Matches 1 - 50 out of 74 1 2 >


Match Document Document Title
US20120181376 MUNITION AND GUIDANCE NAVIGATION AND CONTROL UNIT  
A guidance and control unit assembly for use with a munitions projectile includes a guidance and control unit being roll isolated with respect to the munitions projectile such that roll of the...
US20120048993 AERODYNAMIC FLIGHT TERMINATION SYSTEM AND METHOD  
A missile has a flight termination system that includes deployable lift surfaces that deploy forward of a center of gravity of the missile. When deployed, the lift surfaces cause the missile to...
US20100314487 PREDICTING AND CORRECTING TRAJECTORIES  
Technology for predicting and correcting a trajectory is described. The technology can create a model to predict a position of the reusable launch vehicle at a time in the future; observe a wind...
US20150041582 TACTIcal MISSILE AND BALANCE WEIGHT FOR SAID MISSILE  
According to the invention, the balance weights of the missile are made from pellets whereof the particle size is at most equal to 1 mm which is enclosed in a closed package.
US20140203134 SYSTEMS AND METHODS FOR RETAINING AND DEPLOYING CANARDS  
Disclosed are systems and methods for retaining and deploying a plurality of canards and canard covers on a projectile. The projectile includes a projectile housing defining an interior chamber...
US20120153070 AUTOMATIC RE-INITIALIZATION OF RESONANT SENSORS IN ROCKET AND MISSILE GUIDANCE SYSTEMS  
An apparatus and method improves the fault tolerance of a rocket or missile guidance system which includes a resonant sensor. When improper initialization is detected, the resonant sensor is...
US20120024136 METHOD FOR LAUNCHING A MISSILE  
An air-based vertical launch system is described by means of which ballistic missile defense can be achieved effectively from a large aircraft. A method for ensuring safe missile egress is...
US20120209455 Autopilot with Adaptive Rate/Acceleration Based Damping  
A control system includes a rate-damping loop that uses a motion parameter error (heading pitch, heading yaw, attitude pitch, attitude yaw, and attitude roll) to non-linearly scale a rate-feedback...
US20120181375 Modular Guided Projectile  
A modular artillery projectile and method of engaging a target. A modular artillery projectile may include a payload module, a guidance module coupled to the payload module and a rear module...
US20100270418 MISSILE TRAINING SYSTEM  
The present invention is directed to missile training systems, especially to those relating to the provision of a mechanism that allows missiles and similar devices to be fired at a target in a...
US20060169832 Rocket propelled barrier defense system  
A system providing a physical-barrier defense against rocket-propelled grenades (RPGs). The system is suitable for use on aircraft, ground vehicles, and ships.
US20120055323 Systems and Methods for Launching Munitions  
Systems and methods for launching munitions are provided. In some embodiments, a launcher configured to retain a munition during transport by a vehicle may comprise a first housing, circuitry, and...
US20060091255 Antiballistic missile defense  
Multiwavelength satellites, illuminating satellites and multiwavelength antiballistic missiles working in cooperation may overcome enemy missile countermeasures (i.e. decoys, aerosols, changing...
US20110108660 SMALL SMART WEAPON AND WEAPON SYSTEM EMPLOYING THE SAME  
A weapon and weapon system, and methods of manufacturing and operating the same. In one embodiment, the weapon includes a warhead having destructive elements. The weapon also includes a folding...
US20110068220 Unknown  
The invention concerns the field of devices for improving the piloting of projectiles More specifically, the object of the invention is a piloting device for a missile or a projectile, for...
US20110120337 ARTILLERY PROJECTILE WITH SEPERATELY CONTROLLED BOOSTER ACTUATION AND FRAGMENT DISPERSION  
An artillery projectile for firing from an artillery gun, mortar or artillery rocket launcher. The artillery projectile includes a body, a payload with a number of inert fragments located within...
US20060138276 Dome  
The present invention relates to process for producing a transparent missile dome having a spanning angle larger than 180°, comprising the step of: (a) growing from single crystals of a ceramic...
US20090114761 RAM neutralization system and method  
An article for neutralizing an enemy weapon comprising an interceptor and a deployable net attached to the interceptor, said deployable net remaining attached to the interceptor upon deployment is...
US20120109538 SYSTEM AND METHOD FOR DETERMINING, UPDATING, AND CORRECTING KINEMATIC STATE INFORMATION OF A TARGET  
A process to preserve the kinematic state of a target includes determining an initial kinematic state estimate of the target using an observer with an active sensor. The initial kinematic state...
US20090230234 GUIDED MISSILE  
A guided missile has a sensor unit, a propulsion unit, and a payload unit. A missile casing forms the outer contour, extends along a longitudinal direction, and accommodates the sensor unit, the...
US20090090809 METHOD OF INCREASING THE RANGE OF A SUBCALIBRE SHELL AND SUBCALIBRE SHELLS WITH LONG RANGE  
The invention relates to a method for increasing the range of shells (1, 8, 13) charged with an explosive substance and other types of shell, which function as carriers of the one or other type of...
US20080035785 Unmanned missile and method for determining the position of an unmanned missile which may be uncoupled from an aircraft  
An unmanned missile which may be uncoupled from a preferably propelled aircraft has a navigation and control device which has a receiver for position determination signals. The receiver is...
US20070295856 Flying object for transonic or supersonic velocities  
The invention relates to a flying object being moved with transonic or supersonic velocities. Known flying objects comprise so called “aerospikes” used for reducing the wave drag and improving the...
US20090288389 INTEGRAL THRUST VECTOR AND ROLL CONTROL SYSTEM  
An apparatus for vectoring the thrust of a motor that produces thrust along a longitudinal axis by expelling combustion gases through a nozzle may include a plurality of linearly-positionable...
