with no abatement of the disadvantages.
  • Prior art inventions related to weapons almost all firearms taught since 1900 describe or assume ammunition loads to be cartridges pre-packaged with ammunition and primer, loaded one at a time into the weapon receiver, and mechanically discharged by percussion on the primer. After firing, the chamber is cleared and a new ammunition load is introduced for firing. This procedure can be done in a single shot or manual manner or, as in automatic weapons, the pace or loading and unloading procedure cycled faster so that multiple rounds or shots can be fired in quick succession.
  • the sequence is first to load the firing chamber with the proper cartridge followed by firing of that cartridge and removal of the residue or cartridge casing which is then replaced by another cartridge or ammunition load.
  • the method for igniting the propelling charge is typically mechanical: the fall of the firing pin on the primer.
  • the use of percussion primers and associated physical components in modern firearms has imposed constraints which have inhibited significant advances in accuracy, safety, performance and reliability.
  • Electro-percussive inventions are exemplified by the following.
  • U.S. Pat. No. 4,285,153 (1981) describe a form of axially preloaded magazine in which the ammunition loads are sequentially fired through a plastic tube, inserted as a unit behind a separate smooth-bore weapon barrel.
  • This disadvantageous separation of the ammunition from the barrel is overcome in U.S. Pat. Nos. 6,123,007 (2000) and 6,510,643 (2003), in which preloading of the actual barrel is taught.
  • U.S. Patents 4,332,098 (1982), 6,286,241 (2001) and 3,650,174 (1972) teach the use of a spring- loaded pin delivering a high voltage pulse to resistively heat and ignite the primer, which requires a relatively slow firing cycle.
  • U.S. Pat. No. 5,625,972 discloses an electrically discharged firearm in which a heat sensitive primer is ignited by a voltage induced across a fuse wire extending through the primer.
  • a laser ignited primer is disclosed in U.S. Pat. No. 5,272,828 (1993), wherein an optically transparent plug or window is centered in the case of the cartridge to permit laser ignition of the primer.
  • a long standing need has existed to provide a target sensor combined with a corresponding novel weapon which weapon incorporates a plurality of ammunition loads which may be electronically detonated so as to fire individual or multiple loads from within the same firing chamber, and thus be amenable to near-instantaneous firing response to electrical signals from the target sensor, without mechanical impulse or vibration.
  • a weapon comprises an electrically- actuated firearm, a target sensor, analytic and power electronics to actuate the weapon fire at such time both that the user has signaled a desire or readiness to fire and that a target is present at the expected point of strike of the missile.
  • the present invention provides a novel weapon having a target sensor unit comprising a target sensor and a target sensor processor, which transmits a "target-present" target sensor signal to a fire controller at such times that the point of missile impact coincides with a projected target position.
  • the fire controller creates a firing signal when it receives both a "target present” signal and a trigger signal.
  • a stock is provided for mounting one or a plurality of ammunition tubes and for incorporating a trigger mechanism.
  • a sequence controller means actuates a firing circuit means upon receipt of the firing signal.
  • An ammunition tube which houses a plurality of axially stacked ammunition loads wherein each load comprises a detonator, gunpowder, wadding and suitable missile.
  • the ammunition tube incorporates a firing circuit means, which may be electronically energized via the sequence controller for selectively detonating selected or respective ones of the plurality of ammunition loads.
  • the target sensor has an electronic fiducial mark which is adjusted to coincide with the conjugate image of the missile's expected point of impact.
  • the target sensor receives radiation from the target, and provides an image signal to the target sensor processor. Typically, this will be infrared radiation, and the preferred radiation for human targets will be detected in the waveband 6 to 20 microns, and preferably in the waveband of 8 to 14 microns.
  • the target sensor processor discriminates the target radiation from the background radiation and determines the velocity of the target relative to the average background, and transmits a "target present" signal to the firing unit when the projected target position is coincident with the fiducial.
  • the firing unit transmits a firing signal when both a trigger signal and a target present signal are received.
  • This firing signal causes the receiver firing circuit means to initiate a firing pulse which is received by the ammunition tube firing circuit means, and thereby ignites the gunpowder in the selected ammunition load to place the missile approximately on the centroid of the target.
  • An electronic sequence controller is operably connected between the trigger mechanism and the receiver firing circuit so that the sequence of firing of the ammunition loads for units is sensibly automatic and does not require any pre-selection on the part of the operator.
  • Means are provided within the bore of the ammunition tube for defining individual firing chambers therein and for accepting and distributing the forces of recoil into the barrel to prevent pre- ignition of the next propellant charge, and into the stock of the weapon for external support.
  • a manual fire selector switch means is provided, whereby the fire controller may be actuated and the weapon fired independent of any target sensor signal.
