Abstract: A live-fire simulation system uses a position sensitive detector (PSD) in a weapon-mounted sensor to intercept emitted light from target emitters spatially distributed about a target. Each target emitter is modulated with a unique frequency. The system can thus not only determine the points of interception on the PSD but also determine which emitter caused which interception by using a frequency analysis.

Abstract: A live-fire simulation system uses a position sensitive detector (PSD) in a weapon-mounted sensor to intercept emitted light from target emitters spatially distributed about a target. Each target emitter is modulated with a unique frequency. The system can thus not only determine the points of interception on the PSD but also determine which emitter caused which interception by using a frequency analysis.

Abstract: A live-fire simulation system uses a position sensitive detector (PSD) in a weapon-mounted sensor to intercept emitted light from target emitters spatially distributed about a target. Each target emitter is modulated with a unique frequency. The system can thus not only determine the points of interception on the PSD but also determine which emitter caused which interception by using a frequency analysis.

Abstract: Various gun sights and related methods are provided. In one embodiment, a gun sight includes a light source adapted to project light, a user-viewable interface, and an optical element. The optical element includes a first surface adapted to pass the light to provide a reticle at the user-viewable interface. The optical element also includes a second surface adapted to refract the light to provide a light guide at a peripheral area of the user-viewable interface to aid a user to substantially align the user's eye with the reticle. Various mechanisms for aligning gun sights, attaching gun sights, related methods, and other embodiments are also provided.

Abstract: A scanning imaging apparatus including a rotatable support platform, an imaging device that is attached to the support platform; a mirror that is rotatably attached to the support platform and is configured to deflect an optical path of the imaging device; a first motor configured to continuously rotate the rotatable support platform at a first angular velocity; a second motor configured to change an angle of the mirror relative to an optical axis of the imaging device at a second relative angular velocity relative to the optical axis; and a controller configured to control the angle of the mirror so that a waveform of the angle of the mirror as a function of time does not have high frequency components.

Abstract: A scanning imaging apparatus including a rotatable support platform, a first imaging device that is attached to the support platform forming a first optical path, a second imaging device that is attached to the support platform forming a second optical path, a mirror having a first reflective surface and a second reflective surface opposite to the first reflective surface, the mirror rotatably attached to the support platform and configured to deflect the first optical path with the first reflective surface, and to deflect the second optical path with the second reflective surface, a first motor configured to continuously rotate the rotatable support platform at a first angular velocity, and a second motor configured to change an angle of the mirror relative to a first optical axis and a second optical axis formed by the first and second imaging devices.

Abstract: An optical hazard detection system for aircraft based on a dynamic parallax mechanism to alert the pilot of an object in the flight path by a selected amount of time in advance.

Abstract: A projectile tracking system for acquiring and precisely tracking a projectile in flight in order to reveal the source from which the projectile was fired. The source is revealed by the back projection of a 3-dimensional track file. The system is particularly suited for tracking a bullet fired by a sniper and identifying the location of the sniper. Projectiles of interest typically become hot due to aerodynamic heating. A telescope focuses infrared light from a relatively large field of view on to an infrared focal plane array. In a detection mode, the system searches for the infrared signature of the projectile. The telescope's field of view is steered in the azimuth by a step and stare mirror which is driven by an azimuth drive motor mounted on the frame. When a projectile is detected, the system switches to a tracking mode and the mirror is steered by the azimuth drive motor and a pivot motor to track the projectile.

Abstract: The present invention provides a projectile tracking system for acquiring and precisely tracking a projectile in flight in order to reveal the source from which the projectile was fired. The source is revealed by the back projection of a 3-dimensional track file. The system is particularly suited for tracking a bullet fired by a sniper and identifying the location of the sniper. Projectiles of interest are typically traveling at a substantial fraction of the speed of sound or even faster than the speed of sound and therefore become hot due to aerodynamic heating. A telescope focuses infrared light from a relatively large field of view on to an infrared focal plane array. In a projectile detection mode, the system searches for the infrared signature of the fast moving projectile. The telescope's field of view is steered in the azimuth by a step and stare mirror which is driven by an azimuth drive motor mounted on the frame.

Abstract: A compact coude optics system comprising a two axis gimbal system. Two mirrors rotate on one gimbal axis and the other two mirrors pivot on the other gimbal axis. The axes of the two gimbals intersect and light beams passing through the system effectively are turned at this point of intersection at a desired angle.