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Overview of Optical Inter-orbit Communication Engineering Test Satellite (OICETS)

机译:光学轨道间通信工程测试卫星(OICETS)概述

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The optical inter-orbit communication test satellite (OICETS) has been developed by NASDA (National Space Development Agency of Japan) in order to perform the inter-satellite optical link experiment with a GEO-satellites of ESA (European Space Agency) named "ARTEMIS (Advanced Relay and Technology Mission Satellite)". OICETS will be launched into a circular low earth orbit in 2005. In this paper, the overview of OICETS and the optical terminal "LUCE(Laser Utilizing Communications Equipment)" boarded on OICETS is introduced. The objective of OICETS is to perform on-orbit demonstrations of pointing, acquisition and tracking technologies, and other key technology elements for optical inter-orbit communications. The data rates for forward (ARTEMIS to OICETS) and return (OICETS to ARTEMIS) links correspond to 2 and 50 Mbps at the optical wavelength of 0.8 μm, respectively. The proto-flight tests of the OICETS flight model was finished in January 2002. In addition, results of an optical compatibility test between LUCE and the optical terminal of ARTEMIS in geo-stationary orbit at 21.5° East is described. The engineering model (EM) of LUCE is placed at ESAs Optical Ground Station (OGS) in Tenerife, Canary Island. The aim of the test is to verify the end-to-end optical interfaces such as intensity, wavelength, polarization, modulation scheme of optical signals and also acquisition sequences between both optical terminals.
机译:光学轨道间通信测试卫星(OICETS)已由纳斯达(日本国家空间开发机构)开发,以便使用名为“Artemis”的ESA(欧洲空间机构)的地质卫星进行卫星间光链路实验(高级继电器和技术任务卫星)“。 OICET将于2005年推出到圆形低地轨道中。在本文中,介绍了OICET和光学终端“Luce(激光利用通信设备)”的概述。 OICET的目标是执行指向,获取和跟踪技术的轨道演示以及用于光学轨道通信的其他关键技术元素。向前(Aricemis至OICET)的数据速率和返回(OICET到Artemis)链路分别对应于0.8μm的光波长的2和50mbps。 OICETS飞行模型的原型试验于2002年1月结束。此外,还描述了在21.5°EAST的地理静止轨道中劳动和Astemis光学端子之间的光学相容性测试的结果。 Luce的工程模型(EM)位于加那利岛特内里费岛的ESAS光学地面站(OGS)。该测试的目的是验证光信号的强度,波长,极化,调制方案的端到端光学接口,以及两个光学终端之间的采集序列。

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