The present invention relates to locating mobile targets, and more particularly, the present invention relates to an improved system for tagging, tracking, targeting and termination (T4) of mobile targets.
There is a need in the art for a real-time integration of command and control, intelligence, surveillance, and reconnaissance (C4ISR) and attack functions at a target. The current targeting and attack process is dependent on coordination through the Air Operations Center or an equivalent controlling agency. This off-target coordination requires time-consuming communications that could allow the target to escape and (in the case of a very lethal target such as an mobile Intercontinental Ballistic Missiles) allow the target sufficient time to launch its weapons prior to destruction. Currently, target selection requires a significant period of time and a significant amount of resources. This is particularly difficult and laborious (and more often than not, unsuccessful) in the case of mobile targets. A few examples of how this is currently accomplished follows:
1) Forward Air Control (FAC) Mobile Target Identification: A forward air controller will identify targets within a general area and report the target types, general location, bearing and heading back to the Air Operations Center. The Air Operations Center will determine if the targets warrant destruction and if so, will order an air strike via the most effective assets within the general target area. The strike leader then proceeds to the general vicinity of the target based upon original target information and any updated target location information. The strike team then begins a search pattern in order to locate and confirm the target. This process is frequently unsuccessful due to a number of factors (i.e. time between target reporting and strike sortie, weather, time of day, and target directional changes since last known sighting, etc.) and also causes the strike team to be subjected to a significant level of risk as they engage in a predictable and time consuming search pattern which could allow enemy surface-to-air missiles to engage the strike team due to increased loiter time. Additionally, target confirmation is also a difficult process, and at night is even more difficult. Once the target is identified, then the strike team employs weapons which are suited for the task, generally more expensive/standoff weapons unless visual identification is easy and no known threats are in the area. Frequently, however, conditions cause the aircraft to come within range of enemy anti-aircraft weapons.
2) Non-Mobile Target Identification—Frequently non-mobile targets are selected based upon satellite (or reconnaissance aircraft) imagery, however, this has its limitations and often ground assets are required for target confirmation. Even in the case of non-mobile targets, the target may not be destroyed or the wrong target destroyed because the technique used to locate the intended target may be severely flawed. In an effort to pinpoint the location of the target land navigation techniques have been employed. These techniques, called ‘intersection’ and ‘resection’, are only adequate to provide a general location and are not accurate enough to provide the actual location required for aerial targeting. As a result, targets may be mistakenly identified, when in fact, its actual whereabouts may be thousands of feet away.
Therefore, there is a need in the art for a system and method for remote tagging, tracking, and targeting of target locations and a more rapid, precise, safer, inexpensive and less complex method of mobile target termination. There is also a need for the ability to precisely tag non-mobile targets to decrease the likelihood of accidental destruction of the wrong target.
One embodiment of the present invention provides a system for tagging and locating a target. The system includes a projectile frangible on impact, a RF tagging system located in the projectile, and a bonding agent located in the projectile. The RF tagging system may include a RF circuitry, an antenna, and a power source. The RF circuitry may include a circuit board, a processor, and a resonator. The antenna may be a dipole antenna. The bonding agent may include polybutene or polyisobutene.
In another aspect of the invention, the projectile includes a cover that forms a distal end of the projectile. The cover may be scored to enable the cover to be frangible upon impact of the cover with the target. In another aspect of the invention, the RF tagging system includes a reflective circuitry, that enables the RF tagging system to be selectively powered on and off. The selectively powering on and off through the reflective circuitry may be accomplished through a radar transmission. In yet another aspect of the invention, a GPS device may be used to determine the location of the system. The location may be determined by the GPS device through transmission through the antenna to a cellular phone tower for transmission to a cellular phone receiver. In yet another aspect, the RF tagging system transmits a signal to at least three cellular towers to determine the location of the RF tagging system. In yet another aspect of the invention, the RF tagging system and bonding agent are delivered to the target using a delivery device, such as a gun.
