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21. 发明专利

JPWO2016059835A1 情報処理装置、情報処理方法およびプログラム审中-公开
公开(公告)号：JPWO2016059835A1
公开(公告)日：2017-08-03
申请号：JP2016553985
申请日：2015-06-30
申请人：ソニー株式会社
发明人：忠邦奈良部 , 忠邦奈良部
IPC分类号： H04N5/232 , B64B1/02 , B64D47/08 , G03B15/00 , G03B17/56 , H04N5/91 , H04N5/915
CPC分类号： G01W1/08 , A63H2027/1066 , B64B1/26 , B64B1/58 , B64D47/08 , G03B15/006 , G03B37/00 , G05D1/0094 , G05D1/102 , G05D1/105 , H04N5/2257 , H04N2005/2255
摘要：面白味のある画像を記録する。情報処理装置は、撮像部および制御部を具備する情報処理装置である。この撮像部は、空気よりも軽い気体を利用して空中を移動する飛行体に設置され、被写体を撮像して画像データを生成するものである。また、制御部は、飛行体に関する情報および飛行体の周囲の情報のうちの少なくとも1つの情報に基づいて、飛行体の移動を制御するとともに、撮像部により生成された画像データを記録する制御を行うものである。

22. 发明专利

JP2013169972A Unmanned aerial vehicle 有权
标题翻译：无人驾驶的航空机
公开(公告)号：JP2013169972A
公开(公告)日：2013-09-02
申请号：JP2013028377
申请日：2013-02-15
申请人： Boeing Co:The , ザ・ボーイング・カンパニーThe Boeing Company
发明人： CRIADO ALFREDO
IPC分类号： B64C31/024 , B64C39/02 , B64D27/24 , B64D41/00 , B64D45/00
CPC分类号： B64C19/00 , B64C31/02 , B64C31/024 , B64C39/024 , B64C2201/021 , B64C2201/042 , G05D1/0005 , G05D1/105 , Y02T50/53
摘要： PROBLEM TO BE SOLVED: To provide an unmanned aerial vehicle (UAV) capable of obtaining energy from an ascending air current and an operation method of the unmanned aerial vehicle.SOLUTION: An unmanned aerial vehicle having a gliding capability is provided which includes a power generator 140 driven by a rotary wing 190 and a battery 200. This unmanned aerial vehicle can operate in an energy obtaining mode where the rotary wing 190 is driven and rotated by movement of the unmanned aerial vehicle and the rotary wing 190 drives the power generator 140; and the power generator 140 charges the battery 200; in this energy obtaining mode, thanks to regenerative braking of the power generator 140, a forward speed of the unmanned aerial vehicle declines to generate electricity, and the unmanned aerial vehicle is prevented from flying exceeding a predetermined altitude.
摘要翻译：要解决的问题：提供能够从上升气流获得能量的无人机（UAV）和无人驾驶飞行器的操作方法。解决方案：提供具有滑行能力的无人机，其包括发电机该无人驾驶飞行器可以以能量获取模式操作，其中旋转翼190通过无人驾驶飞行器的移动而被驱动和旋转，旋转翼190驱动发电机140; 并且发电机140对电池200充电; 在该能量获取模式中，由于发电机140的再生制动，无人驾驶飞行器的前进速度下降以发电，并且防止无人驾驶飞行器超过预定高度。

23. 发明公开

KR1020100058052A 일반폭탄 비행보조체의 비행조종장치 및 방법 有权
标题翻译：用于控制用于通用燃料的飞行支持装置的飞行器的装置和方法
公开(公告)号：KR1020100058052A
公开(公告)日：2010-06-03
申请号：KR1020080116721
申请日：2008-11-24
申请人： 국방과학연구소
发明人： 윤형식 , 이광현 , 이은용
IPC分类号： F42B15/01 , G05D1/00
CPC分类号： F42B10/60 , B64C2201/121 , G05D1/105
摘要： PURPOSE: A flight control apparatus of a flight assist device for general purpose bombs is provided to improve the accuracy of bomb-dropping by guiding general purpose bombs to a target using a guidance and control program of a flight control computer without an aviator's command. CONSTITUTION: A flight control apparatus of a flight assist device for general bombs comprises an inertia detector(202), a navigation module(203), a bomb drop sensor(204), an unfolded wing sensor(205), and a flight control computer(206). The inertia detector detects the speed and the acceleration of a general purpose bomb. The navigation module provides information for the guidance operation of the general purpose bomb using signals from the inertia detector and a GPS(Global Positioning System). The bomb drop sensor senses the dropping of the general purpose bomb and transmits sensing signals. The unfolded wing sensor senses the unfolding of the left and right main wings of the flight assist device and transmits the sensing signals. The flight control computer receives the sensing signals and generates the operation command of a flaperon actuator(207).
摘要翻译：目的：提供用于通用炸弹的飞行辅助装置的飞行控制装置，以通过使用没有飞行员指令的飞行控制计算机的引导和控制程序将通用炸弹引导到目标来提高炸弹的准确性。构成：用于一般炸弹的飞行辅助装置的飞行控制装置包括惯性检测器（202），导航模块（203），炸弹落下传感器（204），未折叠翼传感器（205）和飞行控制计算机（206）。惯性检测器检测通用炸弹的速度和加速度。导航模块使用来自惯性检测器和GPS（全球定位系统）的信号提供用于通用炸弹导向操作的信息。炸弹传感器检测到通用炸弹的落下并传输感应信号。展开的机翼传感器感测飞行辅助装置的左右主翼的展开并传送感测信号。飞行控制计算机接收感测信号并产生襟副翼致动器（207）的操作命令。

