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    Methods and apparatus for pointing logic in aircraft
    1.
    发明授权
    Methods and apparatus for pointing logic in aircraft 有权

    公开(公告)号：US12135191B2

    公开(公告)日：2024-11-05

    申请号：US18166222

    申请日：2023-02-08

    Applicant: The Boeing Company

    Inventor： Douglas Famularo ,  Jeffery Saunders

    IPC: F41G5/18 ,  B64U10/14 ,  B64U101/16 ,  F41J9/08 ,  G05D1/00

    Abstract: Methods and apparatus for pointing logic in aircraft are disclosed. A disclosed example apparatus to aim an aiming device carried by an aircraft includes at least one memory, machine readable instructions, and processor circuitry. The processor is to at least one of instantiate or execute the machine readable instructions to determine a position of a target, determine an orientation of the aircraft, determine aiming points based on the orientation and a movement range of the aiming device, and determine a movement of at least one of the aircraft or the aiming device based on the aiming points and the position to orient the aiming device toward the target.

    System and method for decoy management
    3.
    发明授权
    System and method for decoy management 有权
    诱饵管理系统和方法

    公开(公告)号：US09372052B2

    公开(公告)日：2016-06-21

    申请号：US14326545

    申请日：2014-07-09

    Applicant: Timothy P. McGeehan

    Inventor： Timothy P. McGeehan

    IPC: F41G7/22 ,  F41J9/08 ,  F41G7/00

    CPC classification number: F41G7/224 ,  F41G7/007 ,  F41J9/08

    Abstract: System and method for determining which decoys should not be deployed based on the locations of the nearby high value units and other considerations. The system and method can visualize and manage the employment of decoys in a multi-platform environment by plotting the predicted path of decoys relative to high value unit (HVU) motion, and highlighting any situations that exist where the decoys (both air-drifting and self-propelled) launched from a platform can direct an incoming threat towards a high value unit. The system and method can develop, display, and automatically transmit a recommendation to launch or not launch a specific decoy.

    Abstract translation: 根据附近高价值单位的位置和其他考虑，确定不应部署哪些诱饵的系统和方法。 该系统和方法可以通过绘制相对于高值单位（HVU）运动的预测诱饵路径，在多平台环境中可视化和管理诱饵的使用，并突出显示任何存在于诱饵（空气漂移和 自推进）可以将进入的威胁引导到高价值单位。 该系统和方法可以开发，显示和自动传送推出或不启动特定诱饵的建议。

    SYSTEM AND METHOD FOR DECOY MANAGEMENT
    4.
    发明申请
    SYSTEM AND METHOD FOR DECOY MANAGEMENT 有权

    公开(公告)号：US20160010952A1

    公开(公告)日：2016-01-14

    申请号：US14326545

    申请日：2014-07-09

    Applicant: Timothy P. McGeehan

    Inventor： Timothy P. McGeehan

    IPC: F41G7/22 ,  F41J9/08

    CPC classification number: F41G7/224 ,  F41G7/007 ,  F41J9/08

    Abstract: System and method for determining which decoys should not be deployed based on the locations of the nearby high value units and other considerations. The system and method can visualize and manage the employment of decoys in a multi-platform environment by plotting the predicted path of decoys relative to high value unit (HVU) motion, and highlighting any situations that exist where the decoys (both air-drifting and self-propelled) launched from a platform can direct an incoming threat towards a high value unit. The system and method can develop, display, and automatically transmit a recommendation to launch or not launch a specific decoy.