Another embodiment of the invention provides a method for tagging and locating a target including the steps of providing a RF tagging system, providing a bonding agent for affixing the RF tagging system to the target, and inserting the RF tagging system and the bonding agent into a projectile for transporting the RF tagging system and bonding agent.
Another embodiment of the invention provides a system for tagging and locating a target that includes a RF tagging system, wherein the RF tagging system comprises RF circuitry, antenna, and power source, a bonding agent for affixing the RF tagging system to the target, a GPS receiver for determining the location of the tagging system, and a projectile for containing and transporting the RF tagging system, bonding agent, and GPS receiver, wherein the projectile is frangible on impact.
Yet another embodiment of the invention provides a system for tagging and locating a target that includes a RF tagging system, wherein the RF tagging system comprises RF circuitry, antenna, and power source, a bonding agent for affixing the RF tagging system to the target, a GPS receiver for determining the location of the RF tagging system, and a projectile for containing and transporting the RF tagging system, bonding agent, and GPS receiver, wherein the projectile is manually affixed to the target.
The present invention now will be described more fully hereinafter with reference to the accompanying drawings, in which exemplary embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will convey the scope of the invention to those skilled in the art.
The present invention includes systems and methods for tagging a target for subsequent locating through the use of a radio frequency system (“RF tagging system”). The tagging also may be used to prepare a battlefield in advance for an attack force by enabling both tactical level command , control, communication, computer, intelligence, surveillance, and reconnaissance (“C4ISR”) platforms and attack platforms to share the same source of real-time target location information. The RF tagging system may form the common operating picture key to time-critical-targets and precision strike by providing location information of a target based upon real-time precision location of time-critical-targets. A target set may include a static or a mobile target, such as a truck, tank, scud, other vehicle, or missiles or even individual/multiple enemy personnel who are tagged.
As illustrated in
The RF circuitry 12 may create an RF signal that has a RF signal power which is transmitted through the antenna 14. The antenna 14 included in the RF tagging system 10 may be of any configuration that permits transmission from its location. In an exemplary embodiment, the antenna 14 is a dipole antenna. In the exemplary embodiment, the antenna has a one quarter inch wavelength dipole. The present invention is not limited to dipole antennas but may include any antenna configuration including logarithmic antennas.
The power source 16 included in the RF tagging system 10 is used to power the system. The power source 16 may be any source that provides sufficient power to operate the RF circuitry and antenna, such as a battery or a thermoelectric device. In an exemplary embodiment, the power source is at least one button battery. One of ordinary skill in the art will appreciate that any battery may be used herein.
The RF tagging system 10 may be miniaturized so as to be covert to limit detectability of the RF tagging system 10 when attached to the target. In an exemplary embodiment, the RF circuitry 12 measures approximately 1.2 millimeters in diameter. One of ordinary skill in the art will appreciate that the RF circuitry 12 may be any size and is not limited to the embodiment illustrated herein. In another exemplary embodiment, the RF circuitry 12, antenna 14, and the power source 16 are collectively approximately 9 millimeters by 9 millimeters. One of ordinary skill in the art will appreciate that the RF tagging system 10 is not limited to the sizes described herein but may be of any dimension suitable to track a target of interest. Furthermore, the RF tagging system 10 may be a single device wherein the RF circuitry 12, antenna 14, and power source 16 are integrated. One of ordinary skill in the art will appreciate that the RF tagging system 10 may be one device or any number of devices combined for operation.
As illustrated in
The RF tagging system 10 and bonding agent 22 may be inserted into a projectile 24 for delivery of the device to a target 20. The projectile 24 may be of any configuration that allows delivery of the projectile 24 to the target 20. For instance, in an exemplary embodiment, the projectile 24 may be any caliber projectile such as a 22 caliber, 0.45 caliber, 9 mm or any other caliber projectile and is not limited to use with 0.45 caliber weaponry. The projectile 24 may be fired from any standard gun or any other specially designed device that can deliver the projectile 24 to the target 20. The projectile 24 when fired will maintain its orientation during flight to the target 20 and impact with the tip of the projectile.
