卫星激光通信滤光膜的研制

为满足卫星激光通信中超高速数据传输的特殊要求,采用电子束和离子辅助沉积技术,制备了532 nm、632 nm和1 064 nm波长处高反射,808 nm和1 550 nm处高透射的多波段滤光膜.选取了H₄和SiO₂作为高低折射率材料,通过对膜系设计曲线的不断优化,减少了灵敏层的个数,得到了相对易于制备的膜系结构;采用电子束加热蒸发方法并加以离子辅助沉积系统制备薄膜, 采用光控与晶控同时监控的方法控制膜厚;通过不断调整工艺,提高了薄膜的抗激光损伤能力,减小了膜厚控制误差,提高了透射波段的透过率及反射波段的反射率,最终得到了光谱性能较好的滤光膜.该薄膜能够承受雨淋、盐雾、高低温等环境测试,满足使用要求.     

多晶硅片反应离子刻蚀制绒后扩散工艺的匹配性

根据机载激光通信的环境和链路距离,采用光电粗精复合轴结构,提出一种双探测器、双光轴机载激光通信复合轴捕获跟踪瞄准系统方案.对整个系统的光路结构进行了分析和优化设计,使粗跟踪精度达120 μrad,精跟踪系统带宽大于300 Hz,执行动态范围达5 mrad,跟踪精度达3 μrad,并成功实现通信距离17.5 km、通信速率1.5 Gbps,误码率达1E-7的飞机对地面激光通信实验.     

无线光链路快速同步技术

介绍了一种小型无线激光通信系统的硬件结构以及针对该硬件的物理层收发协议。具体阐述了该协议中采用的快速同步技术,该技术能够降低通信终端间同步过程中的带宽浪费。在硬件结构中,主要介绍了激光驱动系统、信号放大和整形系统以及信号接口。硬件相关的物理层协议主要用于外部信号接口、数据流的串行化和解串行化、传输错误在线检测以及传输调度。系统主要针对地基无线光通信设计,使用多相位采样技术在本地生成接收端的采样时钟,与基于PLL的时钟复原方法相比具有更快的同步速度,有效提高了无线光通信系统的带宽利用率,降低了通信误码率。     

Model-based predictive controller design for a class of nonlinear networked systems with communication delays and data loss

This paper discusses the model-based predictive controller design of networked nonlinear systems with communication delay and data loss. Based on the analysis of the closed-loop networked predictive control systems, the model-based networked predictive control strategy can compensate for communication delay and data loss in an active way. The designed model-based predictive controller can also guarantee the stability of the closed-loop networked system. The simulation results demonstrate the feasibility and efficacy of the proposed model-based predictive controller design scheme.     

Finite-time sliding mode synchronization of chaotic systems

A new finite-time sliding mode control approach is presented for synchronizing two different topological structure chaotic systems. With the help of the Lyapunov method, the convergence property of the proposed control strategy is discussed in a rigorous manner. Furthermore, it is mathematically proved that our control strategy has a faster convergence speed than the conventional finite-time sliding mode control scheme. In addition, the proposed control strategy can ensure the finite-time synchronization between the master and the slave chaotic systems under internal uncertainties and external disturbances. Simulation results are provided to show the speediness and robustness of the proposed scheme. It is worth noticing that the proposed control scheme is applicable for secure communications.     

机载激光通信终端的模糊变结构跟踪方法研究(英文)

为避免经典固定模型集合中多模型算法造成的模型间竞争并减小计算量,基于有向图切换的变结构方法,建立有向图切换规则和较完备的模型集合.通过模糊逻辑推理得到模型集合中各模型的匹配度,以此代替传统多模型算法中的模式概率来计算,降低了计算的复杂度.采用核粒子滤波克服了标准粒子滤波没有考虑到的量测信息问题,即粒子能够通过核密度估计后朝着状态的后验概率密度的模型移动,使真实和估计模型之间的均方误差最小.仿真结果表明,基于模糊理论的变结构核粒子滤波算法能较大地提高跟踪准确度和减少计算量.     

