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1. 发明授权

US12000674B1 Handheld integrated targeting system (HITS) 有权
公开(公告)号：US12000674B1
公开(公告)日：2024-06-04
申请号：US16602648
申请日：2019-11-18
申请人： Loran Ambs
发明人： Loran Ambs
IPC分类号： F41G3/06 , F41G9/00 , G01S13/72 , G01S13/86
CPC分类号： F41G3/06 , F41G9/00 , G01S13/723 , G01S13/86
摘要： An aiming system for handheld weapons that includes a target detection and tracking system; an IMU integrated with the target detection and tracking system, weapon launching system; an IMU integrated with the weapon launching system, a fire control computer and a display system enabling the weapons launcher operator to point the weapon with the appropriate elevation and azimuth for the weapon projectile to intercept the intended target.

2. 发明授权

US11714407B2 Machine to machine targeting maintaining positive identification 有权
公开(公告)号：US11714407B2
公开(公告)日：2023-08-01
申请号：US17395102
申请日：2021-08-05
申请人： AEROVIRONMENT, INC.
发明人： Macdonald John Peebles , Andrew Martin , Charles Lawrence Baker , Daisy Wang , Kevin Jay Aguilar , Matthew Allen Hanna , Brian Young , Eric Sornborger , Eric James Aagaard
IPC分类号： G05D1/00 , B64C39/02 , B64D1/04 , B64D47/08 , G01C11/06 , F41G3/02 , F41G7/22 , B64D1/16 , F41G3/04 , F41G3/14 , F41G3/16 , F41G7/00 , G08G5/00 , G01C23/00 , F41G7/20 , F41G9/00
CPC分类号： G05D1/0027 , B64C39/024 , B64D1/04 , B64D1/16 , B64D47/08 , F41G3/02 , F41G3/04 , F41G3/145 , F41G3/165 , F41G7/007 , F41G7/20 , F41G7/2233 , F41G9/00 , G01C11/06 , G01C23/00 , G08G5/0047 , G08G5/0013 , G08G5/0026 , G08G5/0034 , G08G5/0069
摘要： A method of targeting, which involves capturing a first video of a scene about a potential targeting coordinate by a first video sensor on a first aircraft; transmitting the first video and associated potential targeting coordinate by the first aircraft; receiving the first video on a first display in communication with a processor, the processor also receiving the potential targeting coordinate; selecting the potential targeting coordinate to be an actual targeting coordinate for a second aircraft in response to viewing the first video on the first display; and guiding a second aircraft toward the actual targeting coordinate; where positive identification of a target corresponding to the actual targeting coordinate is maintained from selection of the actual targeting coordinate.

3. 发明授权

US11579610B2 System and method for interception and countering unmanned aerial vehicles (UAVS) 有权
公开(公告)号：US11579610B2
公开(公告)日：2023-02-14
申请号：US15982578
申请日：2018-05-17
申请人： AeroVironment, Inc.
发明人： Christopher Eugene Fisher , Michael Franklin Morgan
IPC分类号： B64C39/02 , G05D1/00 , F41H11/02 , F41G9/00 , G05D1/10 , F41H13/00 , F41G7/22 , F41G7/30 , G05D1/12
摘要： Systems, devices, and methods for identifying a target aerial vehicle, deploying an interceptor aerial vehicle comprising at least one effector, maneuvering the interceptor aerial vehicle to a position to engage a target aerial vehicle, deploying the at least one effector to intercept the target aerial vehicle, and confirming that the target aerial vehicle has been intercepted.

4. 发明授权

US11300670B2 Weapon on-board velocity and range tracking 有权
公开(公告)号：US11300670B2
公开(公告)日：2022-04-12
申请号：US16782106
申请日：2020-02-05
申请人： BAE SYSTEMS Information and Electronic Systems Integration Inc.
发明人： Michael J. Choiniere , Jason H. Batchelder , Matthew F. Chrobak
IPC分类号： F41G9/00 , G01S11/08
摘要： The system and method of weapon on-board range and velocity tracking using a synchronized clock and a pulse beacon on a fire control system, or the like, coupled with an on-board rear-facing detector and processor. A round or a UAS may use this system to accurately estimate range with respect to the fire control system, over time, and the round's or UAS's velocity at various times along its flight path. The system provides for smaller miss distances, and the like.

5. 发明申请

US20200096291A1 DETERMINATION OF GUIDED-MUNITION ROLL ORIENTATION 审中-公开
公开(公告)号：US20200096291A1
公开(公告)日：2020-03-26
申请号：US16467357
申请日：2017-01-05
申请人： BAE Systems Information and Electronic Systems Integration Inc.
发明人： David J. Schorr , Jason H. Batchelder , Jeremy B. Gibson , James H. Steenson, Jr. , Joseph D. Vasile
IPC分类号： F41G7/36 , F41G9/00 , F42B15/08 , G05D1/10 , F42B15/01 , F41G7/22
摘要： Techniques are provided for determination of a guided-munition orientation during flight based on lateral acceleration, velocity, and turn rate of the guided-munition. A methodology implementing the techniques, according to an embodiment, includes obtaining a lateral acceleration vector measurement and a velocity of the guided-munition, and calculating a ratio of the two, to generate an estimated lateral turn vector of the guided-munition. The method also includes integrating the estimated lateral turn vector, over a period of time associated with flight of the guided-munition, to generate a first type of predicted attitude change. The method further includes obtaining and integrating a lateral turn rate vector measurement of the guided-munition, over the period of time associated with flight of the guided-munition, to generate a second type of predicted attitude change. The method further includes calculating a gravity direction vector based on a difference between the first and second types of predicted attitude change.

