Class / Patent application number | Description | Number of patent applications / Date published |
235404000 |
Aiming
| 77 |
235411000 |
With target tracking means
| 13 |
235414000 |
Range finder
| 7 |
235417000 |
Ballistic factor determination | 3 |
20120312876 | Determination of weapons fratricide probability - A computer-implemented method is provided for determining fratricide probability of projectile collision from a projectile launcher on a platform and an interception hazard that can be ejected or launched from a deployment position. The platform can represent a combat vessel, with the projectile launcher being a gun, the interception hazard being a missile, and the deployment position being a vertical launch cell. The projectile launcher operates within an angular area called the firing zone of the platform. The method includes determining the firing zone, calculating an angular firing area, quantifying a frontal area of the interception hazard, translating the resulting frontal area across a flight trajectory, sweeping the projectile launcher to produce a slew angle, combining the slew and trajectory, and dividing the combined interception area by the firing area. The firing and interception areas are calculated using spherical projection. | 12-13-2012 |
20140158763 | Optical Device Including an Adaptive Life-Cycle Ballistics System for Firearms - A method includes determining a shot count within an optical device coupled to a firearm. The shot count corresponds to a number of shots taken using the firearm. The method further includes determining a muzzle velocity parameter from a life-cycle profile of the firearm based on the shot count as an input into a ballistics solution. | 06-12-2014 |
20140231515 | SYSTEM AND METHOD FOR BALLISTIC SOLUTIONS - Disclosed embodiments, as well as features and aspects thereof, are directed towards providing a system, device and method for calculating comprehensive ballistic solutions, or portions thereof, via a varying magnification optical range determining and ballistic trajectory calculating apparatus referred to as a ballistic solutions device. Advantageously, embodiments of a ballistic solutions device may drastically reduce marksman error in milling targets by employing a measurement component configured to measure angular movement of a projectile launching device, such as a rifle, thus delivering consistently accurate distance to target estimations. Additionally, embodiments of a ballistic solutions device may also comprise features and aspects that enable a user to leverage available real-time field data such that error associated with the measurement of those variables is minimized prior to calculating and rendering a comprehensive ballistic solution derived from stored DOPE. | 08-21-2014 |
Entries |
Document | Title | Date |
20090308923 | CLOSE-AIR-SUPPORT ASSISTANT - A system includes a signal interface configured to receive first data from at least one onboard system of at least one aircraft, a display, and a processing device. The processing device is configured to render to the display a graphical representation of a target location, determine from the first data and render to the display a graphical illustration of a position of the at least one aircraft, and determine, from information describing munitions carried by the at least one aircraft, and render to the display a graphical illustration of a blast radius associated with munitions deliverable by the at least one aircraft to the target location. | 12-17-2009 |
20100155472 | ENERGY HARVESTING POWER SOURCES FOR ACCIDENTAL DROP DETECTION AND DIFFERENTIATION FROM FIRING - A method is provided for differentiating a non-firing event of a munition from a firing event. The method including: providing the munition with a power supply having a piezoelectric material for generating power from a vibration induced by the munition; monitoring an output from the power supply; calculating an impact pulse from the output; and determining whether the munition is to be fired based on the calculation. | 06-24-2010 |
20100155473 | ENERGY HARVESTING POWER SOURCES FOR VALIDATING FIRING; DETERMINING THE BEGINNING OF THE FREE FLIGHT AND VALIDATING BOOSTER FIRING AND DURATION - A method is provided for validating a firing of a munition and duration of firing of the munition. The method including: providing the munition with a power supply having a piezoelectric material for generating power from a vibration induced by the munition; monitoring an output from the power supply; calculating an impact pulse from the output; and determining one or more of whether the munition has been fired and the duration of firing based on the calculation. | 06-24-2010 |
20100237147 | METHOD AND DEVICE FOR CONTROLLING THE CADENCE OF AN AUTOMATIC WEAPON - The aim of the invention is to devise an inexpensive method and device that allows predefined target tolerances of an automatic weapon ( | 09-23-2010 |