In an exemplary embodiment, the projectile 24 is a 0.45 caliber gun delivery system that attaches the RF tagging system 10 to the target 20. The 0.45 caliber is a common weapon with sufficient power to attach the RF tagging system 10 on the target 20. The 0.45 caliber round maintains its orientation during flight to the target 20 and impacts with a predictable orientation ensuring that the bonding agent 22 impacts first and the antenna 14 remains exposed. One of ordinary skill in the art will appreciate that the RF tagging system 10 may be delivered by any ballistic system including any caliber projectile. However, for illustrative purposes only, the 0.45 caliber projectile and gun will be used as examples throughout the remainder of this application.
The RF tagging system 10 may be packaged into a projectile 24 for delivery to the target. The package may include the RF tagging system 10, wadding 26, and propellant 28, The RF tagging system 10, wadding 26 and propellant 28 may be enclosed in a encasing 30. In an illustrative embodiment, the encasing 30 is made of aluminum, however any metal or other non-conductive material is contemplated herein. The encasing 30 may also be any shape. In an illustrative embodiment, the encasing 30 is cylindrically shaped.
The wadding 26 may be used as a space filler in the encasing 30 which also effects the distance and accuracy of the projectile 24. The wadding 26 may be cad fiber or any other material that may be packed into the encasing 30. The amount of wadding 26 may affect the flight of the projectile 24 of which the encasing 30 is incorporated into. For instance, in an exemplary embodiment, a 2 gram wadding 26 in a 0.45 caliber projectile may allow the projectile 24 to travel approximately 50 yards. On the other hand, 4 grams of wadding may allow the projectile 24 to fly 100 yards. Furthermore, the density of the wadding 26 may be altered to affect the accuracy of the projectile 24. For instance, as one of ordinary skill in the art would appreciate, the more the wadding 26 is compacted, the greater the accuracy of the projectile 24.
The encasing 30 encloses the RF tagging system 10 and wadding 26 and secures it in the projectile 24. The encasing 30 may not be required if the RF tagging system 10 does not need to be secured together. For example, if the RF tagging system 10 consists of only one device, the encasing 30 may not be needed. However, if the RF tagging system 10 consists of multiple devices such that the RF circuitry 12, power source 16, and antenna 14 are separate devices, the encasing 30 may be required to secure the devices together for operation.
The projectile 24 may include a cover 32 that may be placed about the encasing 30 to form the tip of the projectile. The cover 32 may be any material that is frangible upon impact. In an exemplary embodiment, the cover 32 is made of plastic. The cover 32 is dimensioned to fit sufficiently in the barrel of the delivery device. For example, if the delivery device is a 0.45 caliber gun, the cover 32 is dimensioned such that the projectile is a 0.45 caliber projectile. One of ordinary skill in the art will appreciate that any caliber projectile is contemplated herein. The cover 32 also may be aerodynamically designed to ensure that the projectile 24 maintains its orientation during flight.
The projectile 24 may be placed into a shell for firing. A standard shell for the 0.45 caliber example, may be a cylindrically shaped brass shell. One of ordinary skill in the art will appreciate that any shell is contemplated herein. Propellant 28 may be inserted behind the encasing 30 to propel the projectile 24 upon firing. One of ordinary skill in the art would appreciate that any propellant such as gun powder may be used to fire the projectile 24. Below the propellant may be a secondary wadding 26 used to fill the projectile space in the shell. One of ordinary skill in the art will appreciate that the propellant and secondary wadding 26 may be enclosed by the shell. Upon firing of the projectile 24, the bonding agent 22, the RF tagging system 10 and wadding 26 are expelled from the gun barrel toward the target 20.
Delivery
As illustrated in
Upon breaking of the projectile, the bonding agent 22 becomes exposed to the target 20. The bonding agent 22 adheres to the target 20 thereby attaching the RF tagging system 10 to the target 20. In an alternative embodiment, the RF tagging system 10 may be manually affixed to the target 20 by human placement, robotic placement, or any other manner of placement. In another exemplary embodiment, the RF tagging system 10 may be placed by a micro-aircraft. For example, the micro-aircraft carrying the RF tagging system may be flown into a hostile area and shoot the RF tagging system at the target 20.
