Abstract: A celestial navigation system (CNS) designed for determining position of a vehicle in GPS denied or degraded environment by imaging celestial objects and measuring vehicle ground speed, attitude, and time.

Abstract: A secured personal communication device (SPCD) with iris imaging and retinal scanning designed to provide sensitive or proprietary information when and where it is needed without the possibility for eavesdropping. Sensitive information is transmitted to the user only if the image of the user's iris matches a pre-recorded template of the user's iris. In preferred embodiments a waist mounted fingerprint reader and a RFID/CAC card reader provides additional assurance that transmission of sensitive information is secure. A proximity sensor and waist-mounted communication-control electronic module can also be provided to assure that there is no display of sensitive information to the wearer unless the retinal scanning and iris imaging components are located with the wearer near the eye to which sensitive information is transmitted.

Abstract: A dual-band (SWIR/visible) optical system operating based on Angles-Only Navigation technology. The SWIR module is optimized for imaging stars. The visible-light sensor is independently optimized for imaging satellites including GPS satellites at night. Preferred embodiment provides continuous high accuracy geo-position solutions day and night (including through the “midnight hole”, when solar-illuminated Low Earth Orbit (LEO) satellites are not available. Applicants have experimentally validated proposed system by imaging LEO satellites during terminator using a 1-inch diameter telescope and GPS satellites at night during midnight hole using a 5-inch telescope.

Abstract: A dual-band (SWIR/visible) optical system operating based on Angles-Only Navigation technology. The SWIR module is optimized for imaging stars. The visible-light sensor is independently optimized for imaging satellites including GPS satellites at night. Preferred embodiment provides continuous high accuracy geo-position solutions day and night (including through the “midnight hole”, when solar-illuminated Low Earth Orbit (LEO) satellites are not available. Applicants have experimentally validated proposed system by imaging LEO satellites during terminator using a 1-inch diameter telescope and GPS satellites at night during midnight hole using a 5-inch telescope.

Abstract: An optical system for providing crosswind aim point correction for a sniper rifles and similar weapons comprising an optical transmitter, an optical receiver, a display device and a processor. The optical transmitter produces a collimated laser beam for illuminating a spot on the target. The optical receiver receives optical signals transmitted by the optical transmitter and scattered back from the target and converts the optical signals into time varying electrical signals. The processor processes the time varying electrical signals to determine a path weighted average crosswind. The processor is equipped with software that permits it to calculate the path-weighted average crosswind utilizing at least three different methods.

Abstract: A head worn display system with at least one retinal display unit having a curved reflector positioned in front of one eye or both eyes of a wearer. The unit includes a first set of three modulated visible-light lasers co-aligned and adapted to provide a foveal laser beam with selectable color and a first scanner unit providing both horizontal and vertical scanning of the laser beam across a small portion of the curved reflector in directions so as to produce a reflection of the color laser beam through the pupil of the eye onto a portion of the retina large enough to encompass the fovea.

Abstract: A celestial compass kit. The kit includes an inclinometer, a camera system with a special telecentric fisheye lens for imaging at least one celestial object and a processor programmed with a celestial catalog providing known positions at specific times of at least one celestial object and algorithms for automatically calculating target direction information based on the inclination of the system as measured by the inclinometer and the known positions of at least one celestial object as provided by the celestial catalog and as imaged by the camera. The telecentric fisheye lens produces an image on the sensor located at or near the focal plane which remains spatially constant within sub-micron accuracies despite thermally produced changes in the focus of the lens.

Abstract: A head mounted display system with at least one retinal display unit having a curved reflector positioned in front of one eye or both eyes of a wearer. The unit includes a first set of three modulated visible-light lasers co-aligned and adapted to provide a laser beam with selectable color and a first scanner unit providing both horizontal and vertical scanning of the laser beam across a portion of the curved reflector in directions so as to produce a reflection of the color laser beam through the pupil of the eye onto a portion of the retina large enough to encompass the fovea.

Abstract: A celestial compass with a sky polarization feature. The celestial compass includes an inclinometer, a camera system for imaging at least one celestial object and a processor programmed with a celestial catalog providing known positions at specific times of at least one celestial object and algorithms for automatically calculating target direction information based on the inclination of the system as measured by the inclinometer and the known positions of at least one celestial object as provided by the celestial catalog and as imaged by the camera. Preferred embodiments include backup components to determine direction based on the polarization of the sky when celestial objects are not visible.

Abstract: A celestial weapons orientation measuring system. The system includes a miniature celestial direction detection device. The device includes an inclinometer, a camera for imaging at least one celestial object and a processor programmed with a celestial catalog providing known positions at specific times of at least one celestial object and algorithms for automatically calculating target direction information based on the inclination of the system as measured by the inclinometer and the known positions of the celestial object as provided by the celestial catalog and as imaged by the camera. Similar to the training technique discussed in the background section, the pretend enemy wears a GPS detector and transmitter, and a computer system is preferably provided which determines when a trigger-pull results in a “casualty”.

Abstract: A celestial direction finding system. The system includes an inclinometer, at least one camera for imaging both the daytime sky and the nighttime sky and a computer programmed with a sun, moon and star catalog and algorithms for automatically determining directions based on positions of celestial bodies imaged by at least one camera and incline positions measured by the inclinometer. In a preferred embodiment all of the above features are combined in a single battery operated miniature celestial direction finding module. Geographical positions of nearby objects can be determined with the addition of a rangefinder and knowledge of the geographical position of the camera. The geographical position of the system in preferred embodiments can be determined with the addition of a GPS unit.