  • Fig. 1 shows a flow chart of the firing algorithm of the present invention
  • Fig. 2 shows a side-elevational view, partly in section, of a novel firearm or weapon incorporating the present invention
  • Fig. 3 shows a front-elevational view of the firearm or weapon shown in FIG. 2;
  • Fig. 4 shows a side-elevational view of a three-chambered ammunition tube employed in the weapon of Figs. 2 and 3, including its interface with the muzzle end of the receiver, with tube bore and typical internal ammunition loading indicated in dotted lines.
  • Fig. 5 shows a fragmentary sectional view of the ammunition tube receiver showing circular electrical conductors on the ammunition tube and congruent electrical conductors in the ammunition tube receiver;
  • Fig. 6 shows a side-elevational view of a three-chambered ammunition tube employed in the weapon of Figs. 2 and 3 and partly broken away to expose a typical ammunition or firing load;
  • Fig. 7 shows a side-elevational view of a target sensor employed in the weapon of
  • Figs. 2 and 3 and partly broken away to expose the lens means and the detector, and showing the ray traces from typical targets;
  • Fig. 8 shows a simplest detector element array;
  • Fig. 9 shows a quad-cell detector array, with an indicated target image
  • Fig. 10 shows a cruciform detector array
  • Fig. 11 shows a matrix detector array, with a multiplicity of typical target images
  • Fig. 12 shows a quantified target image on a matrix detector array
  • Fig. 13 shows a multiplicity of quantified target images on a matrix detector array
  • Fig. 14 shows a side-elevational view of a dual-waveband target sensor employed in the weapon of FIGS. 2 and 3 and partly broken away to expose the lens means, the beamsplitter, and the dual detectors, and showing the ray trace from an on-axis targets;
  • Fig. 15 shows the vector directions of the weapon and target motion in the far field, and
  • Fig. 16 shows a thermal image of a scene in the field, with a scan pattern of the user's point of aim.
  • the weapon will be described in two parts: the electrically controlled firing subsystem and the target sensor subsystem which controls the firing subsystem.
  • the electrically controlled firing system has two major subsystems: the target sensor unit and the firing unit. Starting from the top, the system has a power-saving on/off switch, not shown.
  • a target sensor creates a signal related to the scene which it images, and the signal is analyzed in the target sensor processor.
  • the target sensor processor outputs a signal when a target is detected and projected to be at the weapon's projected point of impact.
  • a trigger means creates a "fire" trigger signal which indicates the desire of the operator to have the weapon fire.
  • Signals from the trigger means and the target sensor processor are input to a fire controller which performs a logical AND operation, and from which ⁇ a signal is sent to the sequence control means.
  • the sequence control means energizes one of a plurality of conductors in the receiver firing circuit in the weapon stock, which signal is conductively transmitted to one of a matching plurality of conductors comprising the ammunition tube firing circuit in the proximal end of ammunition tube.
  • Each of the conductor pairs operates through the ammunition tube internal firing circuit to cause the discharge of a single ammunition load, if the operator actuates the trigger means AND if the target sensor processor indicates that a target is present at the point of impact, then the weapon fires one or more ammunition loads, in sequential order from the muzzle end to the receiver end of the ammunition tube.
  • an override means is provided as a "manual fire switch" which on closure enables the operator to discharge the weapon directly, at will, independent of signals from the sensor.
  • the present invention is illustrated in a side view which includes a target sensor 1, and a stock 2 having a recoil transfer means 13 extending from one end thereof.
  • the stock 2 also includes a trigger means 3 and a hollow ammunition tube receiver 5 which can insertably accept and fixedly locate one or more ammunition tubes 4.
  • the stock 2 has a hand grip 14A and trigger guard 14B and the recoil transfer means 13 is a shoulder interface.
  • the hand grip 14B serves to absorb the recoil.
  • the recoil means may be a mounting structure which transfers the recoil to the surface which supports the mounting structure
  • the ammunition tube 4 contains a plurality of contiguous axially stacked ammunition loads adjacent the receiver 5 and is terminated at the distal end with a barrel 15 which serves to direct the trajectory of the missile.
  • the ammunition loads are individually discharged by electrical signals from the sequence controller 9, which signals are transmitted to the ammunition load via the receiver firing circuit 6, the receiver tube electrical contacts 8B, the ammunition tube contacts 8A (here 8A and 8B are shown superimposed) and the ammunition tube internal firing circuit which is shown in a subsequent figure.
  • the trigger means 3 creates an electrical signal to the fire controller 10.
  • the target sensor 1 creates a signal to the target sensor processor 11 which analyzes the input signal to note the presence of a target, and transmits a "target present" signal to the fire controller 10.
  • the fire controller 10 typically will be a microprocessor means, and performs a mathematical AND operation on the inputs from the trigger means 3 and the target sensor processor 11 to create an output signal pulse to the sequence controller 9.
  • the sequence controller 9 discharges the ammunition loads sequentially, from the muzzle end to the receiver end.
