高带宽量子通信信标跟踪技术研究

分析了ATP跟瞄相机的探测采样频率、闭环信号延时对ATP系统带宽的影响,并在此基础上,提出了高采样频率和低闭环延时的高带宽设计思路,设计并实现了高带宽ATP跟踪系统.仿真分析和试验测试结果表明:使用该跟瞄相机的ATP系统的干扰抑制带宽约为200Hz;在给定的输入条件下,系统跟瞄精度优于±lurad,能够满足星地量子通信的需求.     

自由空间光通信ATP技术的研究

自由空间光通信将成为一种可行且非常具有吸引力的通信方式．光束的捕获、跟踪和对准（ATP）是自由空间光通信中必须解决的关键技术之一，介绍了ATP系统的工作原理．详细论述了ATP系统组成、伺服控制系统的组成与工作流程、光束跟踪算法及其捕获方法．给出了该系统误差信号的处理方法．     

10.6μm激光大气通信的自动瞄准与跟踪

激光大气通信双端的自动瞄准与跟踪，是开发激光大气传输信道、赖以传送大容量信息的一个关键问题。本文在分析扰动大气对光束瞄准跟踪所产生的影响的基础上，提出了适于大气激光通信的跟瞄系统结构和设计准则，建立了跟瞄系统模型，合理地设计了数字式瞄准跟踪系统，并给出了光束跟踪系统的实验结果。１０．６μｍ大气通信瞄准问题，国内外还未见有更深入的研究报告。     

大气光通信PAT子系统指标初步设计分析

分析了跟踪角速度，功率，跟踪精度等因素对大气激光通信系统中瞄准，捕获和跟踪子系统参数选择的影响，给出了波束发散角，扫描角范围，接收视场等主要参数的选择原则，对地面终端光通信系统设计背景提出了瞄准，捕获和跟踪了系统的相应指标。     

一种基于捕获跟踪策略的光束发散角分析方法

根据捕获跟踪策略和激光检测理论，给出了直接探测情况下最佳光束发散角的表示式。利用这一表示式，分析了背景光功率和探测器暗电流效光功率对系统性能的影响，为大气激光通信系统中激光光束发散角的设计提供了参考依据。     

双机之间激光通信ATP技术研究

机载激光通信系统中,激光光束的对准是通信能否进行的关键,采用ATP(捕获、跟踪和瞄准)技术来解决两机光端机的对准问题。主要进行了两机之间信标光捕获方法研究以及对跟踪和瞄准光学系统进行设计。给出了具体计算的原理方法和数学模型,同时对ATP系统的跟踪和瞄准精度指标进行确定。     

自由空间光通信ATP系统关键技术研究

自由空间光通信将成为未来通信的最佳解决方案之一。首先需要解决实现空间光通信的关键问题是光束的捕获、跟踪和瞄准。该文介绍了自由空间光通信终端机中ATP系统的组成和工作原理，设计了用于ATP系统的精瞄偏转镜、闭环控制器、星上终端二次电源系统，并给出了该系统性能的测试结果。     

基于FSO自由空间光通信中自动伺服系统的研究

在空间光通信中,为建立可靠的通信链路,捕获跟踪瞄准技术成为了ATP系统的关键所在,伺服系统主要采用了复合轴的控制结构,即粗跟踪和精跟踪两部分,精跟踪是建立在粗跟踪的基础上的,主要是为抑制粗跟踪中残差所引起的扰动。随后对伺服系统的关键参数进行分析,指出提高灵敏度和跟瞄精度的重要性,最后对ATP伺服系统的传递函数进行推导与仿真,得出结果完全满足系统跟踪控制的要求。     

高能激光武器的跟瞄精度要求分析

从高能激光武器的跟瞄精度要求与激光武器发射的激光束传输到目标处时的角发散量间的关系出发，导出了高能激光武器跟瞄精度要求的数学表达式，并据此分析了目标的远近、大气湍流的强弱和系统的性能参数等对跟瞄精度要求的影响，给出了一些情况下跟瞄精度要求的计算结果。     

通信

0217869大气光通信 PAT 子系统指标初步设计分析[刊]/唐涛//红外与激光工程.—2002,31(3).—280～282(E)分析了跟踪角速度、功率、跟踪精度等因素对大气激光通信系统中瞄准、捕获和跟踪子系统参数选择的影响,给出了波束发散角、扫描角范围、接收视场等主要参数的选择原则,对地面终端光通信系统设计背景提出了瞄准、捕获和跟踪子系统的相应指标。参3     