20100264216 | METHODS AND APPARATUS FOR PATH PLANNING FOR GUIDED MUNITIONS - Methods and apparatus for providing path planning for a guided munition. In one embodiment, a boundary value problem solver is used to guide the munition from one configuration to another configuration at a different altitude using a waypoint-based search tree where a number of leaves grows linearly with the depth of the tree. | 10-21-2010 |
20100264217 | System and Method for Implementing Non-Lethal Chemical Warfare Against Rampage Shooters - A system and method for implementing non-lethal chemical warfare against rampage shooters. A sound detection module detects a sound of a gunshot from at least one of a collection of sensors within a building. A sound location module determines a location of the gunshot by analyzing the sound. At least one emitter releases non-lethal chemical countermeasures from at least one at the location of the gunshot. | 10-21-2010 |
20110049237 | ARCHITECTURE FOR A LAUNCH CONTROLLER - A scalable and distributable software architecture for use in conjunction with various different weapons control system and launch systems is disclosed. The architecture discards the proprietary and non-open protocols and services that characterize in favor of open source adaptive and middleware components. In the illustrative embodiment of the invention, the inventive architecture is implemented as a Launch Control Module that separates different layers of responsibility within a launch controller (e.g., LCU) and exposes its variation points. | 03-03-2011 |
20110089237 | SHARED DRIVE LAUNCHER/WEAPON INTERFACE - A weapon launch system includes at least a command and control system, a launcher system and at least one weapon system. The command and control system generates command signals received by the launcher system. The launcher system comprises a launcher operating system that maintains a mapping server connected to a hard drive and a network layer. The mapping server partitions the hard drive into any number of virtual drives accessible by the network layer and each virtual drive maintains operational data for a specific weapon system. The weapon system is coupled to the launcher system and comprises a weapon and a weapon operating system that maintains a mapping client which mounts a designated virtual drive and obtains operational data therefrom and transfers the operational data to the weapon. | 04-21-2011 |
20110309143 | AEROSPACE-GROUND INTEGRATION TESTBED - An aerospace-ground integration testbed may include a truth data scheme, a common sensor adaptor, a common sensor framework, a visualization scheme and a communications scheme. The truth data scheme may generate truth data configured to provide data of at least one of threats, terrain, targets and offensive and defensive systems. The common sensor adaptor may provide sensed data generated from at least the truth data. The common sensor framework may provide modeled sensed data generated from at least the truth data utilizing sensor models. The visualization scheme may generate visual data to be displayed from the sensed data and the modeled sensed data. The communications scheme may provide communication and testbed messaging infrastructure between the truth data scheme, the common sensor adaptor, the common sensor framework, and the visualization scheme. | 12-22-2011 |
20120067951 | Management and Weapon Operation System for Support to Military Management Processes - A management and weapon operation system for support to military management processes, which has interfaces to at least one sensor and at least one effector. The system can be controlled via a graphic control interface 2 that can be displayed on at least one display device for mutual communication between a user and the system. For simple configuration of the system and for reuse of individual applications, the graphic control interface 2 is broken down into individual fragments 8. These are integrated in a desktop manager 4, which carries out the process control for the management and weapon operation system. The fragments 8 have a standard desktop interface 10 for integration. The fragments 8 furthermore have a user interface 12 for communication via an intermediate application 22 with the sensors and/or effectors. The invention also relates to a method for configuration of a management and weapon operation system. | 03-22-2012 |
20120211562 | METHODS AND APPARATUS FOR INTERCEPTING A PROJECTILE - Methods and apparatus for firing a projectile in response to a threat according to various aspects of the present invention operate in conjunction with a computer coupled to a launch system for the projectile. The computer may be configured to select the projectile from multiple available projectiles and calculate a fire control solution according to a characteristic of the selected projectile. Calculating the fire control solution may comprise deriving the fire control solution from a look-up table according to a predicted intercept point. The computer may initiate a launch of the selected projectile and provide the fire control solution to the selected projectile. | 08-23-2012 |
