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8178825 Guided delivery of small munitions from an unmanned aerial vehicle  
The present invention provides apparatus and methods for accurate guidance of small munitions to a target. The guidance for the small munition is mainly provided by a device external to the small...
8173945 Apparatus and method for guidance of a projectile  
There is disclosed an apparatus and a method for guidance of a projectile. The method for guidance of a projectile, includes emission from the launching position of the projectile of beams pointing...
8173946 Method of intercepting incoming projectile  
A method of defeating an incoming missile, such as a rocket propelled grenade, includes soft launching an interceptor missile, and then using pitch over motors of the interceptor missile to alter...
8164037 Co-boresighted dual-mode SAL/IR seeker including a SAL spreader  
In a co-boresighted SAL/IR seeker, the optical system and particularly the secondary lens and position of the SAL detector are configured to produce a well-corrected spot of laser energy at the SAL...
8165731 System for aerial delivery of fire retardant  
A system for launching, controlling and delivering in a preselected target pattern a plurality of low-cost, guided fire-retardant-containing vehicles, i.e., “smart water bombs” equipped with con...
8153943 Tornado detection network  
A tornado disarming network includes a command center, tornado detection systems, and tornado busting missile launch sites in communications with the command center. Tornado busting missiles are at...
8134103 Burnout time estimation and early thrust termination determination for a boosting target  
A system senses the presence of a boosting missile or target and processes the information by comparison of the data with a plurality of predetermined templates of nominal missile characteristics,...
8130137 Template updated boost algorithm  
A method and a system for sensing a boosting target missile, estimate position and velocity and boost acceleration parameters of the target missile, and control an interceptor missile to the target...
8124921 Methods and apparatus for guidance of ordnance delivery device  
A guidance system according to various aspects of the present invention operates in conjunction with a suite of different ordnance delivery devices. In one embodiment, the guidance system comprises...
8119958 Method and device for matrix of explosive cells  
A matrix of explosive cells can include plural explosive cells formed in an array in a common substrate. Each cell can be formed as a recess filled with explosive material. An ignition device has...
8119959 Flight control of missiles  
A missile in which a nose portion is rotatably mounted on a main body portion of the missile and is subjected to thrust to bring it to a demanded roll attitude and to apply to it a demanded lateral...
8119957 Submunition and method of destroying a target in a target area by the submunition  
A submunition is formulated for destroying a target in a target area. Accommodated in a casing are a signal processing unit connected to a radar antenna and/or an infrared sensor and/or another...
8119956 Multi-stage hyper-velocity kinetic energy missile  
A multi-stage hyper-velocity kinetic energy missile (HVKEM) uses a ‘missile in a missile’ architecture in which the HVKEM includes a 1st stage flight missile and a 2nd stage kill missile that inc...
8115148 Method for targeting a preferred object within a group of decoys  
Current targeting approaches involve guiding to a spatially derived guidepoint of a group of objects likely to be the preferred object. This method may not allow the intercepting missile to contain...
8115149 Gun launched hybrid projectile  
A Hybrid Projectile is provided for delivering an explosive payload to a target wherein the Hybrid Projectile may be steered in flight using relatively inexpensive means. The Hybrid Projectile is...
8110784 Projectile having one or more windows for transmitting power and/or data into/from the projectile interior  
A projectile including: a casing; first and second windows provided on the casing for at least one of transmitting a first optical signal into an interior of the casing and transmitting a second...
8106340 Generalized midcourse missile guidance  
A method for guiding a multistage interceptor missile toward a target missile that may transition from a boost mode to a ballistic mode during the engagement. The method comprises the steps of...
8104719 Digital interface unit (DIU) and method for controlling stages of a multi-stage missle  
A multi-stage missile with plural stages adapted to be physically coupled to and decoupled from adjacent stages and a processor disposed on a single stage for controlling each stage thereof. In the...
8100359 Intercept system for falling bombs  
An intercept system for destroying a falling bomb includes a packable structure including a compressed expandable net of break resistant cords, a radio altimeter and a deployment mechanism for...
8098191 Electronic curtain for vehicle protection  
An apparatus and method for protecting against incoming projectiles comprising transmitting two radar waveforms, the first waveform comprising a pulsed continuous wave waveform, and the second...
8093539 Integrated reference source and target designator system for high-precision guidance of guided munitions  
A method for guidance of a moving object towards a target. The method including: providing reference signals from RF reference sources to illuminate RF sensors on the moving object; positioning the...
8089033 POD launched unmanned air vehicle  
A method and apparatus for attacking a plurality of dispersed targets are herein presented. In particular, the method and apparatus herein presented allow the user to upload target data onto a pod...
8084724 Enhanced multiple kill vehicle (MKV) interceptor for intercepting exo and endo-atmospheric targets  
By sharing tasks between the CV and the KVs, the MKV interceptor provides a cost-effective missile defense system capable of intercepting and killing multiple targets. The placement of the...
8085188 Method and apparatus for determining a deviation between an actual direction of a launched projectile and a predetermined direction  
A method of determining a deviation of a path of a projectile from a predetermined path. The method uses an image of a target area in which the desired path or direction is pointed out....
