公开(公告)号：US20170343325A1

公开(公告)日：2017-11-30

申请号：US15130526

申请日：2016-04-15

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Jacob ROVINSKY ,  Yoav TOURGEMAN

IPC: F41J2/00 ,  F41J2/02 ,  F41J9/08 ,  F41G7/00 ,  F42B8/24 ,  F42B8/12

CPC classification number: F41J2/00 ,  F41G7/003 ,  F41G7/004 ,  F41G7/006 ,  F41J2/02 ,  F41J9/08 ,  F42B8/12 ,  F42B8/24 ,  F42B10/60 ,  F42B10/62

Abstract: An inflatable dummy target comprising a chassis of inflatable ducts wrapped with a sheet.

公开(公告)号：US20170122705A1

公开(公告)日：2017-05-04

申请号：US15339011

申请日：2016-10-31

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Jacob ROVINSKY ,  Yoav TOURGEMAN

IPC: F41G7/00 ,  F42B8/24 ,  F41J2/02 ,  F41J9/08

CPC classification number: F41G7/002 ,  F41G7/003 ,  F41G7/004 ,  F41G7/006 ,  F41G7/30 ,  F41J2/02 ,  F41J9/08 ,  F42B8/24 ,  F42B12/58

Abstract: An inflatable dummy target comprising a chassis of inflatable ducts wrapped with a sheet. The chassis of inflatable ducts can include one or more ring shaped ducts and one or more elongate ducts. The chassis can include at least two ring shaped ducts interconnected by one or more elongate ducts. The dummy target can include several attached axi-symmetrical sections, each section have a chassis of inflatable ducts. Each section can be conical, frustoconical or cylindrical, thereby achieving a concave or convex dummy target geometry.

公开(公告)号：US20160231089A1

公开(公告)日：2016-08-11

申请号：US14935831

申请日：2015-11-09

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Jacob ROVINSKY

IPC: F41H11/02 ,  G01S13/00 ,  F41G7/30 ,  F42B15/01

CPC classification number: F41H11/02 ,  F41G7/30 ,  F41G7/303 ,  F42B15/01 ,  G01S7/003 ,  G01S13/003 ,  G01S13/878

Abstract: A counter-flying object system comprising a sensor array including at least one active sensor configured to detect and track the flying object, and a missile launcher configured to launch an interceptor to intercept the flying object, wherein upon launching of the interceptor, the sensor array is configured to determine the location of the interceptor and send said object and interceptor locations to a control system, the control system being configured to provide mission data to the interceptor based on said object and interceptor locations for guiding the interceptor toward the flying object and activating a fragmentation warhead on or in the vicinity of said flying object when a lethality criteria is met.

公开(公告)号：US20160047636A1

公开(公告)日：2016-02-18

申请号：US14861328

申请日：2015-09-22

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Jacob ROVINSKY ,  Yoav TOURGEMAN

IPC: F41J2/00

CPC classification number: F41J2/00 ,  F41G7/003 ,  F41G7/004 ,  F41G7/006 ,  F41J2/02 ,  F41J9/08 ,  F42B8/12 ,  F42B8/24

Abstract: An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile

Abstract translation: 一个可充气的虚拟目标，可以安装在能够在外部大气飞行期间从载体导弹释放的载体导弹; 在释放时，虚拟目标或其部分能够被充气并显示出类似GTG导弹特性的特征，其中GTG导弹特征包括IR签名，RF签名和GTG导弹

公开(公告)号：US20140240160A1

公开(公告)日：2014-08-28

申请号：US14063645

申请日：2013-10-25

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Jacob ROVINSKY ,  Yoav TOURGEMAN

IPC: F41J2/00

CPC classification number: F41J2/00 ,  F41G7/003 ,  F41G7/004 ,  F41G7/006 ,  F41J2/02 ,  F41J9/08 ,  F42B8/12 ,  F42B8/24

Abstract: An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile

Abstract translation: 一个可充气的虚拟目标，可以安装在能够在外部大气飞行期间从载体导弹释放的载体导弹; 在释放时，虚拟目标或其部分能够被充气并显示出类似GTG导弹特性的特征，其中GTG导弹特征包括IR签名，RF签名和GTG导弹

公开(公告)号：US20210310768A1

公开(公告)日：2021-10-07

申请号：US17340852

申请日：2021-06-07

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Michael MAIDANIK ,  Oded M. GOLAN ,  Miki LIVNE ,  Jacob ROVINSKY

IPC: F41G7/00 ,  G06T7/50 ,  G06T7/70

Abstract: The presently disclosed subject matter includes a computerized method and system for determining miss-distance between platforms. The proposed method and system make use of an electro optic sensor (e.g. camera) mounted on one of the platforms for obtaining additional data which is used for improving the accuracy of positioning data obtained from conventional positioning devices. A navigation error is calculated where the relative position of the two platforms is converted to the camera reference frame. Once the navigation error is available, it can be used to correct a measured miss-distance.

公开(公告)号：US20200182590A1

公开(公告)日：2020-06-11

申请号：US16472757

申请日：2017-12-24

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

Inventor： Michael MAIDANIK ,  Oded M. GOLAN ,  Miki LIVNE ,  Jacob ROVINSKY

IPC: F41G7/00 ,  G06T7/70 ,  G06T7/50

Abstract: The presently disclosed subject matter includes a computerized method and system for determining miss-distance between platforms. The proposed method and system make use of an electro optic sensor (e.g. camera) mounted on one of the platforms for obtaining additional data which is used for improving the accuracy of positioning data obtained from conventional positioning devices. A navigation error is calculated where the relative position of the two platforms is converted to the camera reference frame. Once the navigation error is available, it can be used to correct a measured miss-distance.