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    UAV LAUNCHING FROM MOVING PLATFORM
    242.
    发明申请
    UAV LAUNCHING FROM MOVING PLATFORM 有权
    无人机从移动平台发射

    公开(公告)号：US20140252162A1

    公开(公告)日：2014-09-11

    申请号：US14197389

    申请日：2014-03-05

    Applicant: IGOR TELLER ,  PAVEL SOIFER

    Inventor： IGOR TELLER

    IPC: B64F1/10

    CPC classification number: B64F1/10 ,  B64C2201/08 ,  B64C2201/205 ,  B64C2201/208

    Abstract: A system for launching an unmanned aerial vehicle (UAV) from a moving platform, the system comprising: a platform configured to carry the UAV; one or more sensors configured to measure forces acting between said platform and said UAV in one or more directions; a mooring mechanism configured to moor said UAV to said platform; and a controller configured to: transmit at least one trimming command to said UAV based on measurements of said one or more sensors, and cause said mooring mechanism to release said UAV from said platform following the transmitting of the at least one trimming command, when the measurements of said one or more sensors indicate that a lift force is sufficiently close to a weight of the UAV.

    Abstract translation: 一种用于从移动平台发射无人机（UAV）的系统，该系统包括：被配置为承载无人机的平台; 一个或多个传感器被配置为在一个或多个方向上测量在所述平台和所述UAV之间作用的力; 系泊机构，其构造成将所述无人机停泊在所述平台上; 以及控制器，其被配置为：基于所述一个或多个传感器的测量将至少一个修整命令发送到所述UAV，并且在所述至少一个修整命令的发送之后使所述系泊机构从所述平台释放所述UAV， 所述一个或多个传感器的测量指示提升力足够接近无人机的重量。

    SYSTEMS AND METHODS TO LAUNCH AIRCRAFT
    243.
    发明申请
    SYSTEMS AND METHODS TO LAUNCH AIRCRAFT 审中-公开
    启动飞机的系统和方法

    公开(公告)号：US20140117153A1

    公开(公告)日：2014-05-01

    申请号：US13662269

    申请日：2012-10-26

    Applicant: The Boeing Company

    Inventor： James J. Childress ,  Daniel J. Perron

    IPC: B64F1/04

    CPC classification number: B64C39/024 ,  B64C2201/08 ,  B64C2201/208 ,  B64F1/04

    Abstract: Systems and methods to launch an aircraft are disclosed. In one embodiment, a system to launch an aircraft comprises a launch arm comprising at least one load cell, an aircraft coupled to the launch arm, and a release mechanism in communication with the at least one load cell, wherein the release mechanism releases the aircraft when the at least one load cell indicates that a load on the launch arm is below a predetermined threshold. Other embodiments may be described.

    Abstract translation: 公开了发射飞机的系统和方法。 在一个实施例中，发射飞行器的系统包括发射臂，其包括至少一个称重传感器，耦合到发射臂的飞行器以及与所述至少一个称重传感器通信的释放机构，其中所述释放机构释放飞行器 当所述至少一个称重传感器指示所述发射臂上的负载低于预定阈值时。 可以描述其他实施例。

    Aerial vehicle launching system and method
    244.
    发明授权
    Aerial vehicle launching system and method 有权
    航空发射系统及方法

    公开(公告)号：US07665691B2

    公开(公告)日：2010-02-23

    申请号：US11679365

    申请日：2007-02-27

    Applicant: Patrick T. Hanzlick ,  Joshua J. Lange

    Inventor： Patrick T. Hanzlick ,  Joshua J. Lange

    IPC: B64F1/10

    CPC classification number: B64F1/10 ,  B64C2201/084 ,  B64C2201/208

    Abstract: An aerial vehicle launching system includes a launch platform and a restraint system coupled to the launch platform. The restraint system has at least one passive restraint suitably adapted to indirectly restrain an aerial vehicle. The restraint system is configured to coordinate the uniform retention and release of the passive restraint in order to launch the aerial vehicle.

    Abstract translation: 飞行器发射系统包括发射平台和耦合到发射平台的约束系统。 约束系统具有至少一个适当地适应于间接限制飞行器的被动约束。 约束系统被配置为协调被动约束的均匀保持和释放以便发射飞行器。

    Unmanned Airborne Vehicle For Geophysical Surveying
    245.
    发明申请
    Unmanned Airborne Vehicle For Geophysical Surveying 审中-公开
    无人机地球物理测量

    公开(公告)号：US20080125920A1

    公开(公告)日：2008-05-29

    申请号：US11576590

    申请日：2005-10-11

    Applicant: Philip John Miles ,  Richard Thomas Partner ,  Kenneth Ronald Keeler ,  Terence James McConnell

    Inventor： Philip John Miles ,  Richard Thomas Partner ,  Kenneth Ronald Keeler ,  Terence James McConnell

    IPC: G05D1/04 ,  G01C23/00 ,  G01V3/165 ,  B64C39/02 ,  G01V3/40 ,  G06F19/00

    CPC classification number: B64C39/024 ,  B64C2201/084 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/182 ,  B64C2201/208 ,  G01V3/165

    Abstract: An un-manned airborne vehicle (UAV), for acquiring aeromagnetic data for geophysical surveying at low altitude on land or over water, comprising an extended fuselage that is adapted to hold and maintain magnetometer and a magnetic compensation magnetometer at a minimum distance from the avionics and propulsion systems of the UAV. The magnetometer measures magnetic anomalies and the magnetic compensation magnetometer measures magnetic responses corresponding to the pitch, yaw and roll of the UAV. A data acquisition system stores and removes the magnetic response measurements from the magnetic anomaly measurements. The data acquisition system also stores a survey flight plan and transmits the same to the avionics system. The generator of the UAV is shielded and the propulsion system is stabilized to reduce magnetic and vibrational noises that can interfere with the operation of the magnetometer.

    Abstract translation: 一种无人载客空中飞行器（UAV），用于获取陆上或水上低空地球物理测量的航空数据，包括一个延伸的机身，适用于将磁力计和一个磁性补偿磁力计保持在离飞行距离最远的距离 和无人机的推进系统。 磁力计测量磁异常，磁补偿磁力计测量对应于无人机的俯仰，偏航和滚动的磁响应。 数据采集​​系统从磁异常测量中存储和去除磁响应测量。 数据采集​​系统还存储一个调查飞行计划，并将其传送到航空电子系统。 无人机的发电机被屏蔽并且推进系统被稳定以减少可能干扰磁力计操作的磁和振动噪声。

    VEHICLE ASSIST DRONE
    249.
    发明公开
    VEHICLE ASSIST DRONE 审中-公开

    公开(公告)号：US20240019864A1

    公开(公告)日：2024-01-18

    申请号：US17864734

    申请日：2022-07-14

    Applicant: GM Cruise Holdings LLC

    Inventor： Mohamed Mostafa Elshenawy

    IPC: G05D1/00 ,  B64C39/02

    CPC classification number: G05D1/0088 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/208 ,  B64C2201/141 ,  G05D2201/0213

    Abstract: Particular embodiments described herein provide for a vehicle assist drone. The vehicle assist drone can be operated in different modes. For example, the vehicle assist drone can be deployed in a user of an AV service assist mode, a clear occlusion mode, refined routing mode, a security mode, a search and rescue mode (e.g., search for missing child mode), or some other mode. In addition, the vehicle assist drone can be used to supplement a vehicle's sensors. For example, supplementary sensor data from the vehicle assist drone can be used in place of the vehicle's sensors or combined with sensor data from the onboard sensors of the vehicle to supplement the vehicle's sensors.

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