US20090294574 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...
US20130037651 NUTATING SPLIT PETAL FLARE FOR PROJECTILE FLUID DYNAMIC CONTROL  
A system and methods for fluid dynamically controlling a projectile are disclosed. At least one actuator coupled to at least one common actuation structure is actuated to provide an actuation...
US20140027563 GROUND-PROJECTILE GUIDANCE SYSTEM  
A guidance unit system is configured to be used for a ground-launched projectile. The system includes a housing configured to be attached to a ground-launched projectile. The housing is coupled to...
US20090145996 Method and Device for Varying a Flight Path of a Projectile by Intentional Tumbling of the Projectile  
A method for varying the flight path of a missile, in particular of a spin-stabilized projectile, which has an outer wall and which is provided with at least one impulse device. The impulse device...
US20050056723 FIXED CANARD 2-D GUIDANCE OF ARTILLERY PROJECTILES  
Applicants have invented a guidance system for guiding a projectile, the projectile having a body portion capable of being spun in a first direction and a nose portion connected to the body...
US20080203216 Multi-Environment Engine  
The inventive multi-environment engine (1) comprises a body (2), wings (4, 5) and a propulsion system (8), wherein at least one wing is foldable between a first levitation flying position, a...
US20130015288 SPRING CLIP RETENTION SYSTEMS SUITABLE FOR USAGE WITHIN VEHICLES AND GUIDED MUNITIONS  
Embodiments of a spring clip retention system are provided for securing a generally cylindrical component, as are embodiments of a guided munition including a spring clip retention system. In one...
US20120012690 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...
US20080035784 AIRCRAFT WAKE VORTEX PREDICTOR AND VISUALIZER  
A method to predict a location, intensity and movement of wake vortexes may include collecting one or more ground-based measurements related to predicting the location, intensity and movement of...
US20080006735 Guided missile with distributed guidance mechanism  
A weapons system including a guided missile and a guidance mechanism, separate from the guided missile. The guided missile includes a seeker for producing signals indicative of a position of a...
US20060289695 Device with remote motor for controlling an aerodynamic control surface of a missile  
An aircraft comprising at least one aerodynamic control surface (26) controlled using a remote motor (4), through a transmission comprising a linear device (7) rigid in torsion but flexible in...
US20100000438 Methods and apparatus for selectable velocity projectile system  
Methods and apparatus according to various aspects of the present invention comprise a propelling system for propelling projectiles with variable velocity. In one embodiment, a cartridge comprises...
US20070042315 Visual feedback implements for electromagnetic energy output devices  
An electromagnetic energy output device in the form of laser handpiece and a trunk assembly is disclosed. The electromagnetic energy output device includes a digital camera and electromagnetic...
US20070007382 Solver for a restrained deformable system with released degrees of freedom  
A process of using finite element analysis for determining the behaviour of a system, submitted to predetermined load and displacement boundary conditions with a degree of freedom relative to a...
US20090308970 POD launched unmanned air vehicle  
A method for attacking dispersed targets from a single aircraft standing off at a significant distance from the target area, wherein pods of individually targeted UAVs are carried in lieu of a...
US20120216700 TIPPED PROJECTILES  
A projectile is provided with a projectile tip having enhanced aerodynamic properties to improve accuracy of the projectile. The tip has a body having a base or lower end, an upper end and a...
US20060022083 Marking of objects for speed and spin measurements  
A system for measuring the flight of a projectile, comprising: a projectile comprising an exterior surface and a set of orientation identifiers distributed over the exterior surface, such that,...
US20150001335 BRAKE PANEL FOR A DETONATOR OR A PROJECTILE  
The invention relates to a brake panel (3, 3′) for a projectile (1), in which those surfaces (A) of the brake panel (3, 3′) which are facing in the direction of travel of the projectile are wholly...
US20080001022 Precision targeting  
The disclosed system, device and method for targeting and measurement of stationary target locations in addition to prediction of moving target positions for given weapon intercept times generally...
US20070241227 Ballistic Guidance Control for Munitions  
A method and system for guiding and controlling an ordinance body having a trajectory and a bore sight angle including making corrections to the trajectory based on bore sight angle vs. time...
US20110101154 Steerable Projectile  
A steerable projectile (30) comprises a body portion (32) and a nose portion (34). The nose portion and body portion are substantially coaxially arranged and rotatable relative to one another...
US20090272839 SYSTEM AND METHOD FOR CONTROLLING HIGH SPIN RATE PROJECTILES  
A method is disclosed for controlling a flight trajectory of a spinning projectile. In one aspect the method may involve supporting a nose of the projectile in a manner permitting the nose to be...
US20110204177 PROJECTILE DIVERTER RELEASE AND METHOD OF DIVERTING A PROJECTILE  
A diverter for changing the trajectory of a projectile includes a release mechanism that extends along a longitudinal axis between first and second ends. A mass is coupled to the first end, and...
US20120181372 ACTUATION ASSEMBLY  
An actuation assembly is provided. The actuation assembly includes a casing, a plurality of linear actuators coupled to the casing, each of the linear actuators having first and second components...
US20070158493 Fire control system using a lidar (laser identification, detecting and ranging) unit  
A fire control system that includes an array of photodiode elements. For each element of the photodiode array, there is a specific optical path in the atmosphere leading from the laser to a target...
US20070295855 TARGET MANEUVER DETECTION  
The present invention includes, in its various aspects and embodiments, a method and apparatus for determining whether a moving target is maneuvering. The method comprises determining an expected...

Matches 1 - 50 out of 74 1 2 >