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1. 发明申请

WO2003102505A1 AIRBORNE RECONNAISSANCE SYSTEM 审中-公开
标题翻译： AIRBORNE重新建立系统
公开(公告)号：WO2003102505A1
公开(公告)日：2003-12-11
申请号：PCT/IL2003/000422
申请日：2003-05-22
申请人： RAFAEL - ARMAMENT DEVELOPMENT AUTHORITY LTD. , GREENFELD, Israel , YAVIN, Zvi , UHL, Bernd
发明人： GREENFELD, Israel , YAVIN, Zvi , UHL, Bernd
IPC分类号： G01C11/02
CPC分类号： G01S3/7864 , F41G5/14 , F41G7/2213 , F41G7/2253 , F41G7/2293 , G01C11/025 , G01C21/005 , G01C21/165
摘要： An airborne reconnaissance system comprising: (1) Gimbals having at least two degrees of freedom; (2) At least one array of light sensors positioned on the gimbals, for being directed by the same within at least two degrees of freedom; (3) Map storage means for storing at least one Digital Elevation Map of an area of interest, divided into portions; (4) Inertial Navigation System for real-time providing to a gimbals control unit navigation and orientation data of the aircraft with respect to a predefined global axes system;(5) Portion selection unit for selecting, one at a time, another area portion from the area of interest; and (6) servo means for directing the gimbals. The system uses data from the inertial navigation system and from the digital elevation map for real-time calculating direction to selected area portions, and for maintaining the direction during integration of light from the terrain, and for producing corresponding images of area portions.
摘要翻译：一种机载侦察系统，包括：（1）具有至少两个自由度的万用表; （2）定位在万向面上的至少一组光传感器，由至少两个自由度引导; （3）地图存储装置，用于存储感兴趣区域的至少一个数字高程图，被分成多个部分; （4）惯性导航系统，用于相对于预定义的全局轴系统实时提供飞行器的万向节控制单元导航和取向数据;（5）部分选择单元，用于一次一个地从另一个区域部分感兴趣的领域和（6）用于引导万向架的伺服装置。该系统使用来自惯性导航系统的数据和数字高程图的实时计算方向的数据，并且用于在来自地形的光的集成期间保持方向，并且用于产生区域部分的相应图像。

2. 发明授权

EP1508020B2 AIRBORNE RECONNAISSANCE SYSTEM 有权
标题翻译： LUFTAUFKLÄRUNGSSYSTEM
公开(公告)号：EP1508020B2
公开(公告)日：2017-03-08
申请号：EP03725555.1
申请日：2003-05-22
申请人： RAFAEL - ARMAMENT DEVELOPMENT AUTHORITY LTD.
发明人： GREENFELD, Israel , YAVIN, Zvi , UHL, Bernd
IPC分类号： G01C11/02 , G01S3/786
CPC分类号： G01S3/7864 , F41G5/14 , F41G7/2213 , F41G7/2253 , F41G7/2293 , G01C11/025 , G01C21/005 , G01C21/165

3. 发明授权

EP1508020B1 AIRBORNE RECONNAISSANCE SYSTEM 有权
标题翻译： AIR教育体系
公开(公告)号：EP1508020B1
公开(公告)日：2007-04-18
申请号：EP03725555.1
申请日：2003-05-22
申请人： RAFAEL - ARMAMENT DEVELOPMENT AUTHORITY LTD.
发明人： GREENFELD, Israel , YAVIN, Zvi , UHL, Bernd
IPC分类号： G01C11/02 , G01S3/786
CPC分类号： G01S3/7864 , F41G5/14 , F41G7/2213 , F41G7/2253 , F41G7/2293 , G01C11/025 , G01C21/005 , G01C21/165
摘要： An airborne reconnaissance system comprising: (1) Gimbals having at least two degrees of freedom; (2) At least one array of light sensors positioned on the gimbals, for being directed by the same within at least two degrees of freedom; (3) Map storage means for storing at least one Digital Elevation Map of an area of interest, divided into portions; (4) Inertial Navigation System for real-time providing to a gimbals control unit navigation and orientation data of the aircraft with respect to a predefined global axes system;(5) Portion selection unit for selecting, one at a time, another area portion from the area of interest; and (6) servo means for directing the gimbals. The system uses data from the inertial navigation system and from the digital elevation map for real-time calculating direction to selected area portions, and for maintaining the direction during integration of light from the terrain, and for producing corresponding images of area portions.

4. 发明公开

EP1508020A1 AIRBORNE RECONNAISSANCE SYSTEM 有权
标题翻译： AIR教育体系
公开(公告)号：EP1508020A1
公开(公告)日：2005-02-23
申请号：EP03725555.1
申请日：2003-05-22
申请人： RAFAEL - ARMAMENT DEVELOPMENT AUTHORITY LTD.
发明人： GREENFELD, Israel , YAVIN, Zvi , UHL, Bernd
IPC分类号： G01C11/02 , G01S3/786
CPC分类号： G01S3/7864 , F41G5/14 , F41G7/2213 , F41G7/2253 , F41G7/2293 , G01C11/025 , G01C21/005 , G01C21/165
摘要： An airborne reconnaissance system comprising: (1) Gimbals having at least two degrees of freedom; (2) At least one array of light sensors positioned on the gimbals, for being directed by the same within at least two degrees of freedom; (3) Map storage means for storing at least one Digital Elevation Map of an area of interest, divided into portions; (4) Inertial Navigation System for real-time providing to a gimbals control unit navigation and orientation data of the aircraft with respect to a predefined global axes system;(5) Portion selection unit for selecting, one at a time, another area portion from the area of interest; and (6) servo means for directing the gimbals. The system uses data from the inertial navigation system and from the digital elevation map for real-time calculating direction to selected area portions, and for maintaining the direction during integration of light from the terrain, and for producing corresponding images of area portions.

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