Tracor, Inc.

Bae Systems Integrated Defense Solutions Inc.

Tracor Aerospace, Inc.

Marconi Aerospace Defense Systems Inc.

Other

Bae Systems Information and Electronic Systems Integration Inc.

Tracor Aerospace Austin, Inc.

Bradley T Sallee

David J Schorr

James K Vinson

Beryl W Cotton

Robert Goan

Joe Gleave

One aspect of the invention relates to a laser ranging system. In this version of the invention, a guided missile is provided with laser that directs laser radiation in the general direction of a target that is subsequently reflected from the target back to the missile. A receiving lens is mounted on the missile that receives the reflected laser radiation. A ferrule containing optical fibers divided into a plurality of pixels that receive the reflected laser radiation from the receiving lens, wherein each pixel in the plurality of pixels is provided a different pointing angle by arranging the fibers within the pixel such that the centroid of the field of view of the fibers is different from the centroids of the field of views of the other fibers in the other pixels. A plurality of optical sensors coupled to the optical fibers, each optical sensor being dedicated to a separate pointing angle and adapted to generate an electrical signal whose amplitude is responsive to the amplitude of the reflected radiation for the pointing angle that the optical sensor is dedicated to.

Fiber optic laser detection and ranging system

Fiber optical laser detection and ranging system

The present invention relates to a system for sweeping a laser beam in a preset pattern, while, at the same time, directing the pattern to any area in a predetermined scanning area. The invention is particularly useful in LADAR applications. In one version of the invention, a series of optical prisms are arranged in concentric tubes so that the prisms have a common optical path. The tubes and, hence, the prisms, may be independently rotated by precision electric motors coupled to gear rings on the tubes.

Optical system for LADAR guidance application

One aspect of the invention relates to a laser ranging system. In one embodiment, the invention includes a laser adapted to transmit a beam of laser radiation to a target area, a plurality of apertures for receiving reflected laser radiation from the target area, each aperture being coupled to a start tank circuit by a start optical fiber, the start optical fibers being substantially the same length for each aperture in the plurality, an oscillator, a receive phase comparator circuit that determines the phase difference between the output signals from the start tank circuit and the oscillator, a transmitter tank circuit that generates and output signal responsive to the transmission of the laser radiation, a transmit phase comparator circuit that determines the phase difference between the output signals from the transmitter tank circuit and the oscillator, a pulse counter circuit that counts the number of pulses generated by the oscillator between transmission of the laser beam and the receipt of the signal from the start tank circuit, and a distance measuring circuit that calculates the distance from laser ranging system to the target based upon the number of pulses counted by the pulse counter, the phase difference determined by the receive phase comparator circuit and the phase difference determined by the transmit phase comparator circuit.

Multi spectral imaging ladar

One aspect of the invention relates to a laser ranging system. In one embodiment, the invention includes: a laser adapted to transmit a beam of laser radiation to a target area; a plurality of apertures for receiving reflected laser radiation from the target area, wherein each aperture is coupled to a start tank circuit by a start optical fiber, and wherein the start optical fibers are substantially the same length for each aperture in the plurality; an oscillator; a receive phase comparator circuit that determines the phase difference between the output signals from the start tank circuit and the oscillator; a transmitter tank circuit that generates an output signal responsive to the transmission of the laser radiation; a transmit phase comparator circuit that determines the phase difference between the output signals from the transmitter tank circuit and the oscillator; a pulse counter circuit that counts the number of pulses generated by the oscillator between transmission of the laser beam and the receipt of the signal from the start tank circuit; and a distance measuring circuit that calculates the distance from laser ranging system to the target based upon the number of pulses counted by the pulse counter, the phase difference determined by the receive phase comparator circuit and the phase difference determined by the transmit phase comparator circuit.

