Abstract: A measuring apparatus for measuring the trajectory of a target object includes a receiving device having a primary mirror and a secondary mirror; a first detector for detecting first electromagnetic radiation having a first wavelength and a second detector for detecting second electromagnetic radiation having a second wavelength. The primary mirror is designed to reflect the first electromagnetic radiation and the second electromagnetic radiation and to direct the radiation onto a focal region. The secondary mirror is arranged between the primary mirror and the focal region and is designed to reflect only the second electromagnetic radiation in the direction of the second detector. The first detector is arranged behind the secondary mirror in the focal region of the primary mirror.

Abstract: A stationary test device for a missile includes a retaining device for an avionics testpiece of the missile, where the retaining device enables a movement of the avionics testpiece in three rotational degrees of freedom, and a display device configured to display information on the missile surroundings, where the display device is configured to be moved inside a virtual plane by a translational carriage system. The display device can be detected by the avionics testpiece if the avionics testpiece is disposed on the retaining device.

Abstract: A laser beam directing system including a first deflection mirror which is connected with an elevation axis of the laser beam directing system; a primary laser which is coupleable into telescope optics by the first deflection mirror; a first auxiliary laser that is oriented in parallel to an azimuth rotation axis of the laser beam directing system; a second auxiliary laser that is oriented parallel to an elevation rotation axis of the laser beam directing system; and a first detector, wherein the first auxiliary laser, the second auxiliary laser and the first detector are arranged and oriented in the laser beam directing system so that the first deflection mirror is alignable by comparing beams of the first auxiliary laser and the second auxiliary laser impacting the first detector so that a beam from the primary laser is coupleable into the telescope optics parallel to the elevation rotation axis.

Abstract: A method for automatically generating a three-dimensional reference model as terrain information for a seeker head of an unmanned missile. A three-dimensional terrain model formed from model elements obtained with the aid of satellite and/or aerial reconnaissance is provided. Position data of the imaging device at least at one planned position and a direction vector from the planned position of the imaging device to a predetermined target point in the three-dimensional terrain model are provided. A three-dimensional reference model of the three dimensional terrain model is generated that incorporates only those model elements and sections of model elements from the terrain model, which in the viewing direction of the direction vector from the planned position of the imaging device, are not covered by other model elements and/or are not located outside the field of view of the imaging device.

Abstract: An adjustable support assembly for an object to be accurately positioned relative to a base, in particular for a secondary mirror of an optical mirror telescope, has at least one support structure connected to the base and to the object. The support structure has at least two struts extending in a non-parallel manner relative to each other, where each strut has associated therewith a drivable actuator element in such a way that the actuator element applies a force onto the strut that deflects the strut transversely to the longitudinal extension thereof. The support structure may be supported in an articulated manner relative to the base.

Abstract: The present embodiment relates to a guided missile launch system comprising a launch tube with a guided missile space for receiving a guided missile and with a cartridge space for receiving a blank cartridge, further comprising a handle piece mountable on the launch tube and separable from the launch tube, the handle piece having a striking pin system for firing the blank cartridge.

Abstract: A method for local stabilization of a radiation spot formed by a high energy laser beam includes receiving radiation reflected by the target object, where the radiation reflected by the target object passes through the same optical path as the high energy laser beam. An image processing is performed by analyzing and comparing the image of the illuminated target object or part of the illuminated target object to at least one image of the illuminated target object or part of the illuminated target object produced at a prior point in time. A correction signal is computed, with which an optical correction device is actuated. A filter correction signal is produced by a filter device, while a controller correction signal is produced by a fine tracking controller. Finally, the correction signal is formed from the filter correction signal and the controller correction signal.

Abstract: A method for focusing a beam of a high energy radiation source on a reference point on the surface of a flying object, comprising: recording a number of consecutive two-dimensional images of the flying object determining the trajectory of the flight path simultaneously determining the line of sight angle between the image acquisition device and the position of the flying object calculating a three-dimensional model of the flying object displaying the currently acquired two-dimensional image marking the reference point on the displayed two-dimensional image of the flying object; calculating the three-dimensional reference point on the surface of the flying object focusing the beam of the high energy radiation source on the three-dimensional reference point.

Abstract: An active system includes a transmitting/capturing device having a detection device configured to capture a target object, where the transmitting/capturing device includes a laser source and a camera. The active system also includes a first control system configured to drive a first positioning system to align a beam path between the transmitting/capturing device and the target object, and a second control system configured to drive a second positioning system to align the beam path. The active system further includes a third control system configured to drive a third positioning system to align the transmitting/capturing device, where the third control system has an additional capturing device, and the third positioning system can be driven on the basis of data from the additional capturing device.