24. 发明公开

KR1020130095167A 무인 항공기 审中-实审
标题翻译：不定期的空中客车
公开(公告)号：KR1020130095167A
公开(公告)日：2013-08-27
申请号：KR1020120142813
申请日：2012-12-10
申请人： 더 보잉 컴파니
发明人： 알프레도크리아두
IPC分类号： G05D1/10
CPC分类号： B64C19/00 , B64C31/02 , B64C31/024 , B64C39/024 , B64C2201/021 , B64C2201/042 , G05D1/0005 , G05D1/105 , Y02T50/53
摘要： PURPOSE: An unmanned aerial vehicle (UAV) is provided to control the rotation speed of a rotor during a flying operation by controlling a bank angle, thereby easily controlling the lift force and the advance speed. CONSTITUTION: A motor/generator (140) is arranged to be driven by a rotor (190). The motor/generator charges a battery (200) by supplying power to the battery. The rotor is driven to rotate by the relative flow of air passing by a UAV (10). A flight management system (210) includes a speed controller and aircraft sensors (160). The aircraft sensors are arranged to measure the total sum of the kinetic energy and potential. [Reference numerals] (140) Motor/generator; (160) Aircraft sensors; (200) Battery; (210) Flight managing system
摘要翻译：目的：提供无人飞行器（UAV），通过控制倾斜角度来控制飞行操作期间转子的转速，从而容易地控制升力和提前速度。构成：电动机/发电机（140）布置成由转子（190）驱动。电机/发电机通过向电池供电来对电池（200）充电。转子通过无人机（10）通过的空气的相对流动被驱动旋转。飞行管理系统（210）包括速度控制器和飞行器传感器（160）。飞机传感器布置成测量动能和潜力的总和。（附图标记）（140）电动机/发电机; （160）飞机传感器; （200）电池; （210）飞行管理系统

25. 发明公开

EP3355151A1 METHODS AND APPARATUS FOR DYNAMICALLY UPDATING DROP ZONE DATA DURING FLIGHT 有权
公开(公告)号：EP3355151A1
公开(公告)日：2018-08-01
申请号：EP18153261.5
申请日：2018-01-24
申请人： Honeywell International Inc.
发明人： P R, Sriram , LETSU-DAKE, Emmanuel
IPC分类号： G05D1/10 , B64D1/02 , B64D1/08 , G08G5/00
CPC分类号： G06F3/04847 , B64D1/02 , B64D1/08 , B64D43/00 , G05D1/105 , G08G5/0021 , G08G5/0039 , G08G5/0052 , G08G5/0091
摘要： A method for computing drop zone data onboard an aircraft is provided. The method obtains, by a processor, current drop zone parameters for an air drop, during flight of the aircraft; receives, by the processor, changes to dynamic conditions associated with operation of the aircraft, wherein the dynamic conditions comprise at least one of wind speed, drop altitude, current temperature, angle of approach, aircraft speed, and number of stages of planned drop; calculates, by the processor, updated drop zone parameters, based on the current drop zone parameters and the changes to the dynamic conditions; and presents the updated drop zone parameters, via a display device.

26. 发明公开

EP3344545A1 A VEHICLE COMPRISING AN ENGINE RESTART SYSTEM 有权
公开(公告)号：EP3344545A1
公开(公告)日：2018-07-11
申请号：EP16760141.8
申请日：2016-08-26
申请人： BAE SYSTEMS plc
发明人： WOODHOUSE, Gordon, Charles , BOSTON, Luke, Michael
IPC分类号： B64D31/06 , B64D45/04 , G05D1/10
CPC分类号： B64D31/06 , B64C39/024 , B64C2201/141 , B64D41/00 , B64D45/04 , B64D2041/005 , B64D2045/0085 , G05D1/0088 , G05D1/105 , G07C5/0808 , Y02T50/54
摘要： A vehicle (100) comprising: an engine (102); a system for starting the engine (102); a fault detection module (120); an electrical power source (110); and a controller (116, 122). The controller (116, 122) is configured to, responsive to the fault detection module (120) detecting a fault occurring with the engine (102): determine a window in which to attempt to start the engine (102); control the electrical power source (110) to provide electrical power to the system for starting the engine (102); and control the system for starting the engine (102) to attempt to start the engine (102) using the supplied electrical power only during the determined window.

