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公开(公告)号：US10697794B2
公开(公告)日：2020-06-30
申请号：US15852697
申请日：2017-12-22
发明人： Bernd Nagelrauf
摘要： A flight-path determination device for determining a flight path of a flying object has a position determination apparatus to detect a position of the flying object, an alignment apparatus that to verify whether the position of the flying object is within one specified approach path of a number of specified approach paths, and a path determination apparatus to output the relevant approach path as the flight path of the flying object if the position of the flying object is within one of the specified approach paths.
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公开(公告)号：US10451477B2
公开(公告)日：2019-10-22
申请号：US14941175
申请日：2015-11-13
发明人： Georg Beidenhauser
摘要： The present invention relates to a monitoring apparatus for a laser beam, including a body having a passage opening and a sensor that is disposed on the body, wherein impact of the laser beam onto the body can be detected using the sensor.
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公开(公告)号：US09874422B2
公开(公告)日：2018-01-23
申请号：US15048202
申请日：2016-02-19
CPC分类号： F41G7/002 , B64C27/08 , F41G7/001 , F41G7/005 , G06F17/5009
摘要： 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. A mobile test device for the missile includes a flight platform, a carrier device mounted on the flight platform, for an avionics testpiece of the missile, wherein the carrier device enables a movement of the avionics testpiece in three rotational degrees of freedom, and a control module, where the control module is configured to control the flight platform for taking off on a specified reference trajectory, control the carrier device for orientation of the avionics testpiece, and store navigation data generated by the avionics testpiece. Finally, a test system for the missile includes the stationary test device and the mobile test device.
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公开(公告)号：US09816786B2
公开(公告)日：2017-11-14
申请号：US13091703
申请日：2011-04-21
CPC分类号： F41G7/2226 , F41G7/2253 , F41G7/2293 , G01S3/7865 , G06T17/05
摘要： 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.
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公开(公告)号：US20140245942A1
公开(公告)日：2014-09-04
申请号：US14352908
申请日：2012-10-18
发明人： Thomas Hagen
CPC分类号： B63G8/28 , B63G8/38 , F41H13/005
摘要： 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.
摘要翻译： 水下航行器包括具有辐射发生器，辐射发射装置和将辐射发生器连接到辐射发射装置的辐射传输装置的光束操作系统。 辐射发生器设置在水下航行器上或其中。 辐射发射装置可以由水下航行器带到水面。
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公开(公告)号：US20140218790A1
公开(公告)日：2014-08-07
申请号：US13951868
申请日：2013-07-26
发明人： Thomas HAGEN
CPC分类号： H01S3/005 , F41H13/0062 , H01S3/0007 , H01S3/06754 , H01S3/06783
摘要： 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.
摘要翻译： 用于激光武器系统的光束聚焦单元包括激光产生单元，输出元件单元和光束光学元件。 光束聚焦单元包括静止/部分可移动部分和完全可移动部分。 固定/部分可移动部件适于在操作之间定位或输送光束聚焦单元。 完全可动部分适用于激光武器系统的目标跟踪。 光束光学元件和至少一个输出元件单元布置在完全可移动部分上。
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公开(公告)号：US11187494B2
公开(公告)日：2021-11-30
申请号：US17084160
申请日：2020-10-29
发明人： Robert Kroyer
摘要： A modular missile launch system for launching missiles from a mobile platform includes a rectangular first support frame having a first longitudinal beam having a platform coupling structure formed for releasably fastening the first support frame to the mobile platform. A second longitudinal beam arranged at a distance from the first longitudinal beam includes a first connecting structure on an underside and a launch tube securing structure for mounting a missile launch tube to the first support frame. The first connecting structure defines a first plug connection portion extending in a longitudinal direction, onto which a second support frame with a second plug connection portion can be plugged in the vertical direction, having at least two first through bores that are spaced apart in the longitudinal direction, through each of which one connecting device can be passed in order to secure the first and the second support frame.
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公开(公告)号：US20210131763A1
公开(公告)日：2021-05-06
申请号：US17084160
申请日：2020-10-29
发明人： Robert KROYER
摘要： A modular missile launch system for launching missiles from a mobile platform includes a rectangular first support frame having a first longitudinal beam having a platform coupling structure formed for releasably fastening the first support frame to the mobile platform. A second longitudinal beam arranged at a distance from the first longitudinal beam includes a first connecting structure on an underside and a launch tube securing structure for mounting a missile launch tube to the first support frame. The first connecting structure defines a first plug connection portion extending in a longitudinal direction, onto which a second support frame with a second plug connection portion can be plugged in the vertical direction, having at least two first through bores that are spaced apart in the longitudinal direction, through each of which one connecting device can be passed in order to secure the first and the second support frame.
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9.发明授权公开(公告)号：US10429158B2
公开(公告)日：2019-10-01
申请号：US15344059
申请日：2016-11-04
发明人： Jörg Lutzenberger
摘要： A folding wing for a missile comprises a wing root, an upper wing part foldably supported at the wing root around a swiveling axis, at least one first elastically pre-stressed force element and a latching device. The at least one first elastically pre-stressed force element is coupled with the wing root and the upper wing part and is designed for permanently urging the upper wing part into a working position relative to the wing root through introducing a torque. The latching device is designed for arresting the upper wing part on reaching the working position automatically.
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10.发明授权公开(公告)号：US10317179B2
公开(公告)日：2019-06-11
申请号：US15344072
申请日：2016-11-04
发明人： Jörg Lutzenberger
摘要： A folding wing comprises a wing root, an upper wing part foldable relative to the wing root, at least one guiding device, and an elastically pre-stressed force element. The upper wing part comprises an end edge and a profile foot, wherein the wing root comprises a base and an opposing receiving groove, which is designed to receive the profile foot in a flush manner and is delimited by two delimiting edges having a separation distance that at least equals the maximum profile thickness of the profile foot. The guiding device is arranged at one of the upper wing part and the wing root and is designed for guiding the profile foot in a variable distance to the ground of the receiving groove. The force element is coupled with the wing root and the upper wing part and urges the upper wing part into the receiving groove through the pre-stress.
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