  • These electrical operations are powered by a power supply 12, typically carried within the stock 2.
  • a manual fire selector 7 is a switch means which enables direct operation of the fire controller 10, such that the weapon is caused to discharge in a preset firing sequence independent of the signal state from the target sensor 1.
  • the preset firing sequence might be a single shot, or a plurality of sequential shots.
  • the preset firing sequence is stored in the fire controller 10, and is entered by the operator using a prior art data entry pad such as a key pad, which is not shown.
  • the firing signal generator, sequence controller, target sensor processor and power supply are shown as separate elements. Obviously these may be combined in one or more electronics units for manufacturing convenience.
  • the weapon of FIG. 2 is shown as having a single ammunition tube 4.
  • the receiver 5 will have a plurality of parallel ports which can insertably accept and fixedly locate a corresponding plurality of ammunition tubes 4. This multiplies the number of missiles which may be fired without replacing ammunition tubes.
  • this multiple-tube embodiment permits multiple types of ammunition loads to be installed for selected use, such separate ammunition tubes each containing for examples shotgun loads, or grenade loads, or solid shot loads.
  • the fire selector 7 will further provide for selection of the order in which the ammunition tubes are to be discharged.
  • the novel weapon of the present invention is illustrated in an end view of the muzzle end which further illustrates the target sensor 1, the receiver 5, and the barrel 15 where the lands 16 are shown.
  • the lands are raised spirals in the barrel which serve to rotate solid projectiles to gyroscopically stabilize their axes in flight.
  • the ammunition tube 4 is shown in an external view, with internal parts indicated in dotted lines.
  • the ammunition loads comprise propellant 18 and the missile assembly 17.
  • the ammunition tube firing circuit 19 is comprised of a plurality of conductors, each of which leads from a segment on the ammunition tube contacts 8A to the respective propellant load 18.
  • the ammunition tube firing circuit carries the electrical signal which ignites the propellant; the other side of the circuit , or "ground” is to the casing of the ammunition tube, which is further connected to one of the segments of the ammunition tube contacts 8A.
  • the electrical contacts 8A are individual circular rings stacked within a conical shape envelope, and insert into a congruent mating conical port in the ammunition tube receiver 5, which also serves to mechanically locate the receiver end of the ammunition tube 4 relative to the stock 2.
  • the circular symmetry of the electrical contact rings permits insertion and functioning of the ammunition tube in any rotational position.
  • the ammunition tube 4 is axially compressed into the ammunition tube receiver 5 by a captivation means linking the two elements comprising a ring 49 on the ammunition tube and a clamping means 50 or 51 affixed to the receiver.
  • the ring 51 affixed to the ammunition tube is clamped against a mating surface integral to the receiver 5, and is axially fastened thereto by a mechanical clamp means 52.
  • the ring 50 is of a ferromagnetic material and a mating ring 49 integral to the receiver 5 provides the axial clamping force, where either or both rings 49 and 50 are of magnetized material.
  • the ammunition tube can be preloaded at the factory or by the user in the field, serving as a magazine of ammunition loads.
  • this loaded ammunition tube can be quickly installed into the ammunition tube receiver 5 as a preloaded magazine.
  • the expendable ammunition tubes which also serve as a barrel for directing the missile are thus quickly replaceable.
  • the weapon of the invention can be fired in burst rates of tens of thousands of rounds per minute; in that greatly accelerated barrel erosion attendant on such extraordinary fire rates is acceptable since the barrel is always or often new.
  • the ammunition tube receiver 5 is shown in cross section.
  • the ammunition tube receiver 5 and the ammunition tube 4 have a conical congruent interface for relative mechanical location in three dimensions, and to thus position the receiver tube contacts 8B of the conductors of the receiver firing circuit 6 so that in operation they electrically contact ammunition tube contacts 8A, respectively.
  • the conductors of the receiver firing circuit 6 are terminated in conical electrodes 8A integral with the conical port; in another embodiment the conductors 19 terminate in spring-loaded contacts which abut the ammunition tube contacts 8A upon insertion of the ammunition tube 4 into the ammunition tube receiver.
  • FIG. 6 the ammunition tube and exemplar ammunition loads are illustrated in partial cross section.
  • three different types of ammunition load are shown loaded sequentially.
  • wadding 2OA seals the propellant 18A.
  • a detonation plate 22A closes the ammunition load at the muzzle end. This detonation plate is key to the successful operation of the weapon: it serves to limit the rearward shock transferred to propellant 18A when the preceding propellant 18B is ignited.
  • the detonation plate 22A is concave toward missile 21 A, and at installation provides a seal across the bore of the ammunition tube.
  • a compressible or crushable plug 53 serves at assembly to transmit axial forces to ram the sequential ammunition loads through the muzzle.