Analysis of optical coherence multiplexing networks for satellite communication

Free-space optical communication between satellites networked together can enable a high data rate between the satellites. Coherence multiplexing (CM) is an attractive technique for satellite networking due to its ability to cope with the asynchronous nature of communication traffic and the dynamic changes taking place in the satellite constellation. The use of optical radiation for intersatellite links creates very narrow beam divergence angles. Due to the narrow beam divergence angle, the vibration of the pointing system, the movement of the satellite, and the large distance between them the pointing from one satellite to another is a complicated task. The vibration of the pointing system is caused by two stochastic fundamental mechanisms: 1) tracking noises created by the electrooptic tracker and 2) vibrations created by internal satellite mechanical mechanisms and external environments. We derive mathematical models of signal, noise, the approximate signal-to-noise ratio, and the approximate bit-error rates of optical communication satellite networks as functions of the system's parameters, the number of satellites, and the vibration amplitude for frequency-shift keying coherence multiplexing (FSK-CM). Based on these models, we can calculate the negative impact of both the number of satellites and the optical terminal vibration on the system's performance.     

激光星间通信终端精瞄微定位系统研究现状

激光星间通信是未来通信的最佳解决方案之一,激光束的捕获、瞄准和跟踪技术(APT)是激光星间通信的关键技术。精瞄微定位系统是APT系统的重要组成部分,与粗瞄系统配合执行激光束的捕获、瞄准和跟踪任务。该文介绍了精瞄微定位系统的关键技术,详细阐述了精瞄偏转镜机构、驱动检测技术及控制方法等关键技术的国内外研究现状,指明了系统的发展趋势,对进一步研究微定位系统具有指导意义。     

The SILEX optical interorbit link experiment

The European Space Agency (ESA) has instigated an in-orbit demonstration project known as SILEX (semiconductor laser intersatellite link experiment) using a pre-operational link between the French SPOT-4 low earth orbit satellite and the ESA Advanced Relay and Technology Mission Satellite (ARTEMIS). Such an optical communication system brings some new and challenging requirements. In particular, the communication beam, which has a divergence of around 6 μrad, must achieve and maintain a very demanding pointing accuracy in the presence of both host satellite vibration and relative satellite motion. The authors provide an overview of the SILEX project and describe a novel pointing mechanism     

瞄准误差和Gamma-Gamma大气湍流下信号束散角的优化分析

在自由空间激光通信(FSO)系统中,瞄准误差和大气湍流严重影响系统通信链路,是链路性能恶化的两大主要因素.通过对联合信道的理论分析,建立了信道模型,并利用Meijer G函数推导出了直接探测系统和相干探测系统平均信道容量的表达式.通过在Matlab中的仿真结果可知,在给定瞄准误差和大气湍流的条件下,信号光的光束束散角并非越小越好,而是存在最优束散角,该束散角不仅可以保证系统性能良好,而且使得发射系统功率取得最小值,并且采用相干探测系统可以抑制大气湍流对系统的影响,有效提高系统的性能.     

Laser satellite communication network-vibration effect and possiblesolutions

A number of serious consortiums develop satellite communication networks. The objective of these communication projects is to service personal communication users almost everywhere on Earth. The intersatellite links in those projects use microwave radiation as the carrier. Free-space optical communication between satellites networked together can make possible high-speed communication between different places on Earth. Some advantages of an optical communication system over a microwave communication system in free space are: (1) smaller size and weight, (2) less transmitter power, (3) larger bandwidth, and (4) higher immunity to interference. The pointing from one satellite to another is a complicated problem due to the large distance between the satellite, the narrow beam divergence angle, and vibration of the pointing system. Such vibration of the transmitted beam in the receiver plane decreases the average received signal, which increases the bit error rate. We review: (1) the present status of satellite networks, (2) developing efforts of optical satellite communication around the world, (3) performance results of vibration effects on different kinds of optical communication satellite networks, and (4) seven approaches to overcome the problems caused by transmitter pointing vibration     

星间光通信链路优化设计

建立了一种空间光通信链路模型,对光通信链路的总体性能进行了仿真计算,并研究了在一定误码率、一定发射功率下优化通信光束发散角与径向偏角方差的关系。     

一种自由空间光通信光路的设计与分析

提出了一种用于自由空间光通信的光学系统的设计方法,在这种设计方法中通过卡塞格伦天线实现对激光束的准直,通过偏振分光镜和γ/2波片的巧妙使用来减少杂散光和反射光对信号光的干扰,通过对光学系统的自动跟踪控制消除了通信终端的失准问题。分析和实验表明,基于该光学系统的通信终端激光发散角达到0.4 mrad,对准误差小于6μrad,可实现2 km的自由空间光通信。