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1. 发明申请

US20170326730A1 APPARATUS AND METHOD FOR CONTROLLING MOVING OBJECT, AND COMPUTER-READABLE RECORDING MEDIUM IN WHICH PROGRAM FOR IMPLEMENTING METHOD IN COMPUTER IS RECORDED 审中-公开
公开(公告)号：US20170326730A1
公开(公告)日：2017-11-16
申请号：US15535299
申请日：2015-12-09
申请人： KOREA AEROSPACE RESEARCH INSTITUTE
发明人： Jae Wook KWON , Dong Hun LEE , Hyo Choong BANG
IPC分类号： B25J9/16
CPC分类号： B25J9/1664 , B25J9/1653 , B64G1/242 , B64G2001/1071 , G05D1/10
摘要： According to an embodiment of the present invention, an apparatus for controlling a moving object includes a trajectory control unit configured to control a trajectory of the moving object and a position control unit configured to control a position of the moving object. Thus, it is possible to control an angle at which the moving object enters a target point.

2. 发明授权

US09290279B2 Landing system for a body and space probe provided with such a system 有权
标题翻译：具有这种系统的身体和空间探测器的着陆系统
公开(公告)号：US09290279B2
公开(公告)日：2016-03-22
申请号：US13376231
申请日：2010-05-28
申请人： Christophe Balemboy , Mark Kinnersley , Robert Andre Laine , Xavier Sembely
发明人： Christophe Balemboy , Mark Kinnersley , Robert Andre Laine , Xavier Sembely
IPC分类号： B64G1/62 , B64G1/10
CPC分类号： B64G1/62 , B64G2001/1071
摘要： A landing system of a body and a space probe provided with such a system for landing on a bearing ground. The landing system includes landing legs (5), each with a footpad (6) at the end thereof, intended for braking the landing impact of the body when coming into contact with the ground and for supporting the body on the ground after landing. The footpads (6) are not coplanar.
摘要翻译：身体的一个着陆系统和一个设有这样一个系统的空间探针，用于在轴承地面上着陆。着陆系统包括着陆腿（5），每个脚蹬在其末端具有足垫（6），用于在与地面接触时制动身体的着陆冲击，并在着陆后将身体支撑在地面上。脚垫（6）不共面。

3. 发明授权

US09001313B2 Laser radar device, safe landing sensor for planetfall, docking sensor for space apparatus, space debris collection sensor, and vehicle-mounted collision avoidance sensor 有权
标题翻译：激光雷达装置，行星落地安全着陆传感器，空间装置对接传感器，空间碎片采集传感器和车载碰撞避免传感器
公开(公告)号：US09001313B2
公开(公告)日：2015-04-07
申请号：US14236792
申请日：2011-11-15
申请人： Shumpei Kameyama , Masaharu Imaki , Nobuki Kotake , Hidenobu Tsuji , Hideaki Ochimizu , Mikio Takabayashi , Yoshihito Hirano
发明人： Shumpei Kameyama , Masaharu Imaki , Nobuki Kotake , Hidenobu Tsuji , Hideaki Ochimizu , Mikio Takabayashi , Yoshihito Hirano
IPC分类号： G01S17/02 , B64G1/64 , B64G1/66 , G01S17/88 , G01S17/89 , G01S7/48 , G01S17/10 , G01B11/24 , G01S17/93 , G01S7/481
CPC分类号： G01S17/02 , B64G1/62 , B64G1/64 , B64G1/646 , B64G1/66 , B64G2001/1071 , G01B11/24 , G01S7/48 , G01S7/481 , G01S17/10 , G01S17/88 , G01S17/89 , G01S17/933 , G01S17/936
摘要： A laser radar device includes: a pulse laser that outputs transmission light to a target; an transmission optical system that makes the transmission light at a predetermined beam spread angle; a light-receiving element array that receives scattered light from the target and converts the light to an electric signal; an electric circuit array that detects a reception intensity and a reception time from the electric signal; a range/three-dimensional shape output unit that measures a range to the target or a three-dimensional shape of the target on the basis of the reception time; a determination unit that determines whether the beam spread angle is changed or not on the basis of the reception intensity and the reception time; and a control unit that changes the beam spread angle on the basis of a determination result.
摘要翻译：激光雷达装置包括：将传输光输出到目标的脉冲激光器; 使透射光成为规定的光束扩展角的透射光学系统; 光接收元件阵列，其接收来自所述目标物的散射光并将所述光转换成电信号; 从电信号检测接收强度和接收时间的电路阵列; 范围/三维形状输出单元，其基于接收时间测量目标的范围或目标的三维形状; 确定单元，其基于接收强度和接收时间来确定波束扩展角是否改变; 以及控制单元，其基于确定结果改变光束扩展角。