  • the compressible plug Upon discharge of the preceding propellant, and the consequential axial flexure of the detonation plate 22 A, the compressible plug permits a small axial flexure of the detonation plate to occur without transfer of the shock to the next missile 21A.
  • the different ammunition load shown subnumbered "B" wherein a quantity of small shot constitutes the missile.
  • This "shotgun" ammunition load similarly comprises propellant 18B, wadding 2OB, and missile shot 21B, and is closed at the front by detonation plate 22B.
  • a compressible plug is not needed to allow the small flexure of the detonation plate when the prior ammunition load is fired.
  • the compressible plug 53 may replace the wadding 2OA, and the conical seal of the detonation plate may be made integral with the side wall of the missile 21A.
  • the missile would move slightly rearward on discharge of the preceding ammunition load, and thereby would seal its own firing chamber by expansion and pressure of the conical skirt of the detonation plate against the inner surface of the ammunition tube.
  • a weapon system has no moving parts other than the missiles and has the advantages of low cost in manufacture, light weight, high reliability and great ruggedness in the field. It utilizes a barrel only for one set of ammunition loads (or a few sets, if reloaded) and has the advantages of low cost in manufacture and enables the use of thin barrels of lightweight materials.
  • a conventional automatic firearm must withstand the shock, pressure and bore erosion of firing thousands of rounds, the limited firing through the bore of the present invention allows for the use of unconventional materials and manufacturing methods.
  • Such unconventional manufacturing methods may include the use of lightweight metals and the use of circumferential fiber strengthening, among others.
  • this limited-life barrel can potentially decrease the weight of the loaded weapon by several pounds.
  • a weapon made according to the present invention has the further advantage of rapid reloading in the field by insertion of a new ammunition tube. It has the advantage of extreme rate of fire, in excess of 10,000 rounds per minute if desired, since the successive missiles are launched by electronic rather than mechanical cycling. A second round may be fired immediately after the first, traveling close behind it while passing through the barrel, and thus maintaining a high compression of the propellant gases; this has the advantage of greatly increasing the velocity of the first missile, e.g., for armor piercing or greater range. Finally it has the great advantage that the instant of fire can be controlled by electronic impulse from a firing circuit, enabling the practical use of a computer firing solution from a target sensor.
  • TARGET SENSOR TARGET CENTROID
  • a lens means 23 serves to project the image 26 of a distant target 25 on a sensing reticle 24.
  • a second target 27 is shown imaged 28 on the sensing reticle.
  • the lens means might be reflective or refractive, adapted to focus a high quality, achromatized "color-co ⁇ ected" image of a distant object onto the sensing reticle 24.
  • the waveband of transmission of the lens means 23 and of the sensing reticle responsiveness is in the range of 6 to 20 microns and preferably within the range of 8 to 14 microns.
  • the electromagnetic radiation from objects at the temperature of human targets peaks in this preferred waveband, while the radiation from cooler foliage of vehicles or buildings is significantly less in this waveband.
  • the reticle 24 generates a signal which varies monotonically with the temperature of the distant object field within the projected image of the reticle, which signal is transmitted to the target sensor processor.
  • the reticle 24 is comprised of detector elements which in concert yield information about the location and properties of target radiance falling on the reticle.
  • the detector elements may be larger or smaller than the image of the target. Preferably it is smaller: the irradiance from a target is thus divided over a multiplicity of contiguous detector elements, to facilitate enhanced location of the center of target irradiance.
  • Detectors for infrared use may operate uncooled, or may be cooled to decrease internal noise and thus to increase the sensitivity of the detector element to a given irradiance.
  • the reticle will operate uncooled and thus consume no power for refrigeration.
  • uncooled arrays of detector elements include silicon for the visible and indium antimonide or InGaAs for the near infrared (3-5 micron wavelength).
  • the thermal infrared (6-20 micron) radiation can be detected by microbolometers, such as vanadium oxide or barium strontium titanate elements, whose electrical properties change measurably in response to a varying thermal radiation load.
  • Another method of radiation detection uses small mechanical elements which deform under temperature change, thus changing the capacitance of each element against a stationary reference electrode.
  • Arrays of vanadium oxide or barium strontium titanate elements are commonly used in infrared cameras for fire fighting or night vision, and are preferred materials for the target detector reticle.
  • a "target present" signal is generated by the target sensor processor 11 (FIG. 2) whenever the single detector element 29 receives radiation in excess of the background radiation by an amount which is greater than a selected positive change in signal called the "threshold".
  • This selection of “threshold” by the operator corresponds to a preference either for higher sensitivity to small or distant or cooler targets, or for fewer “false positives” where the weapon would discharge at a merely warmer but non-target spot.
  • the "threshold” is factory set or else adjusted as an input to the target sensor processor by a prior art keypad or similar control device (not shown).
  • the background radiation is continually measured by a separate element or elements 30 added to the reticle, which is used for measuring the radiation from a spot or spots well separated from the reticle sensor area, as representative of the background radiation.
