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1. 发明授权

CN105050898B 针对对地观测空间任务的创新轨道设计有权
公开(公告)号：CN105050898B
公开(公告)日：2017-07-11
申请号：CN201380067049.2
申请日：2013-12-20
申请人：泰雷兹阿莱尼亚宇航意大利单一股东有限责任公司
发明人：法比奥·迪乔治 , 安德烈亚·弗兰乔尼 , 亚历山德罗·克里琴蒂
IPC分类号： B64G1/10 , B64G1/24 , G01S13/90
CPC分类号： G01S13/9023 , B64G1/1021 , B64G1/242 , B64G1/405 , B64G2001/1035 , G01S13/90 , G06F17/10
摘要：本发明涉及用于减少卫星遥感服务的成本的方法。所述方法包括提供卫星遥感系统，该卫星遥感系统包括配备有被配置成获取地球表面的区域的图像的传感器的唯一一个卫星，所述卫星遥感系统被设计成基于由卫星上的传感器获取的图像提供卫星遥感服务。特别地，卫星遵循绕地球的具有短于三天的轨道重复周期的预定义轨道，从而获得具有非常好的时间性能和优异的干涉能力并且具有极大减少的成本的卫星遥感服务。

2. 发明公开

CN107323685A 敏捷SAR小卫星及其总体设计方法无效
公开(公告)号：CN107323685A
公开(公告)日：2017-11-07
申请号：CN201710343713.1
申请日：2017-05-16
申请人：上海卫星工程研究所
发明人：叶兴彬 , 于迎军 , 陆晴 , 庄磊
IPC分类号： B64G1/10
CPC分类号： B64G1/10 , B64G2001/1035
摘要：本发明提供了一种敏捷SAR小卫星及其总体设计方法，该卫星包括太阳电池阵、卫星本体、载荷专用顶板、反作用飞轮、冷气贮存箱，太阳电池阵位于卫星本体的上方，卫星本体位于载荷专用顶板的上方，太阳电池阵位于载荷专用顶板的上方，反作用飞轮位于冷气贮存箱的一侧，冷气贮存箱位于太阳电池阵的下方，反作用飞轮位于载荷专用顶板的上方。本发明大大降低了星载SAR系统的重量和体积，具有强轨道适应能力、高敏捷机动、高精度跟踪能力、研制周期短、成本低、发射灵活、启用速度快、性能高的特点。

3. 发明公开

CN105050898A 针对对地观测空间任务的创新轨道设计有权
公开(公告)号：CN105050898A
公开(公告)日：2015-11-11
申请号：CN201380067049.2
申请日：2013-12-20
申请人：泰雷兹阿莱尼亚宇航意大利单一股东有限责任公司
发明人：法比奥·迪乔治 , 安德烈亚·弗兰乔尼 , 亚历山德罗·克里琴蒂
IPC分类号： B64G1/10 , B64G1/24 , G01S13/90
CPC分类号： G01S13/9023 , B64G1/1021 , B64G1/242 , B64G1/405 , B64G2001/1035 , G01S13/90 , G06F17/10
摘要：本发明涉及用于减少卫星遥感服务的成本的方法。所述方法包括提供卫星遥感系统(1)，该卫星遥感系统(1)包括配备有被配置成获取地球表面的区域的图像的传感器(111)的唯一一个卫星(11)，所述卫星遥感系统(1)被设计成基于由卫星(11)上的传感器(111)获取的图像提供卫星遥感服务。特别地，卫星(11)遵循绕地球的具有短于三天的轨道重复周期的预定义轨道，从而获得具有非常好的时间性能和优异的干涉能力并且具有极大减少的成本的卫星遥感服务。

4. 发明授权

US10871560B2 Radar satellite and radar satellite system using radar satellite 有权
公开(公告)号：US10871560B2
公开(公告)日：2020-12-22
申请号：US15527042
申请日：2015-11-09
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA
发明人： Toyotoshi Kurose
IPC分类号： G01S13/90 , B64G1/26 , B64G1/22 , G01S7/03 , G01S13/89 , G01S7/02 , B64G1/10 , B64G1/44 , G01S7/00 , G01S7/28 , B64G1/64
CPC分类号： G01S13/90 , B64G1/1014 , B64G1/222 , B64G1/26 , B64G1/443 , G01S7/003 , G01S7/02 , G01S7/03 , G01S7/28 , G01S13/89 , B64G1/648 , B64G2001/1035
摘要： A radar satellite of the present invention comprises a radar unit including a plurality of radar panels coupled to each other in a single flat plate shape, each of the plurality of radar panels including a plurality of antennas which transmit and receive radar waves, and a solar cell; and a communication/control unit which performs communications with a spot on an earth or a spacecraft. The radar unit includes: a radar panel array which is a plate-shaped structure including the plurality of radar panels; and a deployable truss structure including a plurality of side frame members supporting the plurality of radar panels, respectively, and coupled to each other in such a manner that the side frame members are foldable and deployable.

