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    • 2. 发明公开
    • Infrared tracker for a portable missile launcher
    • Infrarotverfolgerfüreinen tragbarenFlugkörperwerfer。
    • EP0562785A1
    • 1993-09-29
    • EP93302129.7
    • 1993-03-22
    • Hughes Aircraft Company
    • Carlson, James J.
    • F41G7/30
    • F41G7/303
    • A portable missile launcher (12) has all of the infrared tracker (20) mounted to the same housing (48). The infrared missile beacon image beam (26) is intercepted by a rotating prism (28) which directs a portion of the beam to a narrow field detector (32) and reflects a further portion from a coating (30) onto a wide field detector (34). The detectors (32,34) provide yaw and pitch signals (40,42) which are compared with on-course information producing error signals communicated to the missile for course correction, if needed.
    • 便携式导弹发射器(12)具有安装到同一壳体(48)的所有红外跟踪器(20)。 红外导弹信标图像光束(26)被旋转棱镜(28)拦截,旋转棱镜(28)将光束的一部分引导到窄场检测器(32),并将另一部分从涂层(30)反射到宽视场检测器 34)。 如果需要,检测器(32,34)提供偏航和俯仰信号(40,42),该偏航和俯仰信号与当前信息产生误差信号进行比较,该误差信号传递给导弹以进行路线校正。
    • 3. 发明公开
    • Optical viewing and near infrared tracking system for a portable missile launcher
    • 光学观测和近红外跟踪系统,便携式导弹发射器。
    • EP0552685A1
    • 1993-07-28
    • EP93100592.0
    • 1993-01-15
    • Hughes Aircraft Company
    • Carlson, James J.Noyes, Gary R.
    • F41G7/30
    • G02B27/142G02B5/282G02B23/04G02B27/1006G02B27/141
    • An optical system (10) for portable missile launcher (23) includes an objective lens (12) for receiving the entire visual and near infrared light energy emanating from a target (14) and immediate background of the target. The light energy from the objective lens then passes through a Porro prism assembly (16) which acts to direct visual light along a first path to an eyepiece (20) and near infrared along a second path at approximately a right angle to the first path where it is received by a tracker assembly (22) and monitored. The Porro prism (16) is constructed in accordance with this invention to include a multi-layer interference dichroic coating (18) disposed between the two prisms (34, 36) which make up the prism assembly. This coating is of such a nature as to readily permit light energy in the visual range to pass directly through the coating, but at the same time to reflect the near infrared components along a second path bringing them to focus on the tracker assembly (22).
    • 用于便携式导弹发射(23)的光学系统(10)包括在用于接收从目标(14)和所述目标的直接背景发出的整个视觉和近红外光的能量物镜(12)。 来自物镜的光能量然后通过波罗棱镜组件(16),其作用于沿着第一路径引导视觉光以目镜(20)和沿第二路径近红外线在大约成直角的第一路径,其中 它是由一个跟踪器组件(22)和监视的接收。 所述波罗棱镜(16)被构造在雅舞蹈与本发明以包括两个棱镜(34,36),其构成了棱镜组件之间设置一个多层干涉二向色涂层(18)。 该涂层是寻求性质容易地允许光能量在视觉范围内穿过涂层直接传递的,但在同一时间,以反映沿着第二路径近红外组分使它们集中在跟踪器组件(22) ,