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    BATTERY MANAGEMENT SYSTEM
    71.
    发明公开
    BATTERY MANAGEMENT SYSTEM 审中-公开
    BATTERIEVERWALTUNGSSYSTEM

    公开(公告)号：EP3138172A1

    公开(公告)日：2017-03-08

    申请号：EP14908164.8

    申请日：2014-12-17

    Applicant: SZ DJI Technology Co., Ltd.

    Inventor： ZHAO, Tao ,  ZHAN, Juncheng ,  LIU, Yuancai ,  WANG, Lei ,  WANG, Wentao

    IPC: H02H7/18 ,  H02J7/00

    CPC classification number: H02J7/0063 ,  B64C39/024 ,  B64C2201/00 ,  H01M10/44 ,  H01M10/48 ,  H01M2220/20 ,  H02H7/18 ,  H02J7/0029 ,  H02J7/007 ,  H02J2007/0067

    Abstract: Systems, methods, and devices of managing a battery assembly used to power an object are provided to discharge a battery assembly for a safe and long-term storage. A controlled self-discharge of the battery assembly may be initiated when the power to the object is turned off for a certain length of time or the battery assembly is not in use for a threshold length of time. The controlled self-discharge may be terminated if the battery assembly reaches a threshold voltage value or the battery is in use again during the self-discharge.

    Abstract translation: 提供管理用于为物体供电的电池组件的系统，方法和装置，用于对电池组件进行放电以进行安全和长期存储。 当对象的电源关闭一段时间或电池组件在阈值时间长度不使用时，电池组件的受控自放电可以开始。 如果电池组件达到阈值电压值或者在自放电期间电池再次使用，则控制的自放电可以终止。

    IMPACT ABSORPTION APPARATUS FOR UNMANNED AERIAL VEHICLE
    72.
    发明公开
    IMPACT ABSORPTION APPARATUS FOR UNMANNED AERIAL VEHICLE 审中-公开
    STOSSDÄFFENDEVORRICHTUNGFÜREIN UNBEMANNTES LUFTFAHRZEUG

    公开(公告)号：EP3093239A1

    公开(公告)日：2016-11-16

    申请号：EP16159247.2

    申请日：2016-03-08

    Applicant: Disney Enterprises, Inc.

    Inventor： WONG, Clifford

    IPC: B64C39/00

    CPC classification number: B64D25/00 ,  B64C39/00 ,  B64C39/024 ,  B64C2201/00 ,  B64C2201/024 ,  B64C2201/14 ,  B64C2201/146 ,  B64C2201/18 ,  B64C2201/185

    Abstract: An unmanned aerial vehicle apparatus comprises a frame. Further, the unmanned aerial vehicle apparatus comprises a propulsion mechanism coupled to the frame that propels the frame through the air. In addition, the unmanned aerial vehicle apparatus comprises a storage device that stores one or more airbags and is coupled to the frame. The unmanned aerial vehicle apparatus also comprises an inflation device coupled to the frame that receives an activation signal and inflates the one or more airbags based upon receipt of the activation signal to deploy the one or more airbags from the storage device prior to an impact of the frame with an object.

    Abstract translation: 无人驾驶飞行器装置包括一个框架。 此外，无人驾驶飞行器装置包括联接到框架的推进机构，其推动框架通过空气。 此外，无人驾驶飞行器装置包括存储一个或多个安全气囊并连接到该框架的存储装置。 无人驾驶飞行器装置还包括耦合到框架的充气装置，其接收启动信号并且基于接收到激活信号而充气该一个或多个安全气囊，以在该冲击之前部署来自存储装置的一个或多个气囊 框架与对象。

    Lenticular airship
    74.
    发明公开
    Lenticular airship 有权

    公开(公告)号：EP2527245A1

    公开(公告)日：2012-11-28

    申请号：EP12180691.3

    申请日：2007-10-15

    Applicant: LTA Corporation

    Inventor： Balaskovic, Pierre

    IPC: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34

    CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

    Abstract: An airship may include a hull (22) substantially shaped as an oblate spheroid, one or more frame members (122, 124) defining a support structure (20), wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member (315) operably coupled to a lower surface of the airship and at least one horizontal stabilizing member (315) having a first end and a second end. The at least one horizontal stabilizing member (315) may define an anhedral configuration. The airship may also include a vertical stabilizing member (310) having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member (310) may be configured to pivot within a vertical plane and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