The invention uses a garnish of tufts of filaments or strips attached to camouflage material, particularly camouflage material for use on mobile equipment, vehicles and personnel. The garnish or tuft is formed from a sheet of flexible, low emissivity material that has been cut into filaments or strips adhesively attached along one uncut longitudinal strip edge portion of the sheet. The tuft is formed by rolling the strip edge portion longitudinally around one part of a tuft retaining anchor, to form a rolled, adhesive-bound segment attached to the tuft part. When the rolled strips or filaments are so bound about the tuft retaining anchor part, a tuft is formed therefrom. When all the tuft retaining anchor parts are assembled, the tuft retaining anchor and tuft together constitute the garnish. A plurality of garnishes is attached to a base camouflage material on, e.g., mobile equipment, vehicles and personnel. The garnishes are preferably removably attached, to enable the color and other properties of the tuft to be varied in accordance with the surroundings in which the camouflage is to be effected. The tuft effectively absorbs and then dissipates heat by inducing air currents around the camouflaged object. The heat absorbed and dissipated otherwise would have been absorbed either by the base camouflage material or the device sought to be camouflaged, with a concomitant increase in the infrared signature of that device. This absorption and dissipation of heat is particularly effective when conditions of bright sunshine and calm or still conditions exist, especially in the early morning hours.

Low thermal signature camouflage garnish

This invention relates to the field of metal detectors. More particularly, it relates to an imaging metal detector for imaging the metal on subjects passing through a spatial plane providing the specific location, shape and mass of the metal object. This invention makes use of an array of active sensors to transmit and receive magnetic beams and a computer for generating an image of the metal object based upon the data received from the sensors. Through the use of this invention it is possible to scan several subjects at the same time and generate a two- or three-dimensional image of any metal object on the subject as well as precise location, mass and type of metal contained in the object.

Apparatus and method for detecting and imaging metal

A directional control system for ballistic projectiles, including a projectile capable of being fired from a gun, a tracking device within the projectile capable of sensing and identifying a preferred target direction, a moveable mass located within the projectile, an electromagnetic mass-shifting device within the projectile capable of reversibly moving the mass from a first position to a second position whereby the flight path of the projectile is controlled. The directional control system may be used with a projectile which has no externally protruding bodies. The system includes at least one microprocessor programmed to obtain input from the tracking device and to perform calculations to determine movements of the mass. The moveable mass is positioned to shift the momentum vector perpendicular to the central longitudinal spin axis of the projectile when in motion. The mass shifting device preferably includes an electromagnetic driver, which is aligned such that the mass can be moved reversibly from a first position to a second position. The system preferably includes a tracking device including optical fibers for receiving incoming radiation. The system may include a tracking device which is sensitive to radio frequency radiation, and has at least one antenna sensitive to radio frequency radiation. The tracking device may alternatively have at least one infrared detector sensitive to infrared radiation, and preferably has a pyroelectric detector pair.

Control system for gun and artillery projectiles

A multiple squib assembly is provided for use in a chaff deployment system. A method of manufacture is also provided. The assembly of this invention represents an improvement over prior art squib assemblies, such as the BBU48. In preferred embodiments, the assembly comprises a brass base plate, a pair of squibs, a center contact connected to the squibs, and a zener diode connected between one of the squibs and the baseplate. All of those components are retained within a molded rubber or plastic body, which is shaped to hold the components in the desired relative position and to form sealing elements around each of the squibs. A reliable, integral assembly is thus provided using a minimal number of parts and electrical connections. In alternative embodiments, a larger number of squibs may be incorporated into the assembly, and alternative discrimination elements may be employed.

Multiple squib assembly

A telescoping support pole suitable for supporting tarpaulins or camouflage netting is described. The pole is made up of a plurality of tubes that nest within one another for storage. To deploy the pole, the tubes are extended in a telescoping fashion. Ball locks are provided for maintaining the extended poles in desired longitudinal relationships. The ball locks are activated by spring loaded collars that force balls into circumferential grooves formed in the outside surfaces of the inner telescoping tubes. The collars may be manually operated to release the ball lock mechanism to permit the pole length to be adjusted or to permit the tubes to be nested within one another for storage. Pivoting fixtures suitable for use at the upper end of the support pole are also described.

