Stabilized gimbal platform
    3.
    发明授权
    Stabilized gimbal platform 失效
    稳定万向平台

    公开(公告)号:US4520973A

    公开(公告)日:1985-06-04

    申请号:US484050

    申请日:1983-04-11

    IPC分类号: F41G7/22 F42B15/01 F42B15/02

    摘要: A stabilized gimbal platform is provided by use of rate gyro stabilized a of a gimbal ring. A bail gimbal is used with both pitch and yaw inner gimbals to provide low friction stabilization over a large angular pointing range. This bail ring combination surrounds a lens assembly sensor, an automatic light level control device suitable to search for and track targets in a given frequency or wavelength range. By aiming, the gimbal arrangement permits the entire lens sensor arrangement to actually point and steer towards the desired target direction. The bail is balanced with drive assembly to provide stability to the bail. The bail itself is not mounted on its axis of rotation but rather is off-axis mounted on bearings for support and driven by an off-axis torque motor drive. The bail assembly can be driven by a metal band to provide smooth rotation of the bail assembly.

    摘要翻译: 通过使用万向节环的速率陀螺稳定轴来提供稳定的万向平台。 一个吊环万向节与俯仰和偏转内部的万向节一起使用,以便在较大的角度指向范围内提供低摩擦稳定性。 这种吊环组合包围一个透镜组件传感器,一个适用于搜索和跟踪给定频率或波长范围内的目标的自动光级控制装置。 通过瞄准,万向架布置允许整个透镜传感器装置实际上指向并转向所需的目标方向。 保释卡与驱动装置平衡,以保证吊环的稳定性。 吊环本身没有安装在其旋转轴线上,而是偏轴安装在轴承上用于支撑并由离轴扭矩电机驱动器驱动。 吊环组件可由金属带驱动以提供吊环组件的平滑旋转。

    Integral data acquisition capacity
    4.
    发明授权
    Integral data acquisition capacity 失效
    积分数据采集能力

    公开(公告)号:US06598828B2

    公开(公告)日:2003-07-29

    申请号:US09801126

    申请日:2001-03-05

    IPC分类号: G08C2500

    CPC分类号: F41G7/007

    摘要: Provided is a modified configuration that permits operation of instrumentation onboard platforms that may experience severe environmental conditions. The instrumentation permits autonomous acquisition of performance data. Acquired data may be recorded for later playback as well as provided to the platform's operator in real time in multiple formats, such as warning lights, digital displays, video, or audio. An application would be for sensor systems used on an automobile to record performance data, providing a warning when routine maintenance is due or a catastrophic failure is imminent. A specific application uses a flight-certified missile launcher pod on an F/A-18 aircraft, as incorporated in the aircraft's wingtip and modified to hold instrumentation conforming, at least in part, to the launcher pod's internal dimensions. This arrangement enables autonomous onboard display and recording of data from the captive carry testing of an AIM-9X missile and follow-on designs that may be based on the AIM-9X.

    摘要翻译: 提供了一种修改的配置,允许可能遇到严重环境条件的仪表板载平台的操作。 仪器允许自动获取性能数据。 获取的数据可以被记录以供稍后播放,并且以多种格式实时提供给平台的操作者,例如警示灯,数字显示器,视频或音频。 一种应用是用于汽车上的传感器系统来记录性能数据,当日常维护到期时提供警告或即将发生灾难性故障。 特定应用程序使用F / A-18飞机上的飞行认证的导弹发射器舱,并将其装配在飞机的翼尖上,并进行修改,以保持至少部分符合发射舱的内部尺寸的仪器。 这种安排使得能够自主地显示和记录来自AIM-9X导弹的自动进位测试和可能基于AIM-9X的后续设计的数据。

    Missile seeker optical system
    5.
    发明授权
    Missile seeker optical system 失效
    导弹探测器光学系统

    公开(公告)号:US4291848A

    公开(公告)日:1981-09-29

    申请号:US506499

    申请日:1974-09-13

    申请人: Keith E. Clark

    发明人: Keith E. Clark

    IPC分类号: F41G7/22 F41G7/26

    摘要: A missile seeker optical system which provides off-boresight viewing anglesp to 135.degree. by the addition of two spherical-toric corrector lenses which cooperate with a conventional achromatic lens used as the seeker objective.

    摘要翻译: 一种导弹探测器光学系统,其通过添加两个与使用作为探测器目标的常规消色差透镜配合的球面复曲面校正器透镜提供高达135度的视距视角。