The RF tagging system 10 may be powered on upon impact through an inertial switch. As illustrated in
The duration of the RF tagging system 10 on the target 20 may be extended through a reflective circuit that can be activated and interrogated at the tactical level by a radar gun or other energy transmitting devices. In an exemplary embodiment, a standard law enforcement radar gun may be used to activate the reflective circuit. In another embodiment, a radar from a military airborne C4ISR or attack platform may be used to activate the reflective circuit. One of ordinary skill in the art will appreciate that the invention is not limited to radar guns and may also include devices such as Global Hawk or reconnaissance satellites.
Location
After the target has been tagged with the RF tagging system 10, the RF tag needs to be located by tactical C42ISR or attack platforms.
As illustrated in
In one exemplary embodiment, GPS receivers are integrated into the RF tagging system 10 to receive the coordinates from the GPS satellite 36 and determine its location. In an exemplary embodiment, miniature UPS receivers measuring 4 millimeters by 4 millimeters are commercially available and can be integrated with the RF circuitry 12 to provide precise real-time geospatial information to both C4ISR and attack platforms.
In another exemplary embodiment, cellular phone technology may be used to locate its position by triangulating between at least three cellular phone towers 38. The RF tagging system 10 can transmit to the cellular phone towers 38 based on the RF tagging system's 10 relative location to each tower. Standard triangulation algorithms may be used to locate a global position of the RF tagging system 10 based on the distance between the RF tagging system's position relative to the towers 38. However, tag location may be determined through the use of only two or possibly one cellular tower 38 to locate the tag.
The RF tagging system may be used to track the target for better battlefield management. The RF tagging system also may be used to guide a munition during the flight and terminal phase of an attack. The target 20 location information may be transmitted to the munition and uploaded to the guidance and control system. Based on the real-time target location, the guidance and control system can accurately guide the munition to the target 20 for impact. If the target moves, the RF tagging system would transmit realtime positional data to the munition for increased accuracy during the terminal phase of the strike.
In an exemplary embodiment, the RF tagging system may be identified by a certain alpha numeric code and this code would be associated with the particular target. In the event that pre-standing orders exist for immediate termination of a target-type, the code may be immediately uploaded to an overhead asset which would then begin tracking the target and no further ground resources would be required to continue to track the target. The order to attack the selected target (along with the encoded alpha-numeric sequence of the tag) would be passed to the strike team which would then proceed immediately to the target location based upon the data being broadcast from the tag. The tag would then be ordered by the strike leader to begin immediate continuous broadcasting and a less expensive standoff GPS guided weapon would be selected for target termination. Additionally, if a strike asset was not available at the time, the target could be selected for destruction at anytime in the future provided the tag has sufficient power to broadcast (generally within 1 year). Pre-conflict tagging of targets also allows for rapid destruction of mobile targets within the first few hours of a conflict. In addition to decreased risk to valuable aircraft and aircrew, other resources are used more economically (i.e. jet fuel) due to quick mission turn around time and decreased need for air-to-air refueling.
It should further be appreciated that the RF tagging system is not limited to military applications. The RF tagging system 10 may be used in nonmilitary applications as such as police force tagging. For example, a policeman equipped with the RF tagging system 10 may shoot the RF tag using a 0.45 caliber weapon to tag a fleeing target. This is not limited to police but can be used in any application.
The foregoing embodiments and figures are presented by way of example only; the scope of the present invention is to be limited only by the following claims and the equivalents thereof.
The present application claims priority to provisional application Ser. No. 60/477,467 entitled Systems and Methods for Tagging, Tracking, Targeting, and Termination of Mobile Targets, filed on Apr. 13, 2006.
The U.S. Government has a paid-up license in this invention and the right in limited circumstances to require the patent owner to license others on reasonable terms as provided for by the terms of Contract No. FO8630-03-M-0162 awarded by the U.S. Department of Defense.