Extendable support pole

Novel structural members are provided that are flexible prior to being rigidized. The structural members are fabricated as bundles of reinforcing fibers commingled with binder materials, e.g. thermoplastic yarn, and a heat source. Means for compressing the bundle during deployment may also be provided. The structural members are rigidized by activating the heat source to melt the binder material, which flows throughout the bundle to bind the reinforcing fibers together, such that when the binder sets or hardens a rigid, reinforced structural member is provided. In preferred embodiments, these structural members are attached to an inflatable enclosure in a structural framework arrangement to form an inflatable structure. Such an inflatable structure may be rolled or folded into a compact space for storage and transport, such as into outer space. The structure may be deployed at a desired location by inflating the enclosure to stretch the structural member bundles into the desired configuration and actuating the heating elements to activate the binder material. After the binder has set, the structure is rigid and inflation pressure may be removed, leaving a rigidized enclosure or a reinforced structural member.

Rigidizable inflatable structure

A rigid habitat structure is provided that is fabricated in an axially compressed condition so that it occupies less volume before it is expanded upon deployment. In a preferred embodiment, the structure is fabricated with a pleated metal skin forming a bellows-like structure. The structure may further comprise structural hoops and stringers connected to the metal skin. The structure may be transported to its desired location in its compressed condition and then deployed by inflating the structure to axially expand the bellows, whereby the metal skin and stringers are stretched into a straightened condition. Inflation may be continued past the elastic limits of the stringers and skin, thereby stiffening them in their expanded condition and creating a rigid expanded structure. Axially expandable micrometeorite shielding and thermal insulation are also provided that can be installed on the compressed structure and that expand along with the structure during deployment.

Expandable rigid structure

An inflatable truss frame member for use in the frame of a large inflatable device such as a ship or satellite decoy. A first embodiment, developed for use in satellite decoys, comprises three main inflatable tubes separated by shear load carrying interlacing inflatable tubes. The first embodiment may be manufactured by laminating two MYLAR sheets together using a triangular pattern of adhesive print to form a series of inflatable tubes. Excess material is removed from between the tubes and the edges of the MYLAR are bonded together forming a cylinder to complete the inflatable truss frame member. A second embodiment, developed for the heavier shear loading of ship decoys, comprises three main inflatable tubes separated by a shear load carrying web. The second embodiment may be manufactured by bonding an inner and outer tube made of MYLAR along arcuately spaced strips. The bonded MYLAR forms the separating web and unbonded MYLAR forms three inflatable tubes. Alternately, the second embodiment may be manufactured by separately forming three inflatable tubes and then bonding the separating web material to the inflatable tubes. Rigid stays or battens may be added between the three inflatable tubes when the separating web will not be strong enough to support the shear loading.

Inflatable truss frame

A chaff device for exoatmospheric deployment as a countermeasure to radar detection of exoatmospheric objects utilizes a plurality of elongated foil members and a plurality of elongated fiber members, each for providing a dipole. The foil dipole members are disposed in an end-to-end overlapping relationship and wrapped in a coil configuration. The fiber dipole members in a group are disposed adjacent one of the foil dipole members so as to be sandwiched between adjacent layers of coil wrapped foil dipole members.

Fiber under foil chaff coil

A differential drag apparatus is disclosed for detecting air pressure forces on a drag-sensing body. The body is movable in response to a predetermined magnitude of air pressure force. A pressure regulator responds to the movement of the body by releasing uniform pressure to an activation system. The activation system in turn releases a trigger provided the air pressure force acting against the drag-sensing body remains above the predetermined magnitude for a predetermined length of time. The trigger upon release may perform any number of activates such as opening or closing an electrical circuit, initiating a mechanical response, i.e. releasing a parachute, or detonating a small munition charge. The detonation of a charge, for example, may in turn ignite a rocket motor, release an explosive, or any other of related activities. The apparatus is insensitive to short duration forces above or below the predetermined magnitude, and radiation as results from proximate nuclear blast. The trigger and regulator are initially primed by a pyro-train fuse; yet, activated only by differential movement of the drag-sensing body for a predetermined length of time.

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Austin, TX, United States of America

Bradley T Sallee