在轨卫星星等建模与计算

星等的大小代表了星体对于人眼的可观测程度。卫星星等的理论计算对于观测跟踪卫星光学系统设计等具有重要的指导意义。结合天文学、轨道动力学、辐射度学、光度学和计算数学理论,建立了计算人造卫星星等的物理数学模型。计算了卫星的可见光反射能量随轨道运行的瞬时特征,结合人眼的视觉特性,推导出了轨道卫星星等的计算方法,并进一步针对卫星表面为灰体的情况给出了一种计算卫星星等的方法及星下点卫星星等的周期性计算曲线,结果表明:星下点观测的卫星星等随卫星在轨道上位置的变化非常显著,对同一卫星,不同星下点观测到的星等差异仅在日照区就可达5个等级之多。     

带时延与丢包的网络化多智能体系统控制器设计

网络时延与数据丢包极大地降低了网络化多智能体系统的控制性能,甚至会破坏稳定性.考虑存在网络时延与数据丢包的网络化多智能体系统,提出了一种基于时延与丢包补偿机制的预测控制器设计方法,来主动地消除网络时延与数据丢包的影响.通过对网络化多智能体预测控制系统的分析,给出了能够保证系统稳定性与一致性的控制器设计步骤.最后的仿真实例表明了该方法的有效性.     

Physical analysis on improving the recovery accuracy of the Earth’s gravity field by a combination of satellite observations in along-track and cross-track directions

The physical investigations on the accuracy improvement to the measurement of the Earth＇s gravity field recovery are carried out based on the next-generation Pendulum-A/B out-of-plane twin-satellite formation in this paper. Firstly, the Earth＇s gravity field complete up to degree and order 100 is, respectively, recovered by the collinear and pendulum satellite formations using the orbital parameters of the satellite and the matching accuracies of key payloads from the twin GRACE satellites. The research results show that the accuracy of the Earth＇s gravity field model from the Pendulum-A/B satellite formation is about two times higher than from the collinear satellite formation, and the further improvement of the determination accuracy of the Earth＇s gravity field model is feasible by the next-generation Pendulum-A/B out-of-plane twin-satellite formation. Secondly, the Earth＇s gravity field from Pendulum-A/B complete up to degree and order 100 is accurately recovered based on the orbital parameters of the satellite （e.g., an orbital altitude of 400 km, an intersatellite range of 100 km, an orbital inclination of 89° and an orbital eccentricity of 0.001）, the matching accuracies of space- borne instruments （e.g. 10-6 m in the intersatellite range, 10-3 m in the orbital position, 10-6 m/s in orbital velocity, and 10-11 m/s2 in non-conservative force）, an observation time of 30 days and a sampling interval of 10 s. The measurement accuracy of the Earth＇s gravity field from the next-generation Pendulum-A/B out-of-plane twin-satellite formation is full of promise for being improved by about l0 times compared with that from the current GRACE satellite formation. Finally, the physical requirements for the next-generation Pendulum-A/B out-of-plane twin-satellite formation are analyzed, and it is proposed that the satellite orbital altitude be preferably designed to be close to 400±50 km and the matching precision of key sensors from the Pendulum-A/B mission be about one order of magnitude higher tha     

Bit error rate analysis with real-time pointing errors correction in free space optical communication systems

Pointing errors caused by the atmospheric turbulence will degrade the performance of free space optical (FSO) communication systems, especially the bit error rate (BER). In this paper, we innovatively analyze the relationship between BER and pointing errors by the probability density functions (PDFs) and intensity displacement in focal plane under the On-Off Keying (OOK) modulation conditions. The closed-loop experimental system is set up in laboratory, where the fast steering mirror (FSM) is real-time controlled by embedded controller with the parallel processing technology and the atmospheric turbulence is simulated by a turbulence simulation box. The results of repeated experiments show that the method of pointing errors correction we proposed is efficient under the conditions of atmospheric turbulence. By utilizing our method, the BER can decrease from nearly 10⁻³ to nearly or even below 10⁻⁹, thus improving the performance of FSO communication systems significantly.