GÖKTÜRK-2: Two years of operation

Goksel Gurgenburan, E. Cinar
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引用次数: 4

Abstract

The first high resolution research and development (R&D) earth observation satellite of Turkey, named as GÖKTÜRK-2 (GKT-2), was successfully launched on 18 December 2012 from Jiuquan Satellite Launch Center, China on a LM-2D launcher to its Low Earth Orbit (LEO). Reaching its operational LEO, the satellite underwent in orbit tests lasting for about 6 months. Both space and ground segments passed acceptance and commissioning tests successfully before the satellite was fully ceded to Turkish Air Force (TurAF) satellite operations team. After commissioning, regular operations such as telemetry, tracking, and command (TT&C), mission planning, data acquisition and image processing have started. This paper will include GKT-2 mission overview, technical specifications and nominal operations loop concept which describes on orbit servicing (OOS), mission planning, image acquisition modes, storage planning and restriction, TT&C, trend analyses and conjunction assessment.
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GÖKTÜRK-2:运营两年
2012年12月18日,土耳其第一颗高分辨率研发(R&D)地球观测卫星GÖKTÜRK-2 (GKT-2)在中国酒泉卫星发射中心成功发射到近地轨道(LEO)。到达可运行的近地轨道后,该卫星进行了持续约6个月的轨道测试。在卫星完全移交给土耳其空军(TurAF)卫星作业队之前,空间和地面部分都成功地通过了验收和调试测试。调试后,常规操作,如遥测、跟踪和指挥(TT&C)、任务规划、数据采集和图像处理已经开始。本文将包括GKT-2任务概述、技术规范和标称操作回路概念,其中描述在轨服务(OOS)、任务规划、图像采集模式、存储规划和限制、TT&C、趋势分析和联合评估。
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