4. 发明授权

US08413927B2 Landing gear for spacecraft 有权
标题翻译：飞船起落架
公开(公告)号：US08413927B2
公开(公告)日：2013-04-09
申请号：US12983360
申请日：2011-01-03
申请人： Robert Buchwald , Erich Werth
发明人： Robert Buchwald , Erich Werth
IPC分类号： B64C25/32 , B64C25/00
CPC分类号： B64G1/62 , B64G2001/1071
摘要： A pivotal connection and a substantially rigid yet disruptable mechanical connection mount a respective foot pad on a distal end of each one of plural landing legs of a lander spacecraft. The mechanical connection includes at least one predetermined rated breaking point designed to break when the foot pad makes contact with a landing ground surface. At least two sensor elements, preferably electrical conductors or switches, are incorporated in the mechanical connection(s) of one or more foot pads. When the foot pad makes ground contact, the mechanical connection breaks at the rated breaking point(s), which also disrupts or actuates the sensor element(s), which thus provides a signal to an evaluating unit, which triggers the shut-down of at least one braking retrorocket or retrothruster.
摘要翻译：枢转连接和基本上刚性但可破坏的机械连接件在着陆器航天器的多个着陆腿的每一个的远端上安装相应的脚垫。机械连接包括至少一个预定的额定断裂点，设计成当脚垫与着陆地面接触时断裂。至少两个传感器元件，优选地电导体或开关，被并入一个或多个脚垫的机械连接中。当脚垫接地时，机械连接在额定断裂点处断裂，这也破坏或致动传感器元件，从而向评估单元提供信号，从而触发关闭至少一个制动回路或后推力器。

5. 发明授权

US08353481B2 Spin-stabilized lander 失效
标题翻译：旋转稳定着陆机
公开(公告)号：US08353481B2
公开(公告)日：2013-01-15
申请号：US12359303
申请日：2009-01-24
申请人： Harold Rosen
发明人： Harold Rosen
IPC分类号： B64G1/28
CPC分类号： B64G1/62 , B33Y80/00 , B64G1/16 , B64G1/242 , B64G1/281 , B64G1/401 , B64G1/402 , B64G1/404 , B64G1/646 , B64G1/66 , B64G2001/1064 , B64G2001/1071
摘要： The invention provides a novel, low-cost, spin-stabilized lander architecture capable (with appropriate system scaling tailored to the attributes of the target) of performing a soft-landing on a solar-system body such as Earth's Moon, Mars, Venus, the moons of Mars, Jupiter, Saturn, Uranus and Neptune, selected near-Earth and main-belt asteroids, comets and Kuiper belt objects and even large human-made objects, and also moving about on the surface of the target solar-system body after the initial landing in movement akin to hopping.
摘要翻译：本发明提供了一种新颖的，低成本的自旋稳定着陆器架构，其能够（在适合于目标的属性的适当的系统缩放）上执行在诸如地球月球，火星，金星等太阳系体上的软着陆，火星，木星，土星，天王星和海王星的卫星，选择了近地和主带小行星，彗星和Kuiper皮带物体，甚至大型人造物体，还在目标太阳系体内表面移动在运动中初始着陆类似于跳跃。

6. 发明申请

US20110163201A1 Landing Gear for Spacecraft 有权
标题翻译：航天器起落架
公开(公告)号：US20110163201A1
公开(公告)日：2011-07-07
申请号：US12983360
申请日：2011-01-03
申请人： Robert BUCHWALD , Erich WERTH
发明人： Robert BUCHWALD , Erich WERTH
IPC分类号： B64C25/02 , B64C25/32 , B64G99/00
CPC分类号： B64G1/62 , B64G2001/1071
摘要： A pivotal connection and a substantially rigid yet disruptable mechanical connection mount a respective foot pad on a distal end of each one of plural landing legs of a lander spacecraft. The mechanical connection includes at least one predetermined rated breaking point designed to break when the foot pad makes contact with a landing ground surface. At least two sensor elements, preferably electrical conductors or switches, are incorporated in the mechanical connection(s) of one or more foot pads. When the foot pad makes ground contact, the mechanical connection breaks at the rated breaking point(s), which also disrupts or actuates the sensor element(s), which thus provides a signal to an evaluating unit, which triggers the shut-down of at least one braking retrorocket or retrothruster.
摘要翻译：枢转连接和基本上刚性但可破坏的机械连接件在着陆器航天器的多个着陆腿的每一个的远端上安装相应的脚垫。机械连接包括至少一个预定的额定断裂点，设计成当脚垫与着陆地面接触时断裂。至少两个传感器元件，优选地电导体或开关，被并入一个或多个脚垫的机械连接中。当脚垫接地时，机械连接在额定断裂点处断裂，这也破坏或致动传感器元件，从而向评估单元提供信号，从而触发关闭至少一个制动回路或后推力器。