5. 发明申请

US20180172824A1 SYSTEMS AND METHODS FOR ENHANCING SYNTHETIC APERTURE RADAR IMAGERY 审中-公开
公开(公告)号：US20180172824A1
公开(公告)日：2018-06-21
申请号：US15737044
申请日：2016-06-15
申请人： Urthecast Corp , King Abdulaziz City of Science and Technology
发明人： Keith Dennis Richard Beckett , George Tyc
IPC分类号： G01S13/90 , G06T1/20 , G01S13/86 , G06K9/62 , B64G1/10
CPC分类号： G01S13/904 , B64G1/1021 , B64G1/1085 , B64G2001/1028 , B64G2001/1035 , G01S13/867 , G01S13/90 , G06K9/6267 , G06T1/20
摘要： An image processing system generates enhanced synthetic aperture radar (SAR) imagery using a trainer that generates an information model that defines a set of trained data based on correlated classifications of pairs of spatially and/or temporally coincident SAR and optical images, and using a SAR image enhancer that applies a transformation to generate a color image from the SAR image data. Correlated classifications may be based on specific applications. The system may generate or update trained data to be used for classification based on a set of training SAR images and training optical images. The system may assess or determine correlations between the classified SAR and optical image data sets, establishing levels of confidence in such correlations.

6. 发明申请

US20140191894A1 THREE-DIMENSIONAL POSITIONING METHOD 审中-公开
标题翻译：三维定位方法
公开(公告)号：US20140191894A1
公开(公告)日：2014-07-10
申请号：US13869451
申请日：2013-04-24
申请人： NATIONAL CENTRAL UNIVERSITY
发明人： Liang-Chien Chen , Chin-Jung Yang
IPC分类号： G01S13/86
CPC分类号： G01S13/86 , B64G2001/1028 , B64G2001/1035 , G01C21/005 , G01S13/867 , G01S13/90 , G06T7/55 , G06T2207/10036 , G06T2207/10044
摘要： A three-dimensional positioning method includes establishing the geometric model of optical and radar sensors, obtaining rational function conversion coefficient, refining the rational function model and positioning the three-dimensional coordinates. Most of the radar satellite companies and part of the optical satellite only provide satellite ephemeris data, rather than the rational function model. Therefore, it is necessary to obtain the rational polynomial coefficients from the geometric model of optical and radar sensors; followed by refining the rational function model by the ground control points, so that object image space intersection is more serious; and then followed by measuring the conjugate point on the optical and radar images. Finally, the observation equation is established by the rational function model to solve the three-dimensional coordinates. It is obvious from the above results that the integration of optical and radar images does achieve the three-dimensional positioning.
摘要翻译：三维定位方法包括建立光学和雷达传感器的几何模型，获得合理的函数转换系数，提炼合理的函数模型和定位三维坐标。大多数雷达卫星公司和部分光卫星只提供卫星星历数据，而不是合理的功能模型。因此，有必要从光学和雷达传感器的几何模型中获得有理多项式系数; 然后通过地面控制点对理性函数模型进行优化，使对象图像空间交叉点更加严格; 然后测量光学和雷达图像上的共轭点。最后，通过理性函数模型建立观测方程来求解三维坐标。从上述结果可以看出，光学和雷达图像的集成确实实现了三维定位。

7. 发明申请

WO2014097263A1 INNOVATIVE ORBIT DESIGN FOR EARTH OBSERVATION SPACE MISSIONS 审中-公开
标题翻译：用于地球观测空间任务的创新轨道设计
公开(公告)号：WO2014097263A1
公开(公告)日：2014-06-26
申请号：PCT/IB2013/061226
申请日：2013-12-20
申请人： THALES ALENIA SPACE ITALIA S.P.A. CON UNICO SOCIO
发明人： DI GIORGIO, Fabio , FRANCIONI, Andrea , CRICENTI, Alessandro
IPC分类号： B64G1/10 , B64G1/24 , G01S13/90
CPC分类号： G01S13/9023 , B64G1/1021 , B64G1/242 , B64G1/405 , B64G2001/1035 , G01S13/90 , G06F17/10
摘要： The invention concerns a method for reducing the costs of a satellite remote sensing service. Said method comprises providing a satellite remote sensing system (1) that includes only one satellite (11) equipped with a sensor (111) configured to acquire images of areas o;f the Earth's surface, said satellite remote sensing system (1) being designed to provide a satellite remote sensing service based on the images acquired by the sensor (111) on board the satellite (11). In particular, the satellite (11) follows a predefined orbit around the Earth with an orbit repeat cycle shorter than three days whereby a satellite remote sensing service with very good time performances and excellent interferometric capabilities and with drastically reduced costs is obtained.
摘要翻译：本发明涉及降低卫星遥感业务成本的方法。所述方法包括提供卫星遥感系统（1），其仅包括配备有传感器（111）的一个卫星（11），所述传感器被配置为获取地球表面上的区域的图像，所述卫星遥感系统（1）被设计基于由卫星（11）上的传感器（111）获取的图像来提供卫星遥感服务。特别地，卫星（11）遵循围绕地球的预定义轨道，轨道重复循环短于三天，由此获得具有非常好的时间性能和优异的干涉能力并且显着降低成本的卫星遥感服务。

