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SURVEYING AIRPLANE, TARGET FOR SURVEYING AIRPLANE, AND AUTOMATIC COLLIMATION SURVEYING SYSTEM

机译:侦察飞机,侦察飞机的目标和自动集合侦察系统

摘要

PPROBLEM TO BE SOLVED: To provide a compact automatic collimation surveying airplane allowing normal and reverse observations, a target for the surveying airplane, and an automatic collimation surveying system therefor. PSOLUTION: An LED light source 12a having 1 of wavelength is provided in a position of a distance L (Fig.4) in an upper side of the center of a reflecting prism P on the vertical center line of the target T, and an LED light source 12b having 1 of wavelength is provided in a position of the distance L (Fig.4) in an under side of the center. The LED light sources 12a, 12b are modulation-light-emitted in a frequency f1. An LED light source 12c having 2 of wavelength is provided in a position of the distance L (Fig.4) in a left side of the center on a horizontal line passed through the center of the reflecting prism P, and an LED light source 12d having 2 of wavelength is provided in a position of the distance L (Fig.4) in a right side of the center. The LED light sources 12c, 12d are modulation-light-emitted in a frequency f2. A two-split photoreception sensor 33A is provided in a telescope part 3 of the survey airplane, modulated lights by the LED light sources 12a, 12b are photoreceived thereby, a two-split photoreception sensor 33B is provided in the telescope part 3 thereof, and modulated lights by the LED light sources 12c, 12d are photoreceived thereby. PCOPYRIGHT: (C)2004,JPO&NCIPI
机译:

要解决的问题:提供一种紧凑的自动准直测量飞机,该飞机可以进行正向和反向观察,该测量飞机的目标及其自动准直测量系统。

解决方案:在目标T的垂直中心线上的反射棱镜P的中心的上侧,在距离L(图4)的位置处提供一个波长为1的LED光源12a,在中心的下侧的距离L(图4)的位置设有波长为1的LED光源12b。 LED光源12a,12b以频率f1调制发光。在通过反射棱镜P的中心的水平线上的中心的左侧的距离L(图4)的位置上,设置波长为2的LED光源12c和LED光源12d。在中心的右侧的距离L(图4)的位置上设置波长为2的光。 LED光源12c,12d以频率f2调制发光。在勘测飞机的望远镜部分3中设置有两分光接收传感器33A,从而对由LED光源12a,12b调制的光进行光接收,在望远镜部分3中设置有两分光接收传感器33B,并且LED光源12c,12d调制的光由此被光接收。

版权:(C)2004,日本特许厅和日本国家唱片公司

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