6. 发明授权

US10337835B2 Method and system for using enhanced location-based information to guide munitions 有权
公开(公告)号：US10337835B2
公开(公告)日：2019-07-02
申请号：US15591681
申请日：2017-05-10
申请人： Rivada Research, LLC
发明人： Clint Smith
IPC分类号： F41G3/00 , F41G3/02 , F41G3/04 , F41G7/00 , F42B15/00 , F41G9/00 , F41G7/36 , G01S5/00 , G01S11/00 , G05D1/10 , F41G7/22 , G01S5/02 , G01S11/02 , G05D1/12 , F41G7/30 , F41G7/34
摘要： An ordnance munition is included in an intelligent ordnance projectile delivery system and equipped with targeting and guidance systems that allow the ordnance munition to collaborate with other devices to intelligently select targets and/or to guide the ordnance munition to its selected target. The ordnance munition may determine its approximate current location, form a communication group with a wireless transceiver that is in close proximity, and send the approximate current location to the wireless transceiver and/or other devices in the communication group. In response, the ordnance munition may receive location information from the wireless transceiver and/or other devices that are in the communication group. The ordnance munition may determine its more precise location based on the information received from the wireless transceiver, and alter its flight path based in the updated and more precise location.

7. 发明授权

US10302398B2 Vehicle based independent range system (VBIRS) 有权
公开(公告)号：US10302398B2
公开(公告)日：2019-05-28
申请号：US15589440
申请日：2017-05-08
申请人： Space Information Laboratories, LLC
发明人： Edmund David Burke , Martin Stewart Waldman
IPC分类号： F41G7/00 , F41G3/04 , F41G9/00 , F41G7/36 , F41G7/34 , G01S5/00 , B64G1/00 , B64G1/10 , F41G7/22 , B64G1/24
摘要： A Vehicle Based Independent Range System (VBIRS) (10) comprised of individual stacked chambered modules that function as a single integrated system that provides a self-contained space based range capability, and is comprised of a power module (12), an artificial intelligence/autonomous engagement/flight termination system module (20), a satellite data modem module system (30) and a navigation, communications and control module system (40), all of which interface with a VBIRS test and checkout system (52) and a weather data system (116). The artificial intelligence/autonomous engagement/flight termination system module (20) is comprised of an inherent artificial intelligence capability that envelopes and interchanges data with an autonomous engagement controller (22) that contains all missile/rocket autonomous cooperative engagement, destruct decision software and range safety algorithm parameters required for optimum mission planning. VBIRS employed aboard an aircraft or between any combination of launching systems allows that aircraft to launch a missile/rocket from any location on earth, whether the missile/rocket is singularly launched by itself or as a larger group of missiles/rockets launched in a salvo arrangement, while providing collaborative real-time targeting to occur directly between missiles/rockets in conjunction with other missile/rocket launch platforms or stand-alone mission control centers.

8. 发明授权

US10260840B2 Mobile ballistics processing and display system 有权
公开(公告)号：US10260840B2
公开(公告)日：2019-04-16
申请号：US14599894
申请日：2015-01-19
申请人： GeoBallistics, LLC
发明人： Joe D. Baker , Jeffrey P. Barstad
IPC分类号： G09G5/00 , F41G9/00 , G06K9/00 , F41G3/02 , F41G3/06 , F41G3/08
摘要： A mobile ballistics processing and display system for receiving data associated with one or more ballistics variables, for processing such variables, and for displaying a ballistics solution associated with such variables in an easily and quickly understandable map format. One or more ballistics variables are inputted into a mobile computing device or are otherwise acquired by such device. Projected in-flight projectile characteristics are calculated by the computing device based upon ballistics variables. Users are provided with the ability to input in-flight bullet characteristics criteria into the computing device. The computing device is configured to depict in map format, projected paths of a projectile from one or more shooter locations to one or more target locations. Differing graphical representations of the projected path of the projectile may be displayed, depending on how the projected in-flight projectile characteristics compare to the in-flight projectile characteristics criteria at each step of the projected path.

9. 发明授权

US10222177B2 Multimode unmanned aerial vehicle 有权
公开(公告)号：US10222177B2
公开(公告)日：2019-03-05
申请号：US14832688
申请日：2015-08-21
申请人： AeroVironment, Inc.
发明人： Carlos Thomas Miralles
IPC分类号： G05D1/00 , F41G7/22 , F41G7/00 , F41G9/00 , G08G5/00 , B64C39/02 , G05D1/12
摘要： A system comprising an unmanned aerial vehicle (UAV) configured to transition from a terminal homing mode to a target search mode, responsive to an uplink signal and/or an autonomous determination of scene change.

10. 发明授权

US09863739B2 Vertical drop segmented munitions dispenser 有权
公开(公告)号：US09863739B2
公开(公告)日：2018-01-09
申请号：US14861010
申请日：2015-09-22
申请人： The Boeing Company
发明人： William C. Hester, Jr.
IPC分类号： B64D1/04 , F41F5/00 , F41G7/00 , F41G7/22 , F41G7/34 , F41G9/00 , B64D1/06 , F41F3/065
CPC分类号： F41F5/00 , B64C39/024 , B64C2201/024 , B64C2201/121 , B64D1/06 , F41F3/065 , F41G7/007 , F41G7/226 , F41G7/2293 , F41G7/346 , F41G9/002
摘要： A munitions dispenser employs a plurality of launch tubes mounted in an array as a segmented dispenser assembly. Each tube in the array is configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture. A frame, mountable to an air vehicle, carries the array of launch tubes. A skin covers the array of launch tubes with the skin and frame with the array configured for nested engagement of multiple segmented assemblies.

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