Abstract: A passive optical crosswind profiling system. The system includes at least one telescope defining two apertures separated at a distance and adapted to collect light along at least two separate paths from a field of view containing a target and at least one high-speed digital camera defining at least one many pixel sensor wherein pixels of said at least one many pixel sensor are identified as separate blocks of pixels. The system further includes an optical system for focusing light collected along said at least two separate paths by said at least one telescope onto said at least one many pixel sensor to produce at least two images of the target scene and a high-speed computer processor programmed to with a special block matching correlation algorithm to correlate image data collected the separate blocks of pixels in order to calculate a crosswind profile along a path between said system and said target.

Abstract: A celestial compass kit. The kit includes an inclinometer, a camera system with a special telecentric fisheye lens for imaging at least one celestial object and a processor programmed with a celestial catalog providing known positions at specific times of at least one celestial object and algorithms for automatically calculating target direction information based on the inclination of the system as measured by the inclinometer and the known positions of at least one celestial object as provided by the celestial catalog and as imaged by the camera. The telecentric fisheye lens produces an image on the sensor located at or near the focal plane which remains spatially constant within sub-micron accuracies despite thermally produced changes in the focus of the lens.

Abstract: A head mounted display system with at least one retinal display unit having a curved reflector positioned in front of one eye or both eyes of a wearer. The unit includes a first set of three modulated visible-light lasers co-aligned and adapted to provide a laser beam with selectable color and a first scanner unit providing both horizontal and vertical scanning of the laser beam across a portion of the curved reflector in directions so as to produce a reflection of the color laser beam through the pupil of the eye onto a portion of the retina large enough to encompass the fovea.

Abstract: A celestial weapons orientation measuring system. The system includes a miniature celestial direction detection device. The device includes an inclinometer, a camera for imaging at least one celestial object and a processor programmed with a celestial catalog providing known positions at specific times of at least one celestial object and algorithms for automatically calculating target direction information based on the inclination of the system as measured by the inclinometer and the known positions of the celestial object as provided by the celestial catalog and as imaged by the camera. Similar to the training technique discussed in the background section, the pretend enemy wears a GPS detector and transmitter, and a computer system is preferably provided which determines when a trigger-pull results in a “casualty”.

Abstract: An improved beaconless adaptive optics system and process. A target is illuminated with a high energy laser beam of a directed energy laser. Wave front measurements are made of high energy laser beam reflections from the target. These wave front measurements are analyzed by a high speed processor to determine both high frequency phase components and low frequency phase components in the wave front data. (Applicants' experiments have shown that there is a direct correlation between beam spot size on the target and the phase variance of the reflected laser beam. The correlation is: the greater the phase variance the smaller the beam spot size.) Applicants have developed a technique for providing special control algorithms that provide very high speed control of the elements of a deformable mirror using this phase variance as a feedback parameter. Applicants have also developed algorithms to correct a limited number of Zernike modes associated with the wave front control.

Abstract: A system and process for converting a series of short-exposure, small-FOV zoom images to pristine, high-resolution images, of a face, license plate, or other targets of interest, within a fraction of a second. The invention takes advantage or the fact that some regions in a telescope field of view can be super-resolved; that is, features will appear in random regions which have resolution better than the diffraction limit of the telescope. This effect arises because the turbulent layer in the near-field of the object can act as a lens, focusing rays ordinarily outside the diffraction-limited cone into the distorted image. The physical effect often appears as magnified sub-regions of the image, as if one had held up a magnifying glass to a portion of the image. Applicants have experimentally shown these effects on short-range anisoplanatic imagery, along a horizontal path over the desert. In addition, they have developed powerful parallel processing software to overcome the warping and produce sharp images.

Abstract: A celestial direction finding system. The system includes an inclinometer, at least one camera for imaging both the daytime sky and the nighttime sky and a computer programmed with a sun, moon and star catalog and algorithms for automatically determining directions based on positions of celestial bodies imaged by at least one camera and incline positions measured by the inclinometer. In a preferred embodiment all of the above features are combined in a single battery operated miniature celestial direction finding module. Geographical positions of nearby objects can be determined with the addition of a rangefinder and knowledge of the geographical position of the camera. The geographical position of the system in preferred embodiments can be determined with the addition of a GPS unit.

Abstract: A passive optical crosswind profiling system. The system includes at least one telescope defining two apertures separated at a distance and adapted to collect light along at least two separate paths from a field of view containing a target and at least one high-speed digital camera defining at least one many pixel sensor wherein pixels of said at least one many pixel sensor are identified as separate blocks of pixels. The system further includes an optical system for focusing light collected along said at least two separate paths by said at least one telescope onto said at least one many pixel sensor to produce at least two images of the target scene and a high-speed computer processor programmed to with a special block matching correlation algorithm to correlate image data collected the separate blocks of pixels in order to calculate a crosswind profile along a path between said system and said target.

Abstract: An angles only aircraft navigation system. The system includes an IMU coupled with a passive optical sensor. The optical sensor provides periodic updates to the IMU in order to correct for accelerometer and gyro drifts. The IMU computes the air vehicle's instantaneous position, velocity, and attitude using gyro and accelerometer measurements. The optical sensor images stars and satellites. The navigation filter combines optical sensor measurements with IMU inputs, and determines those corrections needed to compensate for the IMU drifts. By applying periodic corrections to the IMU using satellite angular measurements, the navigation filter maintains an accurate position estimate during an entire flight.