  • Positive difference between the reticle signal above the reference detector signal is indicative of a possible target "hot spot”.
  • Negative difference is ignored in the signal analysis, as indicative of a hot spot passing before the reference detector but not the reticle.
  • the signal from the reticle is electronically averaged over a time period of the order of a second as the image sensor is angularly moved or swept across the background, to generate a normative background signal level.
  • the reticle must be mechanically adjusted relative to the lens, to place the detector element on the projected point of strike.
  • This is commonly referred to as "sighting in” the weapon system.
  • this will be implemented by moving the reticle vertically and horizontally to correct for range and “windage” respectively, which includes the specific parameters of mechanical mounting and the weapon itself.
  • the entire target sensor is similarly moved in a prior art adjustable cradle ("scope mount").
  • a third dimension of adjustment (focus) is desirable only for cases where close, small targets are expected.
  • the optical system is factory adjusted or focused to the "hyperfocal" range, at which setting the targets will be usably in focus over the useful range of the weapon..
  • this single element has limited angular resolution, or pointing precision: no data indicates which portion of the reticle element is illuminated.
  • a sharply focused image of a distant, suitable hot radiator could illuminate any portion of the element and yield the same electrical signal.
  • a target sensor lens means with a focal length of 100 mm, and a typical reticle element size ("D") of 100 microns ( ⁇ ) square
  • D reticle element size
  • the projected image of the reticle at 250 meters will be a square 25 X 25 centimeters, and the perceived radiation could have come from any spot in that square. This is marginally acceptable resolution for a firing solution.
  • the target sensor processor the firing signal be generated when the temporal first derivative of the signal from an indicated target is zero and second derivative is negative, as the weapon is slowly scanned across the target. This will in general put the point of impact at the radiative center of the target.
  • FIG. 9 another embodiment of sensing reticle is shown as a "quad cell" detector array.
  • One example of such a detector array is the SPS240EN from Fuji & Company, Osaka, Japan. Four detectors are contiguous in a 2 X 2 configuration.
  • the sum of the normalized signals from the upper two elements, subtracted from the sum of the normalized signals from the lower two elements is a measure of the vertical position of the centroid of the irradiance on the four detectors.
  • the sum of the normalized signals from the left two elements, subtracted from the sum of the normalized signals from the right two elements is a measure of the horizontal position of the centroid of the irradiance on the four detectors.
  • the precision multiplier For a noisy detector and a dim target the precision multiplier might decrease to 10; using a low-noise detector and amplifier and with a bright target, the precision multiplier might increase to 1000 or more.
  • the method can be generalized from a 2X2 matrix to an NXM matrix of any desired size, where the weighted moment of the irradiance of each detector element is summed in orthogonal axes, to establish the position of the centroid of the irradiance in those axes.
  • the background radiation signal is first subtracted from the signal of each detector element to establish a measurement of the increased signal received from a target. This background radiation is established either by a long-time average (of the order of a second) of the signals, or else by the use of a reference detector element (not shown) well separated from the quad cell detector elements, to measure the radiation from the off-target field.
  • FIG. 10 another embodiment of sensing reticle is shown as a cruciform array 33 of detector elements.
  • This open array may be operated in a calculational formalism analogous to the quad cell array of FIG. 9.
  • the moments of the signals from each of the elements in the horizontal rows are added to horizontally locate the centroid of the target "blob" image
  • the moments of the signals from each of the elements in the vertical rows are added to vertically locate the centroid of the target "blob". That is to say (for the example of the horizontal direction):
  • K is the horizontal location of the centroid of the illumination
  • the average background signal is subtracted from each elemental signal to measure the incremental illumination from a target: the "net" signal.
  • the background radiation may be established by a moving time average of the detectors' total irradiation as the image sensor is scanned around, or else by a separated detector element 30 which may be taken to be unilluminated by the target.
  • a preferred embodiment of sensing reticle is shown as a filled regular array of detector elements.
  • a detector array might be for instance pyroelectric or a microbolometer array.
  • a preferred embodiment would use a microbolometer array because it can "stare". I.e., it does not require that the input irradiance to be amplitude modulated by a mechanical chopper.
  • Such staring microbolometer arrays are made by Indigo Systems, Raytheon, Lockheed-Martin, and Mitsubishi. For example Raytheon has made an uncooled 15x30 element microbolometer array of modest cost which can operate at 200 frames per second.
  • Such an array is schematically depicted in FIG. 11.
  • each target irradiance "blob" falls on one or more detector elements.
  • the "blob" shape may be unresolved if it is illuminating but a single element, it may be partly resolved into a recognizable man-image if illuminating a sufficient number of detector elements.
  • a variety of exemplar target "blobs" or target images is now described, together with the accuracy with which one may measure the position of the centroid of the irradiation pattern of the blob.