    Perspective tracking system
    5.
    发明授权
    Perspective tracking system 有权
    透视跟踪系统

    公开(公告)号：US09052161B2

    公开(公告)日：2015-06-09

    申请号：US11641123

    申请日：2006-12-19

    Applicant: David Page

    Inventor： David Page

    IPC: G09B9/00 ,  F41G3/26 ,  F41J5/00 ,  F41J5/02 ,  F41J9/00 ,  F41J9/08 ,  F41A33/00 ,  G01S5/16 ,  G09B19/00 ,  G06F3/0346 ,  G06F17/30

    CPC classification number: G06F3/0346 ,  F41A33/00 ,  F41G3/26 ,  F41G3/2605 ,  F41G3/2661 ,  F41J5/02 ,  F41J9/00 ,  F41J9/08 ,  G01B11/14 ,  G01B21/042 ,  G01S5/163 ,  G06F17/30825 ,  G06F17/30831 ,  G06K9/3216 ,  G06K9/78 ,  G06T7/74 ,  G06T7/80 ,  G06T2207/10016 ,  G06T2207/30204 ,  G09B9/00 ,  G09B9/003 ,  G09B9/006 ,  G09B9/04 ,  G09B9/08 ,  G09B9/301 ,  G09B9/307 ,  G09B19/00

    Abstract: Resolution of perspective in three dimensions is necessary for intermeshing real players into simulated environments during virtual training exercises. A combination of small sized sensors and image recognition tracking algorithms allows the tracking element to be placed directly on the device whose perspective is desired. This provides a solution to determining perspective as it provides a direct measurement from the center axis of the observer. This invention employs a perspective tracking device to determine a point-of-gaze or a point-of-aim in a three-dimensional space to a high degree of accuracy. Point-of-gaze may be used to determine views for head mounted displays and aim-points for weapons. The invention may operate in an unconstrained space allowing simulation participants to operate in a larger, open environment. Areas of interest in the environment are bounded by emitters which identify the region and its physical constraints.

    Abstract translation: 在虚拟训练练习中，将真实玩家与模拟环境相互联系在一起，三维视角的分辨是必要的。 小尺寸传感器和图像识别跟踪算法的组合允许将跟踪元件直接放置在期望视角的设备上。 这提供了一种解决方案来确定透视，因为它提供了从观察者的中心轴的直接测量。 本发明采用透视跟踪装置以高精确度确定三维空间中的瞄准点或瞄准点。 注视点可用于确定头戴显示器和武器瞄准点的视图。 本发明可以在无约束空间中操作，允许模拟参与者在较大的开放环境中操作。 对环境感兴趣的领域受到识别该地区及其物理限制的排放者的约束。

    SELF-PROPELLED FLYING APPARATUS ADAPTED TO EMULATE A HOSTILE FIRING ACTION
    6.
    发明申请
    SELF-PROPELLED FLYING APPARATUS ADAPTED TO EMULATE A HOSTILE FIRING ACTION 审中-公开
    自适应飞行装置适用于模拟非常发动的动作

    公开(公告)号：US20140076131A1

    公开(公告)日：2014-03-20

    申请号：US14115774

    申请日：2012-04-16

    Applicant: John Chester-Parsons

    Inventor： John Chester-Parsons

    IPC: F41J2/00 ,  F41G7/00 ,  F41J9/08

    CPC classification number: F41G7/00 ,  F41G7/002 ,  F41J2/00 ,  F41J9/08 ,  F42B12/36 ,  F42B15/08 ,  F42B35/00

    Abstract: A self propelled flying vehicle (1) adapted to emulate a hostile firing action comprises an ultraviolet light source (5) in communication with a driving means (7) for driving the ultraviolet light source. The driving means (7) stores information indicative of an ultraviolet profile of a hostile firing action and, in use, communicates the ultraviolet profile to the ultraviolet light source (5).

    Abstract translation: 适于模拟敌对射击动作的自行车飞行器（1）包括与用于驱动紫外光源的驱动装置（7）连通的紫外光源（5）。 驱动装置（7）存储指示敌对射击动作的紫外线轮廓的信息，并且在使用中将紫外线轮廓传递到紫外线光源（5）。

    Buckle for kites and the like
    8.
    发明申请
    Buckle for kites and the like 失效
    扣风筝等