    GOAL-BASED PLANNING SYSTEM
    76.
    发明申请
    GOAL-BASED PLANNING SYSTEM 审中-公开
    基于目标的规划系统

    公开(公告)号：WO2014177882A1

    公开(公告)日：2014-11-06

    申请号：PCT/GB2014/051368

    申请日：2014-05-02

    Applicant: BAE SYSTEMS PLC

    Inventor： BOOKLESS, John Paterson ,  DEITTERT, Markus ,  HERRING, Richard Norman ,  CULLEN, Elizabeth Jane

    IPC: G06Q10/04 ,  G06Q10/00 ,  G06Q50/00

    CPC classification number: B64C39/024 ,  B64C2201/00 ,  G05D1/0027 ,  G06Q10/20 ,  G06Q50/00

    Abstract: A method and apparatus for determining actions for entities (4, 6) such that a goal is accomplished constraints are satisfied. The method comprises: determining an initial plan comprising actions that, if performed by the entities (4, 6), the goal would be accomplished; determining that a constraint would not be satisfied if the initial plan was implemented; and iteratively performing steps (i) to (v) until a final plan that accomplishes the goal and satisfies the is determined. Step (i) comprises identifying a constraint that is not satisfied in part of the current plan. Step (ii) comprises determining a remedy that, if implemented, satisfies the identified constraint. Step (iii) comprises updating the goal specification to include the remedy. Step (iv) comprises, using the updated goal specification, determining a further plan that accomplishes the goal and the remedy. Step (v) comprises determining whether or not the further plan satisfies each constraint.

    Abstract translation: 一种用于确定实体（4,6）的动作的方法和装置，使得实现目标的约束被满足。 该方法包括：确定初始计划，其包括如果由实体（4,6）执行的动作，则该目标将被实现; 确定如果初始计划得到实施，则约束不会得到满足; 并迭代地执行步骤（i）至（v），直到确定实现目标并满足目标的最终计划。 步骤（i）包括识别在当前计划的一部分中不满足的约束。 步骤（ii）包括确定如果被实现的，满足所识别的约束的补救措施。 步骤（iii）包括更新目标规范以包括补救措施。 步骤（iv）包括使用更新的目标规范来确定实现目标和补救措施的进一步计划。 步骤（v）包括确定进一步的计划是否满足每个约束。

    MICRO UNMANNED AERIAL VEHICLE AND METHOD OF CONTROL THEREFOR
    77.
    发明申请
    MICRO UNMANNED AERIAL VEHICLE AND METHOD OF CONTROL THEREFOR 审中-公开
    微型无人驾驶航空器及其控制方法

    公开(公告)号：WO2014064431A3

    公开(公告)日：2014-07-10

    申请号：PCT/GB2013052745

    申请日：2013-10-22

    Applicant: BCB INT LTD ,  TORQUING GROUP LTD

    Inventor： REEDMAN IVAN ,  DAVIES BARRY

    IPC: G05D1/10

    CPC classification number: B64C39/024 ,  B64C19/00 ,  B64C39/028 ,  B64C2201/00 ,  B64C2201/14 ,  B64C2201/141 ,  B64C2230/00 ,  B64C2230/02 ,  G01S15/06 ,  G01S15/88 ,  G01S15/89 ,  G01S15/8913 ,  G01S15/8929 ,  G01S15/8993 ,  G01S15/93 ,  G05D1/0088 ,  G05D1/0202 ,  G05D1/101 ,  G05D1/102 ,  Y10S367/909

    Abstract: A micro unmanned aerial vehicle or drone ("UAV") 10 is remotely controlled through an HMI (309), although this remote control is supplemented by and selectively suppressed by an on-board controller (302). The controller operates to control the generation of a sonar bubble that generally encapsulates the UAV. The sonar bubble, which may be ultrasonic in nature, is produced by a multiplicity of sonar lobes generated by specific sonar emitters associated with each axis of movement for the UAV. The emitters produce individual and beamformed sonar lobes (80-102) that partially overlap to provide stereo or bioptic data in the form of individual echo responses detected by axis- specific sonar detectors (40-68). In this way, the on-board controller is able to interpret and then generate 3-D spatial imaging of the physical environment in which the UAV is currently moving or positioned. The controller is therefore able to plot relative and absolute movement of the UAV through the 3-D space by recording measurements from on-board gyroscopes (342), magnetometers (344) and accelerometers (346). Data from the sonar bubble can therefore both proactively prevent collisions with objects by imposing a corrective instruction to rotors (12-18) and other flight control system and can also assess and compensate for sensor drift.