7. 发明申请

US20070200033A1 Method for assemblying and landing a habitable structure on an extraterrestrial body 有权
标题翻译：在居民身体上装配和着陆可居住的结构的方法
公开(公告)号：US20070200033A1
公开(公告)日：2007-08-30
申请号：US11363346
申请日：2006-02-28
申请人： Robert Bigelow
发明人： Robert Bigelow
IPC分类号： B64G1/12
CPC分类号： B64G1/12 , B64G1/62 , B64G9/00 , B64G2001/1071 , B64G2001/1092 , B64G2001/224
摘要： A method for assembling and landing a habitable module on an extraterrestrial mass is claimed. At least one inflatable module and a second module are placed into orbit about an extraterrestrial mass. Connecting nodes, propulsion busses, and landing pads are also placed into orbit. A habitable structure is constructed from the modules, busses, pads, and nodes. The structure can be robotically constructed. The habitable structure is then landed onto the surface of the extraterrestrial mass. The landing can be remotely controlled and the modules can be non-occupied.
摘要翻译：要求一种用于组装和着陆在地球上的居住模块的方法。至少一个充气模块和第二模块被放置在绕地球外围的轨道上进行轨道运动。连接节点，推进总线和着陆垫也被放置在轨道上。由模块，总线，焊盘和节点构成可居住的结构。该结构可以机器人构造。然后将可居住的结构降落到地球外表面上。可以远程控制着陆，并且模块可以不被占用。

8. 发明授权

US5397082A Space transport architecture and method for robotic planetary operations 失效
标题翻译：机器人行星运行的空间运输结构和方法
公开(公告)号：US5397082A
公开(公告)日：1995-03-14
申请号：US6920
申请日：1993-03-16
申请人： David R. Scott
发明人： David R. Scott
IPC分类号： B64G1/00 , B64G1/10 , B64G1/24
CPC分类号： B64G1/105 , B64G1/002 , B64G1/1085 , B64G1/242 , B64G2001/1064 , B64G2001/1071 , B64G2001/247
摘要： A space transport architecture (STA) for robotic operations on a planet. The STA comprises and an earth launch vehicle (ELV) (10), adapted to carry a space transfer vehicle (STV) (15) and associated payloads (17) into low earth orbit (LEO). The space transfer vehicle (STV) (15), carried by the ELV (10), is adapted to carry associated payloads from LEO in the planetary orbit and to dispense these payloads (17) from planetary orbit for landing in the locus of at least one planetary exploration site. At least one planetary lander (17) is carried by the STV. The lander (17) is adapted to carry a plurality of robotic operational platforms (58) and deploy these platforms in the locus of the exploration site. A plurality of robotic operational platforms (58) is carried by each of the landers (17).
摘要翻译：用于在地球上进行机器人操作的空间运输结构（STA）。 STA包括适于将空间传输车辆（STV）（15）和相关联的有效载荷（17）运送到低地球轨道（LEO）中的地球运载火箭（10V）（10）。由ELV（10）携带的空间传输车辆（STV）（15）适于承载来自行星轨道的LEO的相关有效载荷，并将这些有效载荷（17）从行星轨道分配至少至少在一个行星探测点。至少有一个行星落地机（17）由STV承载。着陆器（17）适于携带多个机器人操作平台（58），并将这些平台部署在勘探现场的轨迹上。每个着陆器（17）承载多个机器人操作平台（58）。

9. 发明申请

US20190248517A1 EXPLORATION METHOD, EXPLORATION SYSTEM, PROBE, HYDROGEN SUPPLY METHOD, AND IMAGE PROCESSING METHOD 审中-公开
公开(公告)号：US20190248517A1
公开(公告)日：2019-08-15
申请号：US16324537
申请日：2016-08-08
申请人： ispace, inc.
发明人： Takeshi HAKAMADA , Takahiro NAKAMURA , John WALKER , Toshiro SHIMIZU , Toshiki TANAKA , Daisuke FURUTOMO , Yu KUDO , Kiyona MIYAMOTO , Daishi MATSUKURA , Mohamed RAGAB , Abdelkader HAOUCHINE , Damien HAIKAL , Chit Hong YAM , Julian Jakub GRAMATYKA
IPC分类号： B64G5/00 , B64G1/16 , B64G1/10 , B64G1/44 , B64G1/42 , B64G1/66 , B64G3/00 , C25B1/04 , H04N5/265
CPC分类号： B64G5/00 , B64G1/105 , B64G1/1085 , B64G1/16 , B64G1/421 , B64G1/443 , B64G1/66 , B64G3/00 , B64G2001/1071 , C25B1/04 , E21C51/00 , H04N5/2253 , H04N5/265
摘要： An exploration method includes: a step of exploring a natural resource on a satellite, a minor planet, or a planet; a step of acquiring the natural resource detected by the exploration; and a step of storing the acquired natural resource.

10. 发明授权

US09302791B2 Transport landing vehicle 有权
标题翻译：运输着陆车
公开(公告)号：US09302791B2
公开(公告)日：2016-04-05
申请号：US14121596
申请日：2014-09-22
申请人： Bigelow Aerospace LLC
发明人： Robert T. Bigelow
IPC分类号： B64G1/26 , B64G1/60 , B64G1/12 , B64G1/40 , B64G1/10
CPC分类号： B64G1/26 , B64G1/12 , B64G1/402 , B64G1/60 , B64G2001/1071
摘要： A transport landing vehicle for transferring an astronaut to and from an extraterrestrial mass such as a moon, asteroid, or small planet is disclosed. The transport landing vehicle has a cage that is substantially open to the outside environment.
摘要翻译：公开了用于将宇航员转移到诸如月球，小行星或小行星的地球外物质的运输着陆车辆。运输着陆车具有基本上对外部环境开放的保持架。

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