Abstract: An airborne laser weapon system is divided into a ground-based unit and an airborne unit. The relatively heavy components of the laser weapon system, such as the generator, cooling elements with cooling fluid, accumulators, pump diodes, beam couplers and the control station for an operator, are concentrated and/or arranged in the ground-based part. The relatively lightweight components and/or those that ultimately determine the quality of the laser beam, such as active laser element(s), in particular the output stage(s) thereof, the focusing drive, the telescope and the necessary sensors, may be provided on the airborne platform and may be connected by means of a relatively long, e.g. multiple kilometers, optical waveguide to the ground-based part.

Abstract: A radiation emitter includes a device for coupling radiation from at least one radiation generator and a radiation combining device that combines the radiation to bundled radiation. The radiation combining device includes a telescopic optic with a collimation reflector and a secondary reflector. The radiation combining device is configured to accept directional radiation from a plurality of light conducting devices from at least one radiation generator.

Abstract: A fire control sight for a hand-held firearm includes a sight housing, a front sight, and a sight guide having two sight guide side pieces with a plurality of sight crosspieces forming rear sights. The fire control sight also includes a range finder, at least one inertial sensor and/or a magnetic field sensor, a control computer, and a display device for displaying an optimal orientation of the barrel axis of the hand-held firearm determined by the control computer.

Abstract: An active system includes a transmitting/capturing device having a detection device configured to capture a target object, where the transmitting/capturing device includes a laser source and a camera. The active system also includes a first control system configured to drive a first positioning system to align a beam path between the transmitting/capturing device and the target object, and a second control system configured to drive a second positioning system to align the beam path. The active system further includes a third control system configured to drive a third positioning system to align the transmitting/capturing device, where the third control system has an additional capturing device, and the third positioning system can be driven on the basis of data from the additional capturing device.

Abstract: An optical device for a missile seeker head includes an optical sensor with a plurality of pixels, a light source, a detection device, and an optical system. The light source is configured to illuminate, using the optical system, an object that can be mapped using the optical system on at least one subarea of a predefined pixel of the optical sensor. The detection device is configured to detect the light emitted from the light source and reflected by the object.

Abstract: A laser illumination unit for illuminating a target object with high-power laser radiation includes multiple rigidly-interconnected laser beam modules that are designed to emit laser radiation and an aiming unit to aim the laser beam modules at the target object. Each of the laser beam modules includes an optical element that is designed to aim laser radiation at a target point of the target object.

Abstract: A digital filter for reducing a sampling rate for an input signal includes a parallelizing block for splitting the input signal into at least two parallel raw signals, an integration block for converting the parallel raw signals into an intermediate signal, and a differentiation block for generating an output signal by differentiating the intermediate signal. The integration block includes a logic block that is designed for generating two parallel sum signals from the parallel raw signals using summation operations, and a recursion block that is designed for generating the intermediate signal recursively from the parallel sum signals.

Abstract: An underwater vehicle includes an optical beam operating system having a radiation generator, a radiation emission device, and a radiation transmission device connecting the radiation generator to the radiation emission device. The radiation generator is provided on or in the underwater vehicle. The radiation emission device can be brought to the water surface by the underwater vehicle.

Abstract: A device for testing and/or operating an effector unit for acting on a target includes a positioner unit for moving the effector unit and a control unit for driving the positioner unit. The control unit is configured to simulate and/or to damp the accelerations of a carrier platform, on which the device can be mounted under real conditions, by means of the positioner unit.

Abstract: A load test stand includes a frame, a flange, and a spring mechanism. The spring mechanism is mounted on the frame and includes a symmetrical arrangement of at least four spring elements. The spring mechanism also includes frame points connecting the spring mechanism and the frame and articulation points connecting the spring mechanism and the flange. The flange can be coupled, by an adapter, to the output shaft of a servo system that is to be tested.

Abstract: A beam focusing unit for a laser weapon system includes a laser generating unit, an output element unit, and a beam optics element. The beam focusing unit includes a stationary/partly movable part and a fully movable part. The stationary/partly movable part is adapted for positioning or for transporting the beam focusing unit between operations. The fully movable part is adapted for targeting and target-following of the laser weapon system. The beam optics element and the at least one output element unit is arranged on the fully movable part.