  • the signal from the most irradiated detector element 35 is adjacent a less irradiated detector element 36 and an even less irradiated element 37.
  • the accuracy by which the centroid of this target image may be located vertically is of the order of 1% of an element dimension D, while the horizontal position (assumed at the vertical centerline) is actually accurate only to ⁇ D/2 because only one row of elements is irradiated.
  • Target blob 38 as compared with the other blobs is indicative of a target which is larger and/or nearer, and the availability of bilateral data over a multiplicity of detector elements permits the centroid of the target to be located to within approximately ⁇ 1% D in both horizontal and vertical directions.
  • the small single- element blob 39 is indicative of a target which is angularly smaller than one detector; its centroid is best assumed to be at the center of the element, and thus the aiming accuracy has a tolerance of only ⁇ D/2 in horizontal or vertical directions.
  • the aim point 34 is electronically stored in the signal processing electronics as differences among pairs of elements as already described for a quad cell, in order to give the aim point definition the accuracy of the order of ⁇ 1% of D.
  • the aim point is located by conventional sighting-in firing tests, using a radiating target approximately the size of the projected image of several detector elements, through the center of which the projectile passes when the weapon system is sighted in.
  • the point of aim is preferably further offset in the direction of the weapon's motion to account for ("lead") for the change of firing direction between the firing impulse and the instant the missile leaves the end of the barrel. This additional correction in the point of aim offset angle is calculated by the target sensor processor.
  • the weapon In actual use the weapon is generally not stationary, but wavers and moves according to the motion of the shooter. This significantly increases the absolute accuracy of the aiming operation. As the weapon's point of aim is normally moved around more or less steadily, each of the least-detectable target blobs will sequentially cross intersections between contiguous detector elements and allow the ⁇ 1%D accuracy positional measurement whenever the irradiance is on two or more such elements. A straight-line extrapolation of this time track will yield the same predictive positional accuracy even though the target image may be smaller than a single detector element.
  • a lens means having a focal length of 25 mm, and a sensing reticle as depicted in FIG.
  • each element is the image of a 1 meter square at 250 meters distance: approximately the cross section of a man target.
  • the accuracy of locating the centroid of a target image spread across a plurality of elements would be of the order of ⁇ 1 centimeter at 250 meters, depending on the noise level of the sensing circuitry.
  • a further advantage of the present invention is that a relatively low-resolution detector array as depicted in FIG. 11 can be used for extreme precision in weapon sighting, which detector array thus can be small and consequently low in cost and package size.
  • FIG. 12 a more detailed example is shown wherein a target image is spread across a plurality of elements. Here the signal strength from each element is indicated numerically in the element. IfRi, R 2 , ...R n are the vectors from some point on the sensing reticle to the center of the nth element, and if the signals from each reticle are
  • FIG. 13 various target blobs are shown and the signal strength from each element is indicated numerically in the element.
  • the irradiance pattern on the detector is plotted at the bottom of the figure for the horizontal or X- direction, and is representative of the blob's signal strength.
  • the blob on the left has horizontal irradiance curve 43, and is "well behaved", having but a single peak.
  • the blob on the right is more complex, having two peaks in curve 44; this is symptomatic of the presence of two adjacent but not superimposed targets.
  • a mathematically very simple method separates the complex blob into separate target blobs wherever the first derivative of the curve 44 is zero and the second derivative is positive; this is taken as the mid-point between each hypothesized pair of targets.
  • More complex analytical approaches may be used, such as modeling the data subtracted from a first blob by separating the two blobs, based on symmetry considerations using the measured half of the first blob, but such vernier correction are not likely to measurably increase the number of target casualties.
  • prior art methods for "blob analysis" exist in the literature 1 ' 2 ' 3 for separating complex but unresolved blobs into multiple entities, the centroid of each of which may be calculated as a separate target.
  • a target sensor 1 of a preferred embodiment is depicted wherein additional components enable the rejection of targets which are hotter than the expected target temperature. For instances, it is desirable not to automatically fire at an exhaust pipe or a tungsten lamp.
  • a broadband lens means 48 is used which is achromatized for both near infrared (3-5 ⁇ ) and for long infrared (8- 14 ⁇ ) wave length imaging. The lens means 48 focuses the image of a distant target on a first sensing reticle 24 as previously described.
  • the focused beam 47 from the distant target is additionally focused on a second sensing reticle 45 via a beamsplitter means 46 which separates the 3-5 ⁇ and the 8-14 ⁇ wavebands (e.g., passing the longer wavelengths and reflecting the shorter wavelengths).
  • the two reticles are conjugate; that is to say, at the target the image of any detector of the first sensing reticle is superimposed and congruent to the image of the corresponding element of the second sensing reticle.
  • the signals from the corresponding elements are compared to eliminate further signal processing of elements which are exposed to radiators of temperatures higher than that of the expected target.