    公开(公告)号：US20050040292A1

    公开(公告)日：2005-02-24

    申请号：US10643821

    申请日：2003-08-19

    Applicant: Rollin Green

    Inventor： Rollin Green

    IPC: B63B35/79 ,  F41J9/08

    CPC classification number: B63B35/7993

    Abstract: Described is a device that releaseably couples a person to kites and other like sports equipment. The device for coupling to kites and other like sports equipment comprises a releasable hook mechanism attached to a spreader bar, said releasable hook mechanism comprising a releasable hook pivotally attached to a body that attached to the spreader bar, said releasable hook pivotally movable from a closed position to an open position. The releasable hook, preferably, is resiliently biased from the closed position to the open position. The device may further comprise a release plate mechanism that releasably holds the rotatable hook in the closed position. Additionally, the device may further comprise a release defeat mechanism that prevents release of the rotatable hook by the release plate mechanism. Finally, the device may further comprise a rotating safety lease attachment ring that is rotatingly attached to the body of the device.

    Abstract translation: 描述了可释放地将人耦合到风筝和其他类似运动器材的装置。 用于联接到风筝和其它类似运动器材的装置包括附接到吊具杆的可释放的钩子机构，所述可释放的钩子机构包括可枢转地连接到附接到吊架杆的主体的可释放的钩子，所述可释放的钩子可从闭合的 位置到一个开放的位置。 可释放的钩优选地从关闭位置弹性地偏压到打开位置。 该装置还可以包括释放板机构，该释放板机构将可旋转钩可释放地保持在关闭位置。 另外，该装置还可以包括释放失效机构，其防止由释放板机构释放可旋转钩。 最后，该装置还可以包括旋转的安全租赁附接环，其旋转地附接到装置的主体。

    Propeller system for kite
    9.
    发明申请
    Propeller system for kite 审中-公开
    风筝螺旋桨系统

    公开(公告)号：US20050006532A1

    公开(公告)日：2005-01-13

    申请号：US10617220

    申请日：2003-07-10

    Applicant: Don Tabor

    Inventor： Don Tabor

    IPC: A63H27/08 ,  F41J9/08

    CPC classification number: A63H27/082

    Abstract: A propeller system including one or more blade portions configured to couple to each other, and optionally a support portion, and an axle portion configured to couple to the rotating member and to the support portion.

    Abstract translation: 一种螺旋桨系统，包括一个或多个叶片部分，所述叶片部分被构造成彼此联接，并且可选地是支撑部分，以及轴部分，其构造成联接到旋转部件和支撑部分。

    Flight control system for airplane
    10.
    发明授权
    Flight control system for airplane 失效
    飞机飞行控制系统

    公开(公告)号：US5984240A

    公开(公告)日：1999-11-16

    申请号：US882405

    申请日：1997-06-25

    Applicant: Takashi Shinagawa

    Inventor： Takashi Shinagawa

    IPC: F41J9/08 ,  B64C13/16 ,  B64C13/18 ,  G05D1/08

    CPC classification number: B64C13/16 ,  G05D1/085

    Abstract: A flight control system according to the present invention includes a vertical acceleration control device for calculating a pitch axis steering angle command to make a difference between a vertical acceleration of an airplane and a target turn acceleration to zero, and transmitting it as a variable to a pitch axis control device, a reference bank angle device for calculating a reference bank angle from the target turn acceleration, an altitude control device for calculating a bank angle correcting quantity from a difference between an altitude of the airplane and a target altitude and obtaining a bank angle command by correcting the reference bank angle, and a roll axis control device for calculating a roll axis steering angle command for make a difference between a real bank angle and the bank angle command to zero and for transmitting it as a variable to a roll axis control device.

    Abstract translation: 根据本发明的飞行控制系统包括垂直加速度控制装置，用于计算俯仰轴转向角度命令以使飞机的垂直加速度和目标转弯加速度之间的差值为零，并将其作为变量发送到 俯仰轴控制装置，用于从目标转弯加速度计算基准倾斜角度的基准倾斜角度装置，用于根据飞机的高度与目标高度之间的差值计算出倾斜角度校正量的高度控制装置， 通过校正基准倾斜角度的角度指令，以及滚动轴控制装置，用于计算滚动轴转向角度指令，以使实际倾斜角度和倾斜角度指令之间的差为零，并将其作为变量发送到滚动轴线 控制装置

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