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Simulation model and on-ground performances validation of the PAT system for the SILEX program

机译:SILEX程序的PAT系统的仿真模型和现场性能验证

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Abstract: This paper presents a description of the simulation model and the on-ground performances validation of the Pointing Acquisition and Tracking (PAT) subsystem of the European SILEX program (Semiconductor laser Intersatellite Link Experiment). The SILEX scenario is composed of two terminals mounted on low earth orbit (SPOT 4) and geostationary orbit (ARTEMIS) spacecrafts. Due to the limited laser beam divergence angle (typical intersatellite distance of 45000 km) a very accurate pointing performance is required. The PAT subsystem is in charge of the initialization of link (acquisition), of the tracking of incoming beam and of the pointing of emitted laser beam. Taking into account all disturbance sources (host spacecraft vibrations, electromechanical or optical noises) the pointing performance is less than 2 $mu@rad over a frequency bandwidth of 1 kHz. In a first part, a short presentation of the retained strategies (phases of the PAT mission, operating modes) and functional architecture (control laws, sampling frequencies) is given. In order to validate the PAT performance assessment, which is based on measurements at equipment level and analysis at subsystem level, a complete time simulation software has been developed. The second part of the paper presents in detail the simulation model (equipment modeling, dynamical simulation of the terminal structure, operating modes management) and the associated outputs. A System Test Bed (STB) using functional breadboards of each terminal equipment and simulating two terminals in real time, has been built in order to demonstrate the feasibility and assess the performances of an intersatellite optical communication link. The third part of the paper describes the chosen design and architecture for the PAT validation on STB. The last part of the paper will show the validation of a pointing system for optical intersatellite communication, thanks to the combination of simulations and STB measurements.!
机译:摘要:本文介绍了欧洲SILEX程序(半导体激光星际链路实验)的定点捕获与跟踪(PAT)子系统的仿真模型和地面性能验证。 SILEX方案由安装在低地球轨道(SPOT 4)和对地静止轨道(ARTEMIS)航天器上的两个终端组成。由于激光束发散角有限(典型的星际距离为45000 km),因此需要非常精确的指向性能。 PAT子系统负责链接(获取)的初始化,入射光束的跟踪以及发射激光束的指向。考虑到所有干扰源(主机航天器的振动,机电或光学噪声),在1 kHz的频率带宽上,指向性能小于2 $ mu @ rad。在第一部分中,简要介绍了保留的策略(PAT任务的阶段,操作模式)和功能体系结构(控制律,采样频率)。为了验证基于设备级别的测量和子系统级别的分析的PAT性能评估,已经开发了完整的时间仿真软件。本文的第二部分详细介绍了仿真模型(设备建模,终端结构的动态仿真,操作模式管理)和相关的输出。为了证明可行性和评估星际光通信链路的性能,已经建立了使用每个终端设备的功能面包板并实时模拟两个终端的系统测试台(STB)。本文的第三部分描述了STB上PAT验证的所选设计和体系结构。由于仿真和机顶盒测量相结合,本文的最后一部分将展示用于卫星间光通信的指向系统的验证。

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