Automatic configuration control of a device
    1.
    发明授权
    Automatic configuration control of a device 有权
    设备的自动配置控制

    公开(公告)号:US08761967B2

    公开(公告)日:2014-06-24

    申请号:US13478520

    申请日:2012-05-23

    IPC分类号: B64C37/02 G06F19/00

    摘要: Methods, systems, and devices for determining system/device configuration and setting a mode of operation based on the determined configuration. An air vehicle processor: (a) receives a component information set of at least one external component; (b) determine a mode of operation, by the processor having a current mode of operation setting, based on the received component information and at least one of: an initial mode of operation setting and the current mode of operation setting; (c) determines whether all of the one or more received component information sets match a configuration requirement; (d) transitions to a flight-ready status if the determination is a conjunctive match; and (e) transition to a reset status if the determination is not a conjunctive match.

    摘要翻译: 用于确定系统/设备配置并基于所确定的配置来设置操作模式的方法,系统和设备。 一种飞行器处理器:(a)接收至少一个外部部件的部件信息组; (b)基于接收到的分量信息和至少一个操作设置模式和当前操作模式设置中的至少一个来确定具有当前操作模式设置的处理器的操作模式; (c)确定所述一个或多个接收到的分量信息集合是否匹配配置要求; (d)如果确定是联合匹配,则转换到飞行就绪状态; 和(e)如果确定不是联合匹配,则转换到复位状态。

    Automatic Configuration Control of a Device
    2.
    发明申请
    Automatic Configuration Control of a Device 有权
    设备的自动配置控制

    公开(公告)号:US20120232722A1

    公开(公告)日:2012-09-13

    申请号:US13478520

    申请日:2012-05-23

    IPC分类号: G05D1/00

    摘要: Methods, systems, and devices for determining system/device configuration and setting a mode of operation based on the determined configuration. An air vehicle processor: (a) receives a component information 14 set of at least one external component; (b) determine a mode of operation, by the processor having a current mode of operation setting, based on the received component information and at least one of: an initial mode of operation setting and the current mode of operation setting; (c) determines whether all of the one or more received component information sets match a configuration requirement; (d) transitions to a flight-ready status if the determination is a conjunctive match; and (e) transition to a reset status if the determination is not a conjunctive match.

    摘要翻译: 用于确定系统/设备配置并基于所确定的配置来设置操作模式的方法,系统和设备。 一种飞行器处理器:(a)接收至少一个外部部件的部件信息14组; (b)基于接收到的分量信息和至少一个操作设置模式和当前操作模式设置中的至少一个来确定具有当前操作模式设置的处理器的操作模式; (c)确定所述一个或多个接收到的分量信息集合是否匹配配置要求; (d)如果确定是联合匹配,则转换到飞行就绪状态; 和(e)如果确定不是联合匹配,则转换到复位状态。

    Articulated Sensor Support Structure
    3.
    发明申请
    Articulated Sensor Support Structure 有权
    铰接传感器支撑结构

    公开(公告)号:US20120251092A1

    公开(公告)日:2012-10-04

    申请号:US13478764

    申请日:2012-05-23

    IPC分类号: G03B17/56 B64C1/14 B64C1/00

    摘要: Embodiments include an assembly comprising: (a) a camera support structure comprising: a masthead disposed on the distal end of a mast wherein the masthead is configured to receive an imaging element; where a proximal end of the mast rotatably engaging an azimuth-elevation joint assembly wherein the azimuth-elevation joint assembly comprises a first angular actuator of a first rotational degree-of-freedom and a second angular actuator of a second rotational degree of freedom; and (b) a camera support structure housing comprising an aperture and a hatch wherein the hatch is resiliently biased to close the aperture; and wherein the camera support structure is configured to overcome the hatch resilient bias by at least one of: the release of a pin restraining a loaded spring and a rotational actuation of the mast via at least one of the first angular actuator and the second angular actuator.

    摘要翻译: 实施例包括一种组件,包括:(a)照相机支撑结构,包括:桅杆,其设置在桅杆的远端上,其中桅顶被构造成接收成像元件; 其中所述桅杆的近端可旋转地接合方位角接头组件,其中所述方位角接头组件包括第一旋转自由度的第一角度致动器和第二旋转自由度的第二角度致动器; 和(b)相机支撑结构外壳,其包括孔和舱口,其中所述舱口被弹性偏压以关闭所述孔; 并且其中所述照相机支撑结构被配置为通过以下至少一个来克服所述舱口弹性偏压:释放限制装载的弹簧的销和通过所述第一角度致动器和所述第二角致动器中的至少一个的所述桅杆的旋转致动 。

    Articulated sensor support structure
    6.
    发明授权
    Articulated sensor support structure 有权
    铰链传感器支撑结构

    公开(公告)号:US08548314B2

    公开(公告)日:2013-10-01

    申请号:US13478764

    申请日:2012-05-23

    IPC分类号: G03B39/00 G03B17/00

    摘要: Embodiments include an assembly comprising: (a) a camera support structure comprising: a masthead disposed on the distal end of a mast wherein the masthead is configured to receive an imaging element; where a proximal end of the mast rotatably engaging an azimuth-elevation joint assembly wherein the azimuth-elevation joint assembly comprises a first angular actuator of a first rotational degree-of-freedom and a second angular actuator of a second rotational degree of freedom; and (b) a camera support structure housing comprising an aperture and a hatch wherein the hatch is resiliently biased to close the aperture; and wherein the camera support structure is configured to overcome the hatch resilient bias by at least one of: the release of a pin restraining a loaded spring and a rotational actuation of the mast via at least one of the first angular actuator and the second angular actuator.

    摘要翻译: 实施例包括一种组件,包括:(a)照相机支撑结构,包括:桅杆,其设置在桅杆的远端上,其中桅顶被构造成接收成像元件; 其中所述桅杆的近端可旋转地接合方位角接头组件,其中所述方位角接头组件包括第一旋转自由度的第一角度致动器和第二旋转自由度的第二角度致动器; 和(b)相机支撑结构外壳,其包括孔和舱口,其中所述舱口被弹性偏压以关闭所述孔; 并且其中所述照相机支撑结构被配置为通过以下至少一个来克服所述舱口弹性偏压:释放限制装载的弹簧的销和通过所述第一角度致动器和所述第二角致动器中的至少一个的所述桅杆的旋转致动 。