SYSTEMS AND METHODS FOR ATTITUDE CONTROL OF TETHERED AEROSTATS
    1.
    发明申请
    SYSTEMS AND METHODS FOR ATTITUDE CONTROL OF TETHERED AEROSTATS 审中-公开
    系统和方法用于精神病理学的控制

    公开(公告)号:WO2013043586A2

    公开(公告)日:2013-03-28

    申请号:PCT/US2012/055898

    申请日:2012-09-18

    IPC分类号: B64B1/50 B64B1/52 G05D1/10

    CPC分类号: B64B1/00 B64B1/50

    摘要: A control system for a tethered aerostat is provided, where up to two rotational and at least one translational degree of freedom are controlled to setpoints through the variation of tether lengths by an actuator system. The term tether includes a single tether, a tether group or a sub section of tether controlled by an individual actuator. Accurate rotational and translational control is essential for the successful operation of an aerostat under several applications, including surveillance, weather monitoring, and power generation. For a given use case, the controller can be constructed and arranged to manage the tradeoff between several key performance characteristics, such as transient performance, steady-state pointing accuracy, tether tension regulation, and power generation.

    摘要翻译: 提供了一种用于系留式空气净化器的控制系统,其中至多两个旋转和至少一个平移自由度通过致动器系统通过系绳长度的变化被控制到设定点。 术语系绳包括单个系绳,系绳组或由单个致动器控制的系绳的子部分。 精确的旋转和平移控制对于在多种应用(包括监视,气象监测和发电)的成功运行是必不可少的。 对于给定的用例,可以构造和布置控制器以管理诸如瞬态性能,稳态指示精度,系绳张力调节和发电之间的若干关键性能特征之间的权衡。

    SYSTEMS AND METHODS FOR AUTOMATED, LIGHTER-THAN-AIR AIRBORNE PLATFORM
    2.
    发明申请
    SYSTEMS AND METHODS FOR AUTOMATED, LIGHTER-THAN-AIR AIRBORNE PLATFORM 审中-公开
    用于自动轻型空气载体平台的系统和方法

    公开(公告)号:WO2018075632A1

    公开(公告)日:2018-04-26

    申请号:PCT/US2017/057177

    申请日:2017-10-18

    IPC分类号: B64B1/02

    摘要: Embodiments disclosed herein enable routine autonomous execution of at least some major phases of aerostat operation in response to commands from human or automated external operators, a built-in decision-making capacity, or both. Various embodiments combine one or more actively controlled tethers, aerodynamic aerostat control surfaces, mechanical assistive devices (e.g., jointed arms attached to a ground station), and/or active propulsors attached to the aerostat to govern aerostat behavior during launch, flight, and landing phases of operation. Some embodiments enable automatic autonomous performance of all phases of routine post-commissioning aerostat operation, including launch, flight, and landing, without any routine need for availability of a human crew.

    摘要翻译: 这里公开的实施例能够响应于来自人类或自动化外部操作员的指令,内置决策能力,或两者,来常规自主执行浮空器操作的至少一些主要阶段。 各种实施例将发射,飞行和着陆期间的一个或多个主动控制的绳索,空气动力学浮空器控制表面,机械辅助装置(例如,连接到地面站的连接臂)和/或附接到浮空器的主动推进器组合起来 操作阶段。 一些实施例使常规调试后的浮空器操作(包括起飞,飞行和着陆)的所有阶段的自动执行成为可能,而无需任何人员的可用性的常规需求。

    WIRELESS COMMUNICATION STATION
    4.
    发明申请
    WIRELESS COMMUNICATION STATION 审中-公开
    无线通信站

    公开(公告)号:WO2018053291A1

    公开(公告)日:2018-03-22

    申请号:PCT/US2017/051819

    申请日:2017-09-15

    摘要: According to at least one aspect, a large area wireless communication station is provided. The wireless communication station may provide mobile communication signals at distances up to (100) kilometers from the location of the station. The wireless communication station may include a plurality of antennas that are co-located and configured to each provide coverage to a portion of a coverage area and in sum to provide coverage to the entirety of the coverage area, a plurality of transmitters communicatively coupled to the plurality of antennas and configured to communicate with an external system, and a signal routing system configured to dynamically direct a radio frequency signal from any one or more of the plurality of transmitters to any one or more of the plurality of antennas.

    摘要翻译: 根据至少一个方面,提供了一种大面积无线通信站。 无线通信站可以提供距站最远(100)公里的移动通信信号。 无线通信站可以包括多个天线,这些天线共同定位并且被配置为每个提供对覆盖区域的一部分的覆盖并且总计提供对整个覆盖区域的覆盖,多个发射机通信地耦合到 多个天线并且被配置为与外部系统进行通信;以及信号路由系统,其被配置为动态地将来自所述多个发射机中的任何一个或多个发射机的射频信号引导至所述多个天线中的任何一个或多个天线。

    IMPROVED AEROSTAT SYSTEM
    5.
    发明申请
    IMPROVED AEROSTAT SYSTEM 审中-公开
    改进的航空系统

    公开(公告)号:WO2013109689A1

    公开(公告)日:2013-07-25

    申请号:PCT/US2013/021837

    申请日:2013-01-17

    IPC分类号: B64B1/66 B64B1/06 B64B1/52

    摘要: The invention provides an improved aerostat system including an aerostat, multiple tether groups and a base station. Spatially distinct tether groups allow for improved stability and controllability over a wide range of wind conditions. Independent actuation of the tether groups allows for control of the aerostat pitch and roll angle. A rotating platform including rails to rest the aerostat allows docking without auxiliary tethers, minimizing or eliminating the ground crew required to dock traditional aerostat systems. An optional controller allows remote or autonomous operation of the aerostat system. The invention is intended to extend the flight envelope in which aerostat systems can safely operate.