    Abstract translation: 虽然该遥控器被车载控制器（302）补充并选择性地抑制，但通过HMI（309）远程控制微型无人驾驶飞行器或无人驾驶飞机（“UAV”）10。 控制器用于控制通常封装无人机的声纳气泡的产生。 本质上可能是超声波的声纳气泡由与用于UAV的每个运动轴相关联的特定声纳发射器产生的多个声纳波瓣产生。 发射器产生单个和波束形成的声纳波瓣（80-102），其部分重叠以提供由轴特定声纳探测器（40-68）检测的单独回波响应形式的立体声或生物数据。 以这种方式，车载控制器能够解释然后生成UAV当前正在移动或定位的物理环境的3-D空间成像。 因此，控制器能够通过记录来自板载陀螺仪（342），磁力计（344）和加速度计（346）的测量值来绘制无人机通过3-D空间的相对和绝对运动。 因此，来自声纳气泡的数据可以通过对转子（12-18）和其他飞行控制系统施加纠正指令来主动防止与物体的碰撞，并且还可以评估和补偿传感器漂移。

    MICRO UNMANNED AERIAL VEHICLE AND METHOD OF CONTROL THEREFOR
    78.
    发明申请
    MICRO UNMANNED AERIAL VEHICLE AND METHOD OF CONTROL THEREFOR 审中-公开
    微型无人机驾驶舱及其控制方法

    公开(公告)号：WO2014064431A2

    公开(公告)日：2014-05-01

    申请号：PCT/GB2013/052745

    申请日：2013-10-22

    Applicant: BCB INTERNATIONAL LTD. ,  TORQUING GROUP LTD.

    Inventor： REEDMAN, Ivan ,  DAVIES, Barry

    IPC: G05D1/10

    CPC classification number: B64C39/024 ,  B64C19/00 ,  B64C39/028 ,  B64C2201/00 ,  B64C2201/14 ,  B64C2201/141 ,  B64C2230/00 ,  B64C2230/02 ,  G01S15/06 ,  G01S15/88 ,  G01S15/89 ,  G01S15/8913 ,  G01S15/8929 ,  G01S15/8993 ,  G01S15/93 ,  G05D1/0088 ,  G05D1/0202 ,  G05D1/101 ,  G05D1/102 ,  Y10S367/909

    Abstract: A micro unmanned aerial vehicle or drone ("UAV") 10 is remotely controlled through an HMI (309), although this remote control is supplemented by and selectively suppressed by an on-board controller (302). The controller operates to control the generation of a sonar bubble that generally encapsulates the UAV. The sonar bubble, which may be ultrasonic in nature, is produced by a multiplicity of sonar lobes generated by specific sonar emitters associated with each axis of movement for the UAV. The emitters produce individual and beamformed sonar lobes (80-102) that partially overlap to provide stereo or bioptic data in the form of individual echo responses detected by axis- specific sonar detectors (40-68). In this way, the on-board controller is able to interpret and then generate 3-D spatial imaging of the physical environment in which the UAV is currently moving or positioned. The controller is therefore able to plot relative and absolute movement of the UAV through the 3-D space by recording measurements from on-board gyroscopes (342), magnetometers (344) and accelerometers (346). Data from the sonar bubble can therefore both proactively prevent collisions with objects by imposing a corrective instruction to rotors (12-18) and other flight control system and can also assess and compensate for sensor drift.

    Abstract translation: 通过HMI（309）远程控制微型无人驾驶飞行器或无人机（“UAV”）10，尽管该遥控器由车载控制器（302）补充并且由车载控制器（302） ）。 该控制器用于控制通常封装无人机的声纳气泡的产生。 声纳气泡本质上可能是超声波，是由与无人机每个运动轴相关的特定声纳发射器产生的多个声纳波瓣产生的。 发射器产生单独的和波束形成的声纳波束（80-102），部分重叠以提供立体声或活检数据，以由特定于轴的声纳探测器（40-68）检测到的单个回声响应的形式提供。 通过这种方式，机载控制器能够解释然后生成UAV当前移动或定位的物理环境的3-D空间成像。 因此，控制器能够通过记录来自机载陀螺仪（342），磁力计（344）和加速度计（346）的测量结果来绘制UAV通过3-D空间的相对和绝对移动。 因此，来自声纳气泡的数据可以通过向转子（12-18）和其他飞行控制系统施加纠正性指令来主动防止与物体的碰撞，并且还可以评估和补偿传感器漂移。

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