  • data from the element Ni (long waveband) is dropped from further consideration if there is a signal above a selected threshold from the corresponding element Mj (short waveband).
  • data from the element Ni (long waveband) is dropped from further consideration if the signal the corresponding element Mi (short waveband) is greater than a selected threshold fraction of the Ni signal.
  • each blob is computed using, e.g., the technique of block- based MPEG video compression. Both the angular velocity of the average background (from weapon motion) and angular target motion relative to the average background are readily calculated, and the moment of intersection of the angular motion of the target centroid with the aim point is performed by straight-line prediction. Straight-line (linear) prediction suffices due to the very short lag times relative to the limited human potential for acceleration.
  • the point-of-aim offset angle has two components: bullet drop and weapon motion.
  • a range (elevation) correction can be set in for "bullet drop” if needed by very long range. We note that within ⁇ 1.5 inches of allowable vertical error no range correction is needed for an M16 military rifle with usual ball ammunition, out to 250 meters' range: the bullet rises 1.5" above the boresight at approximately 150 meters and drops to 1.5" below the boresight by 250 meters. At greater ranges the elevation correction may be made manually or be made automatically from an electronic range measurement, such as an optical laser rangefinder. Such an automatic correction for
  • ki is a constant of proportionality related to the weapon and missile design.
  • the weapon will be moving.
  • one of the likely modes of use of the invention will be to scan the weapon across the background, letting it fire whenever it detects a target in the compensated point of aim.
  • the measured fixed time between "fire" signal from the target sensor processor and the bullet's leaving the barrel corresponds to the weapon-motion error angle Da as a correction to the aim point: i.e., the motion-related angular offset of point of strike from instantaneous point of aim when the firing signal is initiated.
  • the instantaneous angular velocity of the weapon is proportional to the measured velocity of the background across the image sensor, measured as already described.
  • the electronic point of aim must be offset by an amount corresponding to that delay. Simply enough the required weapon-motion lead angle ⁇ 2 is
  • k a factory constant of proportionality, including fixed optical and mechanical factors
  • the total electronic offset angle of the point of aim is the vector sum ⁇ i + ⁇ 2 .
  • the correct condition for a "fire" signal from the target sensor unit is that the heads of the vectors are superimposed: at that instant, a fired missile will arrive on the projected position of the target - based on straight-line extrapolations.
  • FIG. 15 Such an imagined video image is illustrated in FIG. 15.
  • the point of aim offset angle 5OB from the point of aim 5OA is in this instance down (bullet drop) and to the right (weapon swinging to the right).
  • the target offset angle 51B from target 51A is down and to the left (the trajectory of a target, e.g., moving down a hill face).
  • the other target 52 being tracked by the target sensor processor is moving essentially horizontally right.
  • the point-of-aim offset angle 50B terminates just where the target offset angle 51B terminates, as measured from the point of aim 5OA and the target
  • the discussion above has disclosed a method and apparatus for rejecting false hot spots, and for locating the centroid of a target within a fuzzy blob, and for correcting the point of aim for the effects of target motion and for weapon motion.
  • a final algorithmic calculation is "coring" the target blob.
  • firing is actuated anywhere within a central zone of the target blob, but not in the outer zone. This is particularly needed when the target is close and subtends a significant number of pixels. For example: If in the exemplar detector system already described the target is 25 meters distant, a man target in the above example would be 20 pixels tall X lO pixels wide. Clearly, hitting the centroid of this target is less important than hitting anywhere in the central zone of the target.
  • the central zone is bordered by a radiance contour which is a chosen ratio, e.g., halfway between the peripheral (or background) radiance and the peak central radiance. This is algorithmically conveniently located where the second derivative of the contour of the target blob is zero. Shots anywhere within such a central core of the target blob will then suffice to create a casualty.
  • all the signals from a sensing reticle comprised of a filled regular array of detector elements may be conducted to an image display such as a magnified flat panel display (FPD).
  • the FPD might for examples be an organic light emitting diode or a liquid crystal display.
  • a miniature FPD is fitted with a magnifier eyepiece and mounted on the stock with its axis parallel to the optical axis of the target sensor, or else head- or helmet-mounted.
  • Such an additive display for the target sensor enables the operator to visualize targets not otherwise visible, and to intentionally move the point of aim onto the selected target center.
  • This embodiment of the weapon system provides much of the utility of prior-art day and night awareness of the distant field situation using thermal infrared viewing telescopes, but at a fraction of the current size, power and cost.
  • servo drive motors may be added to the support means in order to aim the weapon on command of a search engine, providing a robotic weapon system which is effective against targets within the search pattern without the attendance of an operator.
  • a search engine has programmed patterns of searching an environment seeking targets, such as a repeating geometric pattern of scan, or by indication from thermal or motion sensors.