20120228379 | SYSTEM INTEGRATION - Systems and methods of integrating weapons systems with the aircraft systems of an aircraft carrying the weapon so as to generate on the aircraft in flight a display indicative of the weapon successfully engaging a target are disclosed. The system can include a ground station for generating a database describing the weapon performance envelope, a generator for creating coefficients characteristic of that performance envelope using a generic algorithm and an uploader for uploading the coefficients to the aircraft, and a reconstructor on the aircraft containing the same generic algorithm and adapted to select the coefficients for the algorithm according to the aircraft and target conditions in order to generate the feasibility display, wherein the algorithm is generic to both air to ground and air to air weapons. | 09-13-2012 |
20120286041 | APPARATUS FOR SYNTHETIC WEAPON STABILIZATION AND FIRING - In methods and apparatuses, a weapon includes a trigger module for sensing trigger input from a shooter and generating a trigger signal, and a firing module for controlling firing of a projectile responsive to a fire control signal. The weapon also includes an image sensor configured for mounting on the weapon and sensing a series of images over a time period of interest while the trigger signal is in a motion-estimation state. A controller is configured for determining when to fire the weapon by receiving the images from the image sensor and generating a motion-estimation history over the time period of interest responsive to changes in the images. The controller is also configured for determining a centroid of the motion-estimation history and asserting the fire control signal when the trigger signal is in a fire-enable state and a current image is within an offset threshold from the centroid. | 11-15-2012 |
20120298748 | SYSTEM, DEVICE AND METHOD OF PROTECTING AIRCRAFTS AGAINST INCOMING MISSILES AND THREATS - The present invention includes a system for protecting an aircraft against one or more incoming threats. The system includes one or more electro-optic sensors to scan an area around the aircraft for one or more possible incoming threats, and to generate an indication signal once an incoming threat is detected; an integrated unit combining a Missile Approach Confirmation Sensor (MACS) with Directed Infra-Red Counter Measure (DIRCM), to verify the incoming threat and to activate a countermeasure against the verified incoming threat; and a processor to receive data from said one or more electro-optic sensors and the integrated MACS-DIRCM unit, and to select a countermeasure technique for deployment against the incoming threat. | 11-29-2012 |
20130105579 | SINGLE CLICK FIRE CONTROL AND VISUALIZATION FOR SMALL UNIT OPERATIONS | 05-02-2013 |
20130126612 | RATIO-METRIC HORIZON SENSING USING AN ARRAY OF THERMOPILES - An example method includes receiving output voltage data from an array of at least four thermopiles placed around the circumference of a projectile such that for any rotation of the projectile during flight thereof, at least a pair of the thermopile having upwardly-facing fields of view referenced to the earth-fixed coordinate system. The method includes determining the pair of upwardly-facing thermopiles based on the output voltage data from the array, with the respective pair of thermopiles including a thermopile p and next adjacent thermopile p+1. The method includes determining a ratio of the output voltage data from thermopiles p and p+1, and applying the ratio to a function associating, for any pair of thermopiles n and n+1, a ratio of output voltage data from thermopiles n and n+1, and a roll angle θ | 05-23-2013 |
20140209678 | SYSTEM, DEVICE, AND METHOD OF PROTECTING AIRCRAFTS AGAINST INCOMING THREATS - System, device and method for protecting aircrafts against incoming threats. The system includes: (a) a dual-band Radio Frequency (RF) track-and-confirm module comprising: a dual-band RF receiver to receive high-band RF signals and low-band RF signals; a threat confirmation module to confirm a possible incoming threat based on processing of RF signals received at the dual-band RF receiver; a threat parameters calculator to calculate a fine angular position and a precise angular position of a confirmed incoming threat, based on processing of RF signals received at low-band RF for fine angular position and at high-band RF for precise angular position; (b) a countermeasure directed Laser module to activate a directed Laser countermeasure towards said precise angular position of said confirmed incoming threat. | 07-31-2014 |