27. 发明公开

EP2873166A1 GEO-FENCING 有权
标题翻译：地理围栏
公开(公告)号：EP2873166A1
公开(公告)日：2015-05-20
申请号：EP13816293.8
申请日：2013-05-09
申请人： Google Inc.
发明人： TELLER, Eric , DEVAUL, Richard, Wayne , WEAVER, Joshua , BIFFLE, Clifford, L. , RHODES, Bradley , STAAF, Anton
IPC分类号： H04B7/185 , H04W4/00
CPC分类号： B64B1/40 , B64B1/62 , B64D1/02 , G05D1/105 , H04B10/1129 , H04W84/02
摘要： A balloon includes a cut-down device, a payload, and an envelope. A control system could be configured to determine a position of the balloon with respect to a predetermined zone. The cut-down device could be operable to cause at least the payload to land in response to determining that the position of the balloon is within the predetermined zone. The predetermined zone includes an exclusion zone and a shadow zone. The shadow zone could include locations from which the balloon would be likely to drift into the exclusion zone based on, e.g., historic weather patterns or expected environmental conditions. Boundaries of the shadow zone could be determined based on, for example, a probability of the balloon entering the exclusion zone.

28. 发明授权

EP1510455B1 Procédé et dispositif pour contrôler l'assiette d'un avion 有权
标题翻译：一种用于飞行器的纵倾角调节方法和装置
公开(公告)号：EP1510455B1
公开(公告)日：2006-03-15
申请号：EP04291583.5
申请日：2004-06-23
申请人： AIRBUS France
发明人： Chardon, Stéphane , Sabathier, Jean-Philippe
IPC分类号： B64D1/02 , B64C13/00
CPC分类号： G05D1/105 , B64C13/00 , B64D1/02 , G05D1/0816

29. 发明公开

EP1462898A3 Waypoint navigation 有权
标题翻译：在基于路标导航
公开(公告)号：EP1462898A3
公开(公告)日：2006-01-04
申请号：EP03445131.0
申请日：2003-11-18
申请人： SAAB AB
发明人： Carlsson, Carl-Olof , Adebjörk, Peter
IPC分类号： G05D1/02 , G05D1/00 , B64C39/02
CPC分类号： G05D1/105 , G05D1/0022 , G05D1/0202
摘要： The invention relates to remote control of an unmanned aerial vehicle, UAV, (100) from a control station (110) by means of a wireless command link (115). The UAV (100) may be controlled in an autonomous mode wherein it flies according to a primary route (R1, R1') defined by a first set of predefined waypoints (WP1-WP8, IP). The UAV (100) may also be controlled in a manual mode wherein it flies according to an alternative primary route (R1') defined in real-time by control commands received via the wireless command link (115). Flight control parameters are monitored in both modes, and in case a major alarm condition occurs, the UAV (100) is controlled to follow an emergency route (R2') defined by a second set of predefined waypoints (HP1-HP7, TP1-TP9, IP). Particularly, a major alarm condition is activated if an engine failure is detected. Then, the emergency route (R2') involves flying the UAV (100) to an air space above a termination waypoint (TP9) on the ground at which it is estimated that the vehicle's (100) flight may be ended without injuring any personnel or causing uncontrolled material damages.

30. 发明公开

EP1004952A2 Automatic guidance system for flight vehicle having parafoil and navigation guidance apparatus for the system 有权
标题翻译：对于滑翔伞及导航装置的导弹这样的自动化控制系统
公开(公告)号：EP1004952A2
公开(公告)日：2000-05-31
申请号：EP99123182.0
申请日：1999-11-24
申请人： FUJI JUKOGYO KABUSHIKI KAISHA
发明人： Yoneda, Hiroshi , Amito, Atushi
IPC分类号： G05D1/10
CPC分类号： G05D1/105
摘要： An automatic guidance system guides a flight vehicle having a parafoil to a target grounding point. The system opens the parafoil of the flight vehicle dropped in a predetermined area above the target grounding point. The system estimates wind velocity and wind direction after the parafoil of the flight vehicle is opened. Then, the system determines the landing flight path of the flight vehicle based on the estimated wind velocity and wind direction, guides the flight of the flight vehicle to the determined landing flight path and descends the flight vehicle according to the landing flight path.
摘要翻译：一种自动导向系统引导具有翼伞到目标接地点飞行车辆。系统打开飞行器的翼伞目标接地点上方的预定面积锐减。飞行器的翼伞被打开后的系统估计风速和风向。然后，系统确定的地雷基于所估计的风速和风向的飞行器的着陆飞行路径，引导飞行器到确定性开采着陆飞行路径飞行和下降飞行车辆雅丁到着陆飞行路径。

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