  • Fig. 16 a representation of one method for using the invention is depicted, adapted from an actual infrared telescope image of relatively low resolution.
  • Five human targets are shown running in front of the buildings.
  • the rifleman in the dark has pulled the trigger and blindly swung his point of aim back and forth, with no certainty of where the enemy is, except perhaps generally from sound or a light flash.
  • the target-actuated weapon of this invention can be used to greatly increase the number of missiles fired with effect to hit targets, and greatly decrease the number of missiles fired to miss targets. It is capable of adjusting the instantaneous projected point of strike of the missile to compensate for weapon and target motion. Furthermore the target-actuated weapon has additional advantages among which are:

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

L'invention concerne une arme pour lancer un projectile d'arme à feu sur un point de frappe (34) d'une cible (25). Cette arme comprend une arme à feu électriquement actionnée dotée de munitions axialement empilées (4), une unité de détection de cible (1) générant un signal de détection de cible, lorsque le point de frappe (34) projeté et que la position cible projetée coïncident; un contrôleur de tir (9) générant un signal de tir lorsque, à la fois un signal de déclenchement et un signal de détection de cible sont présents; et un contrôleur de séquence (10) actionné par le signal de tir pour mettre feu à au moins une munition axialement empilée (4) afin de lancer le projectile sur l'emplacement projeté d'une cible (25).
PCT/US2005/010323 2005-03-03 2005-03-28 Arme activee par une cible Ceased WO2006096183A2 (fr)

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US11/071,680 2005-03-03

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011096854A1 (fr) * 2010-02-02 2011-08-11 Saab Ab Procédé et agencements permettant de tirer avec une arme à feu
WO2012131548A1 (fr) * 2011-03-28 2012-10-04 Smart Shooter Ltd. Arme à feu, système de visée pour celle-ci, procédé d'utilisation de l'arme à feu et procédé pour réduire la probabilité de manquer une cible
US9127909B2 (en) 2013-02-17 2015-09-08 Smart Shooter Ltd. Firearm aiming system with range finder, and method of acquiring a target
US9850241B2 (en) 2014-03-18 2017-12-26 Idorsia Pharmaceuticals Ltd Azaindole acetic acid derivatives and their use as prostaglandin D2 receptor modulators
CN110595426A (zh) * 2019-10-11 2019-12-20 北京理工大学 一种弹载着角测量系统及测量方法
US10782097B2 (en) 2012-04-11 2020-09-22 Christopher J. Hall Automated fire control device

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LU46404A1 (fr) * 1964-06-26 1972-01-01
GB1605027A (en) * 1977-04-07 1981-12-16 Emi Ltd Aiming arrangements
US4402251A (en) * 1981-09-18 1983-09-06 The United States Of America As Represented By The Secretary Of The Army Detection of line of sight reversal and initiation of firing commands for a modified acceleration predictor fire control system engaging maneuvering targets
NL9500285A (nl) * 1995-02-16 1996-10-01 Hollandse Signaalapparaten Bv Vuurleidingssysteem.
FR2794059B1 (fr) * 1999-05-31 2001-08-10 Gemplus Card Int Dispositif portable a circuit integre et procede de fabrication

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011096854A1 (fr) * 2010-02-02 2011-08-11 Saab Ab Procédé et agencements permettant de tirer avec une arme à feu
US8989449B2 (en) 2010-02-02 2015-03-24 Saab Ab Method and arrangements for firing a fire arm
WO2012131548A1 (fr) * 2011-03-28 2012-10-04 Smart Shooter Ltd. Arme à feu, système de visée pour celle-ci, procédé d'utilisation de l'arme à feu et procédé pour réduire la probabilité de manquer une cible
US10097764B2 (en) 2011-03-28 2018-10-09 Smart Shooter Ltd. Firearm, aiming system therefor, method of operating the firearm and method of reducing the probability of missing a target
EA031066B1 (ru) * 2011-03-28 2018-11-30 Смарт Шутер Лтд. Система прицеливания огнестрельного оружия (варианты) и способ управления работой огнестрельного оружия
US10782097B2 (en) 2012-04-11 2020-09-22 Christopher J. Hall Automated fire control device
US12222191B2 (en) 2012-04-11 2025-02-11 Christopher J. Hall Automated fire control device
US9127909B2 (en) 2013-02-17 2015-09-08 Smart Shooter Ltd. Firearm aiming system with range finder, and method of acquiring a target
US11619469B2 (en) 2013-04-11 2023-04-04 Christopher J. Hall Automated fire control device
US9850241B2 (en) 2014-03-18 2017-12-26 Idorsia Pharmaceuticals Ltd Azaindole acetic acid derivatives and their use as prostaglandin D2 receptor modulators
CN110595426A (zh) * 2019-10-11 2019-12-20 北京理工大学 一种弹载着角测量系统及测量方法

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