    摘要翻译: 本发明提供了一种改进的航空器系统,其包括空气净化器,多个系绳组和基站。 空间不同的系链组允许在宽范围的风力条件下提高稳定性和可控性。 系绳组的独立启动允许控制空气调节器俯仰和侧倾角。 包括轨道的旋转平台包括空气放置器,可以在没有辅助系绳的情况下进行对接,最大限度地减少或消除了对接传统的空气净化系统所需的地勤人员。 一个可选的控制器允许远程或自主运行空气净化系统。 本发明旨在扩展飞行包络,其中空气净化系统可以安全地操作。

    SYSTEMS AND METHODS FOR ATTITUDE CONTROL OF TETHERED AEROSTATS
    6.
    发明申请
    SYSTEMS AND METHODS FOR ATTITUDE CONTROL OF TETHERED AEROSTATS 审中-公开
    系统和方法的姿态控制受束缚的恒星

    公开(公告)号:WO2017087515A8

    公开(公告)日:2017-05-26

    申请号:PCT/US2016/062266

    申请日:2016-11-16

    IPC分类号: G05D1/08 B64B1/50 B64F3/00

    摘要: A control system for a tethered aerostat is provided, where at least one rotational and at least one translational degree of freedom are controlled to setpoints through the variation of tether lengths by an actuator system. The term tether includes a single tether, a tether group or a sub section of tether controlled by an individual actuator. Accurate rotational and translational control is essential for the successful operation of an aerostat under several applications, including surveillance, weather monitoring, communications, and power generation. For a given use case, the controller can be constructed and arranged to manage the tradeoff between several key performance characteristics, such as transient performance, steady-state pointing accuracy, tether tension regulation, and power generation.

    摘要翻译: 提供了用于系绳式空气静力持续器的控制系统,其中通过致动器系统通过系绳长度的变化将至少一个旋转和至少一个平移自由度控制为设定点。 术语系绳包括由单独的致动器控制的单系绳,系绳组或系绳的子部分。 精确的旋转和平移控制对于在多种应用中成功运行浮空器至关重要,这些应用包括监视,天气监测,通信和发电。 对于一个给定的用例,控制器可以构建和安排来管理几个关键性能特征之间的权衡,例如瞬态性能,稳态指向精度,系绳张力调节和发电。

    LIGHTER-THAN-AIR CRAFT FOR ENERGY-PRODUCING TURBINES
    7.
    发明申请
    LIGHTER-THAN-AIR CRAFT FOR ENERGY-PRODUCING TURBINES 审中-公开
    用于能源生产涡轮的轻型空气压缩机

    公开(公告)号:WO2014022770A1

    公开(公告)日:2014-02-06

    申请号:PCT/US2013/053421

    申请日:2013-08-02

    IPC分类号: B64B1/02 B64B1/50 F03D9/00

    摘要: A wind-based power generating system provides a wind energy converter for converting wind energy into another form of energy using a lighter-than-air craft configured to produce a positive net lift. The net lift includes both a net aerodynamic lift and a net buoyant lift. A tethering mechanism is configured to restrain the lighter-than-air craft with respect to the ground. The lighter-than-air craft defines an interior volume for containing a lighter-than-air gas, and the lighter-than-air craft has a fore section and an aft section. The tethering system has at least one attachment point on the fore section of the lighter-than-air craft and at least one attachment point on the aft section of the lighter-than-air craft. The lighter-than-air craft provides a stable aerodynamic moment with respect to a yaw axis about a center-of-mass of the lighter-than-air craft. The craft can be formed in a variety of aerodynamic profiles/shapes.

    摘要翻译: 风力发电系统提供了一种用于将风能转换成另一形式的能量的风能转换器,其使用被配置成产生正净升降机的轻于空气的工艺。 净升降机包括净空气动力升降机和净浮力升降机。 束缚机构构造成相对于地面限制轻型飞行器。 轻型空中飞行器具有用于容纳比空气较轻的气体的内部空间,而轻型飞行器具有前部和后部。 系绳系统在轻型飞行器的前部上具有至少一个连接点,以及轻型飞行器的后部上的至少一个附接点。 轻型飞行器相对于偏航轴提供了围绕轻型飞行器的中心质量的稳定的空气动力学力矩。 该工艺可以形成各种空气动力学特性/形状。

    PAYLOAD SUSPENSION FOR LIGHTER-THAN-AIR STRUCTURES
    8.
    发明申请
    PAYLOAD SUSPENSION FOR LIGHTER-THAN-AIR STRUCTURES 审中-公开
    用于轻型空气结构的载荷悬挂

    公开(公告)号:WO2013126891A1

    公开(公告)日:2013-08-29

    申请号:PCT/US2013/027650

    申请日:2013-02-25

    IPC分类号: B64B1/58 B64B1/38

    摘要: This invention provides a configuration of suspension lines, anchored with respect to an inner surface of an LTA structure, and which provide reactive forces between an LTA structure and its payload so as to constrain the translational and rotational motion of the payload to be nearly rigid with respect to the LTA structure. Illustratively, the configuration constrains the motion of the payload with respect to the LTA structure along all six degrees of freedom: e.g. horizontal, vertical and longitudinal translation and rotation about the longitudinal, horizontal and vertical axes.

    摘要翻译: 本发明提供了相对于LTA结构的内表面锚定的悬挂线的构造,并且其在LTA结构及其有效载荷之间提供反作用力,以便将有效载荷的平移和旋转运动约束为几乎刚性的 尊重LTA结构。 说明性地,该构造约束有效载荷相对于沿着所有六个自由度的LTA结构的运动:例如。 水平,垂直和纵向平移和围绕纵向,水平和垂直轴线的平移和旋转。