8084726 Control system for an exoatmospheric kill vehicle  
A control system for a maneuverable kill vehicle is provided. The control system includes a pressurized fluid source configured to provide a pressurized fluid, a valve in fluid communication with...
8084725 Methods and apparatus for fast action impulse thruster  
Methods and apparatus for a fast action impulse thruster according to various aspects of the present invention may comprise a projectile comprising an impulse thruster system. The impulse thruster...
8080771 Steering system and method for a guided flying apparatus  
A steering system for use in a traveling guided flying apparatus (10) and method for driving the steering system are provided. The system includes an outer housing (111), an inner housing (113) and...
8080772 Modular, harnessless electromechanical actuation system assembly  
A modular electromechanical actuation system assembly is provided that includes an electronic control unit housing having a plurality of motor receptacles and a plurality of battery receptacles...
8076622 Low profile, conformal global positioning system array for artillery  
The present invention is a device which includes an antenna and circuitry. The antenna may receive a circularly-polarized signal as first and second linearly-polarized signals. The circuitry is...
8076621 Integrated reference source and target designator system for high-precision guidance of guided munitions  
A method for guiding a moving object to a target. The method comprising: transmitting a signal from one or more illuminating sources defined in a reference coordinate system; receiving the signal...
8076623 Projectile control device  
A spin-stabilized projectile is steered by taking air from an air intake at the front of the projectile, and expelling the air along an outer surface of the projectile to alter its trajectory...
8071926 Stability multiplexed autopilot  
Rolling airframe projectile guidance and stability systems are disclosed. Flight control surfaces, such as canards and/or tail fins are attached to a projectile airframe that is designed to roll...
8070854 Passive desiccant system  
In a method for removing moisture from an optical system at high altitude, the improvement comprises using the difference in flow resistance between the desiccant path and the optical cavity path...
8071927 Methods and systems for wave guides  
Methods and systems for a wave guide according to various aspects of the present invention may be implemented in conjunction with a radiation collection device comprising a light pipe, a first...
8063346 Virtual image projector  
Systems and methods are provided for projecting a virtual image of an object. A projector mounted on the object for projecting a light beam. A photographic plate is provided that includes an...
8063347 Sensor independent engagement decision processing  
A method for engaging a target uses sensors to generate target track(s). The tracks are projected forward in time and associated with a track quality measure. The maximum seeker look angle and...
8058595 Collapsible shape memory alloy (SMA) nose cones for air vehicles, method of manufacture and use  
A nose cone formed from a shape memory alloy (SMA) having a recoverable strain of at least 2% collapses about the dome for storage, deploys at launch to protect the sensor dome and reduce drag...
8058596 Method of controlling missile flight using attitude control thrusters  
A method of controlling flight of a missile includes using gyroscopes, such as pitch rate gyroscopes, to sense when a factor based on the angular rate of change of the missile exceeds a threshold...
8049149 Methods and apparatus for air brake retention and deployment  
Methods and apparatus for an air brake system for a projectile according to various aspects of the present invention comprises a pivot and a protrusion mounted on the pivot. The protrusion is...
8049148 Missile airframe and structure comprising piezoelectric fibers and method for active structural response control  
Embodiments of a missile, an airframe and a structure comprising piezoelectric fibers and a method for active structural response control are generally described herein. In some embodiments, a...
8035547 System and method of assisted aerial navigation  
A system and method of providing aerial navigation. Techniques are described for receiving global positioning system data, receiving local positioning system data such as instrument landing system...
8022343 Aiming system with integrated deviation meter  
According to the invention, the system comprises an infrared detector (7) for alternately generating images (5′) of sources of light (5) in the near infrared emitted by a missile flying towards a t...
8001901 Signal transmission surveillance system  
A system and method of detecting, processing, and selectively responding to radio frequency transmissions detected by at least one projectile deployed above a geographic area.
7999726 Antenna pointing bias estimation using radar imaging  
A system for estimating an antenna boresight direction. The novel system includes a first circuit for receiving a Doppler measurement and a line-of-sight direction measurement corresponding with...
7999212 Precision guided munitions  
A guidance system for actively guiding a projectile, such as a bullet after it has been fired from a gun. The guidance system includes a radar unit that includes a plurality of receiver arrays. An...
7989744 Methods and apparatus for transferring a fluid  
Methods and apparatus for a missile having an external system operate in conjunction with an airframe and a fluid transfer system. The airframe includes an interior surface defining a substantially...
7989742 Process to control the initiation of an attack module and initiation control device implementing said process  
The invention relates to a process to control the initiation of an attack module, such as a projectile or sub-projectile, such attack module having at least one pre-determined direction of action....
7989743 System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system  
A reliable and inexpensive attitude control system uses a plurality of pitch-over thrusters to perform rapid and precise attitude maneuvers for a flight vehicle. The pitch-over thrusters create...
7982662 Scanning array for obstacle detection and collision avoidance  
This scanning array scans an area around the array for nearby objects, collision obstructions, and terrain topography. The scanning array can scan for sounds emitted by objects in the vicinity of...
7977613 System and method for roll angle indication and measurement in flying objects  
A method for onboard measurement of a deviation in orientation of an object from a desired orientation of the object. The method including: transmitting a polarized RF signal from a reference...