8. 发明申请

US20180246202A1 RADAR SATELLITE AND RADAR SATELLITE SYSTEM USING RADAR SATELLITE 审中-公开
公开(公告)号：US20180246202A1
公开(公告)日：2018-08-30
申请号：US15527042
申请日：2015-11-09
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA
发明人： Toyotoshi KUROSE
IPC分类号： G01S13/90 , B64G1/22 , B64G1/26 , B64G1/44 , B64G1/10 , G01S7/00 , G01S7/28
CPC分类号： G01S13/90 , B64G1/1014 , B64G1/222 , B64G1/26 , B64G1/443 , B64G1/648 , B64G2001/1035 , G01S7/003 , G01S7/02 , G01S7/03 , G01S7/28 , G01S13/89
摘要： A radar satellite of the present invention comprises a radar unit including a plurality of radar panels coupled to each other in a single flat plate shape, each of the plurality of radar panels including a plurality of antennas which transmit and receive radar waves, and a solar cell; and a communication/control unit which performs communications with a spot on an earth or a spacecraft. The radar unit includes: a radar panel array which is a plate-shaped structure including the plurality of radar panels; and a deployable truss structure including a plurality of side frame members supporting the plurality of radar panels, respectively, and coupled to each other in such a manner that the side frame members are foldable and deployable.

9. 发明授权

US09977125B2 Innovative orbit design for earth observation space missions 有权
公开(公告)号：US09977125B2
公开(公告)日：2018-05-22
申请号：US14653535
申请日：2013-12-20
申请人： Thales Alenia Space Italia S.p.A. Con Unico Socio
发明人： Fabio Di Giorgio , Andrea Francioni , Alessandro Cricenti
IPC分类号： G01S13/90 , G06F17/10 , B64G1/40 , B64G1/10 , B64G1/24
CPC分类号： G01S13/9023 , B64G1/1021 , B64G1/242 , B64G1/405 , B64G2001/1035 , G01S13/90 , G06F17/10
摘要： The invention concerns a method for reducing the costs of a satellite remote sensing service. The method comprises providing a satellite remote sensing system that includes only one satellite equipped with a sensor configured to acquire images of areas of the earth's surface, the satellite remote sensing system being designed to provide a satellite remote sensing service based on the images acquired by the sensor on board the satellite. In particular, the satellite follows a predefined orbit around the earth with an orbit repeat cycle shorter than three days, whereby a satellite remote sensing service with very good time performance, excellent interferometric capabilities and with drastically reduced costs is obtained.

10. 发明申请

US20160205356A1 Remote Reconnaissance For Space Exploration 审中-公开
标题翻译：空间探测远程侦察
公开(公告)号：US20160205356A1
公开(公告)日：2016-07-14
申请号：US14594128
申请日：2015-01-11
申请人： Kenneth Dean Stephens, JR.
发明人： Kenneth Dean Stephens, JR.
IPC分类号： H04N7/18 , H04N5/232
CPC分类号： G01C11/00 , B64C2201/127 , B64G2001/1035 , B64G2700/00 , H04N5/23203 , H04N5/247 , H04N7/183
摘要： A system of reconnaissance for the staging of a mission in a target area of a remote location in space is disclosed, including satellite surveillance means; a plurality of radio beacon/video camera transceiver means; communication means connecting the satellite surveillance means with the plurality of radio beacon/video camera transceiver means; communication means connecting the plurality of radio beacon/video camera transceiver means with at least one base station; and analysis means to analyze video, positional and other data from the target area.
摘要翻译：披露了一个在空间遥远的目标地区进行任务侦察的系统，包括卫星监视装置; 多个无线电信标/摄像机收发器装置; 通信装置将卫星监视装置与多个无线电信标/摄像机收发装置连接起来; 通信装置将多个无线电信标/摄像机收发信机装置与至少一个基站连接; 和分析手段来分析来自目标区域的视频，位置和其他数据。

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